~ubuntu-branches/ubuntu/quantal/flightgear/quantal

« back to all changes in this revision

Viewing changes to src/FDM/UIUCModel/uiuc_menu.cpp

Committer: Bazaar Package Importer
Author(s): Ove Kaaven
Date: 2002-03-27 21:50:15 UTC
Revision ID: james.westby@ubuntu.com-20020327215015-0rvi3o8iml0a8s93

Tags: upstream-0.7.9

Import upstream version 0.7.9

files added:

AUTHORS

COPYING

ChangeLog

FlightGear.dsp

FlightGear.dsw

INSTALL

Makefile.am

Makefile.in

NEWS

README

Thanks

acconfig.h

aclocal.m4

acsite.m4

config.guess

config.sub

configure

configure.in

docs-mini

docs-mini/AptNavFAQ.FlightGear.html

docs-mini/FlightGear-FAQ.html

docs-mini/README.Cygwin

docs-mini/README.IO

docs-mini/README.IRIX

docs-mini/README.JSBSim

docs-mini/README.Joystick

docs-mini/README.Linux

docs-mini/README.MSVC

docs-mini/README.MacOS

docs-mini/README.SimGear

docs-mini/README.Unix

docs-mini/README.Win32-X

docs-mini/README.autoconf

docs-mini/README.fgjs

docs-mini/README.plib

docs-mini/README.running

docs-mini/README.src

docs-mini/README.uiuc

docs-mini/README.xmlhud

docs-mini/README.xmlpanel

docs-mini/model-howto.html

docs-mini/model.jpg

docs-mini/properties.txt

install-sh

irix-hack.sh

man/Makefile.am

man/Makefile.in

man/est-epsilon.1.in

man/fgfs.1.in

man/fgjs.1.in

man/gl-info.1.in

man/js_demo.1.in

man/pstest.1.in

missing

mkinstalldirs

src/ATC

src/ATC/ATCdisplay.cxx

src/ATC/ATCdisplay.hxx

src/ATC/Makefile.am

src/ATC/Makefile.in

src/ATC/atis.cxx

src/ATC/atis.hxx

src/ATC/atislist.cxx

src/ATC/atislist.hxx

src/Aircraft

src/Aircraft/Makefile.am

src/Aircraft/Makefile.in

src/Aircraft/aircraft.cxx

src/Aircraft/aircraft.hxx

src/Airports

src/Airports/Makefile.am

src/Airports/Makefile.in

src/Airports/genrunways.cxx

src/Airports/gensimple.cxx

src/Airports/runways.cxx

src/Airports/runways.hxx

src/Airports/simple.cxx

src/Airports/simple.hxx

src/Autopilot

src/Autopilot/Makefile.am

src/Autopilot/Makefile.in

src/Autopilot/auto_gui.cxx

src/Autopilot/auto_gui.hxx

src/Autopilot/newauto.cxx

src/Autopilot/newauto.hxx

src/Cockpit

src/Cockpit/Makefile.am

src/Cockpit/Makefile.in

src/Cockpit/cockpit.cxx

src/Cockpit/cockpit.hxx

src/Cockpit/hud.cxx

src/Cockpit/hud.hxx

src/Cockpit/hud_card.cxx

src/Cockpit/hud_dnst.cxx

src/Cockpit/hud_gaug.cxx

src/Cockpit/hud_inst.cxx

src/Cockpit/hud_labl.cxx

src/Cockpit/hud_ladr.cxx

src/Cockpit/hud_lat.cxx

src/Cockpit/hud_lon.cxx

src/Cockpit/hud_opts.hxx

src/Cockpit/hud_scal.cxx

src/Cockpit/hud_tbi.cxx

src/Cockpit/panel.cxx

src/Cockpit/panel.hxx

src/Cockpit/panel_io.cxx

src/Cockpit/panel_io.hxx

src/Cockpit/radiostack.cxx

src/Cockpit/radiostack.hxx

src/Cockpit/steam.cxx

src/Cockpit/steam.hxx

src/Controls

src/Controls/Makefile.am

src/Controls/Makefile.in

src/Controls/controls.cxx

src/Controls/controls.hxx

src/FDM

src/FDM/ADA.cxx

src/FDM/ADA.hxx

src/FDM/Balloon

src/FDM/Balloon.cxx

src/FDM/Balloon.h

src/FDM/Balloon/BalloonSim.cpp

src/FDM/Balloon/BalloonSim.h

src/FDM/Balloon/Makefile.am

src/FDM/Balloon/Makefile.in

src/FDM/External.cxx

src/FDM/External.hxx

src/FDM/ExternalNet.cxx

src/FDM/ExternalNet.hxx

src/FDM/IO360.cxx

src/FDM/IO360.hxx

src/FDM/JSBSim

src/FDM/JSBSim.cxx

src/FDM/JSBSim.hxx

src/FDM/JSBSim/AUTHORS

src/FDM/JSBSim/FGAerodynamics.cpp

src/FDM/JSBSim/FGAerodynamics.h

src/FDM/JSBSim/FGAircraft.cpp

src/FDM/JSBSim/FGAircraft.h

src/FDM/JSBSim/FGAtmosphere.cpp

src/FDM/JSBSim/FGAtmosphere.h

src/FDM/JSBSim/FGAuxiliary.cpp

src/FDM/JSBSim/FGAuxiliary.h

src/FDM/JSBSim/FGCoefficient.cpp

src/FDM/JSBSim/FGCoefficient.h

src/FDM/JSBSim/FGColumnVector3.cpp

src/FDM/JSBSim/FGColumnVector3.h

src/FDM/JSBSim/FGColumnVector4.cpp

src/FDM/JSBSim/FGColumnVector4.h

src/FDM/JSBSim/FGConfigFile.cpp

src/FDM/JSBSim/FGConfigFile.h

src/FDM/JSBSim/FGDefs.h

src/FDM/JSBSim/FGEngine.cpp

src/FDM/JSBSim/FGEngine.h

src/FDM/JSBSim/FGFCS.cpp

src/FDM/JSBSim/FGFCS.h

src/FDM/JSBSim/FGFDMExec.cpp

src/FDM/JSBSim/FGFDMExec.h

src/FDM/JSBSim/FGFactorGroup.cpp

src/FDM/JSBSim/FGFactorGroup.h

src/FDM/JSBSim/FGForce.cpp

src/FDM/JSBSim/FGForce.h

src/FDM/JSBSim/FGGroundReactions.cpp

src/FDM/JSBSim/FGGroundReactions.h

src/FDM/JSBSim/FGInertial.cpp

src/FDM/JSBSim/FGInertial.h

src/FDM/JSBSim/FGInitialCondition.cpp

src/FDM/JSBSim/FGInitialCondition.h

src/FDM/JSBSim/FGJSBBase.cpp

src/FDM/JSBSim/FGJSBBase.h

src/FDM/JSBSim/FGLGear.cpp

src/FDM/JSBSim/FGLGear.h

src/FDM/JSBSim/FGMassBalance.cpp

src/FDM/JSBSim/FGMassBalance.h

src/FDM/JSBSim/FGMatrix33.cpp

src/FDM/JSBSim/FGMatrix33.h

src/FDM/JSBSim/FGModel.cpp

src/FDM/JSBSim/FGModel.h

src/FDM/JSBSim/FGNozzle.cpp

src/FDM/JSBSim/FGNozzle.h

src/FDM/JSBSim/FGOutput.cpp

src/FDM/JSBSim/FGOutput.h

src/FDM/JSBSim/FGPiston.cpp

src/FDM/JSBSim/FGPiston.h

src/FDM/JSBSim/FGPosition.cpp

src/FDM/JSBSim/FGPosition.h

src/FDM/JSBSim/FGPropeller.cpp

src/FDM/JSBSim/FGPropeller.h

src/FDM/JSBSim/FGPropulsion.cpp

src/FDM/JSBSim/FGPropulsion.h

src/FDM/JSBSim/FGRocket.cpp

src/FDM/JSBSim/FGRocket.h

src/FDM/JSBSim/FGRotation.cpp

src/FDM/JSBSim/FGRotation.h

src/FDM/JSBSim/FGScript.cpp

src/FDM/JSBSim/FGScript.h

src/FDM/JSBSim/FGState.cpp

src/FDM/JSBSim/FGState.h

src/FDM/JSBSim/FGTable.cpp

src/FDM/JSBSim/FGTable.h

src/FDM/JSBSim/FGTank.cpp

src/FDM/JSBSim/FGTank.h

src/FDM/JSBSim/FGThruster.cpp

src/FDM/JSBSim/FGThruster.h

src/FDM/JSBSim/FGTranslation.cpp

src/FDM/JSBSim/FGTranslation.h

src/FDM/JSBSim/FGTrim.cpp

src/FDM/JSBSim/FGTrim.h

src/FDM/JSBSim/FGTrimAxis.cpp

src/FDM/JSBSim/FGTrimAxis.h

src/FDM/JSBSim/FGTurboJet.cpp

src/FDM/JSBSim/FGTurboJet.h

src/FDM/JSBSim/FGTurboProp.cpp

src/FDM/JSBSim/FGTurboProp.h

src/FDM/JSBSim/FGTurboShaft.cpp

src/FDM/JSBSim/FGTurboShaft.h

src/FDM/JSBSim/FGUtility.cpp

src/FDM/JSBSim/FGUtility.h

src/FDM/JSBSim/FGfdmSocket.cpp

src/FDM/JSBSim/FGfdmSocket.h

src/FDM/JSBSim/JSBSim.cpp

src/FDM/JSBSim/Makefile.am

src/FDM/JSBSim/Makefile.in

src/FDM/JSBSim/Makefile.solo

src/FDM/JSBSim/README

src/FDM/JSBSim/filtersjb

src/FDM/JSBSim/filtersjb/FGDeadBand.cpp

src/FDM/JSBSim/filtersjb/FGDeadBand.h

src/FDM/JSBSim/filtersjb/FGFCSComponent.cpp

src/FDM/JSBSim/filtersjb/FGFCSComponent.h

src/FDM/JSBSim/filtersjb/FGFilter.cpp

src/FDM/JSBSim/filtersjb/FGFilter.h

src/FDM/JSBSim/filtersjb/FGGain.cpp

src/FDM/JSBSim/filtersjb/FGGain.h

src/FDM/JSBSim/filtersjb/FGGradient.cpp

src/FDM/JSBSim/filtersjb/FGGradient.h

src/FDM/JSBSim/filtersjb/FGKinemat.cpp

src/FDM/JSBSim/filtersjb/FGKinemat.h

src/FDM/JSBSim/filtersjb/FGSummer.cpp

src/FDM/JSBSim/filtersjb/FGSummer.h

src/FDM/JSBSim/filtersjb/FGSwitch.cpp

src/FDM/JSBSim/filtersjb/FGSwitch.h

src/FDM/JSBSim/filtersjb/Makefile.am

src/FDM/JSBSim/filtersjb/Makefile.in

src/FDM/JSBSim/filtersjb/Makefile.solo

src/FDM/LaRCsim

src/FDM/LaRCsim.cxx

src/FDM/LaRCsim.hxx

src/FDM/LaRCsim/Makefile.am

src/FDM/LaRCsim/Makefile.in

src/FDM/LaRCsim/atmos_62.c

src/FDM/LaRCsim/atmos_62.h

src/FDM/LaRCsim/c172_aero.c

src/FDM/LaRCsim/c172_aero.h

src/FDM/LaRCsim/c172_engine.c

src/FDM/LaRCsim/c172_gear.c

src/FDM/LaRCsim/c172_init.c

src/FDM/LaRCsim/cherokee_aero.c

src/FDM/LaRCsim/cherokee_engine.c

src/FDM/LaRCsim/cherokee_gear.c

src/FDM/LaRCsim/cherokee_init.c

src/FDM/LaRCsim/default_model_routines.c

src/FDM/LaRCsim/default_model_routines.h

src/FDM/LaRCsim/ls_accel.c

src/FDM/LaRCsim/ls_accel.h

src/FDM/LaRCsim/ls_aux.c

src/FDM/LaRCsim/ls_aux.h

src/FDM/LaRCsim/ls_cockpit.h

src/FDM/LaRCsim/ls_constants.h

src/FDM/LaRCsim/ls_generic.h

src/FDM/LaRCsim/ls_geodesy.c

src/FDM/LaRCsim/ls_geodesy.h

src/FDM/LaRCsim/ls_gravity.c

src/FDM/LaRCsim/ls_gravity.h

src/FDM/LaRCsim/ls_init.c

src/FDM/LaRCsim/ls_init.h

src/FDM/LaRCsim/ls_interface.c

src/FDM/LaRCsim/ls_interface.h

src/FDM/LaRCsim/ls_matrix.c

src/FDM/LaRCsim/ls_matrix.h

src/FDM/LaRCsim/ls_model.c

src/FDM/LaRCsim/ls_model.h

src/FDM/LaRCsim/ls_sim_control.h

src/FDM/LaRCsim/ls_step.c

src/FDM/LaRCsim/ls_step.h

src/FDM/LaRCsim/ls_sym.h

src/FDM/LaRCsim/ls_trim.c

src/FDM/LaRCsim/ls_types.h

src/FDM/LaRCsim/navion_aero.c

src/FDM/LaRCsim/navion_engine.c

src/FDM/LaRCsim/navion_gear.c

src/FDM/LaRCsim/navion_init.c

src/FDM/LaRCsim/navion_init.h

src/FDM/LaRCsim/uiuc_aero.c

src/FDM/LaRCsimIC.cxx

src/FDM/LaRCsimIC.hxx

src/FDM/MagicCarpet.cxx

src/FDM/MagicCarpet.hxx

src/FDM/Makefile.am

src/FDM/Makefile.in

src/FDM/NullFDM.cxx

src/FDM/NullFDM.hxx

src/FDM/UIUCModel

src/FDM/UIUCModel/Makefile.am

src/FDM/UIUCModel/Makefile.in

src/FDM/UIUCModel/uiuc_1DdataFileReader.cpp

src/FDM/UIUCModel/uiuc_1DdataFileReader.h

src/FDM/UIUCModel/uiuc_1Dinterpolation.cpp

src/FDM/UIUCModel/uiuc_1Dinterpolation.h

src/FDM/UIUCModel/uiuc_2DdataFileReader.cpp

src/FDM/UIUCModel/uiuc_2DdataFileReader.h

src/FDM/UIUCModel/uiuc_2Dinterpolation.cpp

src/FDM/UIUCModel/uiuc_2Dinterpolation.h

src/FDM/UIUCModel/uiuc_aerodeflections.cpp

src/FDM/UIUCModel/uiuc_aerodeflections.h

src/FDM/UIUCModel/uiuc_aircraft.h

src/FDM/UIUCModel/uiuc_aircraftdir.h

src/FDM/UIUCModel/uiuc_betaprobe.cpp

src/FDM/UIUCModel/uiuc_betaprobe.h

src/FDM/UIUCModel/uiuc_coef_drag.cpp

src/FDM/UIUCModel/uiuc_coef_drag.h

src/FDM/UIUCModel/uiuc_coef_lift.cpp

src/FDM/UIUCModel/uiuc_coef_lift.h

src/FDM/UIUCModel/uiuc_coef_pitch.cpp

src/FDM/UIUCModel/uiuc_coef_pitch.h

src/FDM/UIUCModel/uiuc_coef_roll.cpp

src/FDM/UIUCModel/uiuc_coef_roll.h

src/FDM/UIUCModel/uiuc_coef_sideforce.cpp

src/FDM/UIUCModel/uiuc_coef_sideforce.h

src/FDM/UIUCModel/uiuc_coef_yaw.cpp

src/FDM/UIUCModel/uiuc_coef_yaw.h

src/FDM/UIUCModel/uiuc_coefficients.cpp

src/FDM/UIUCModel/uiuc_coefficients.h

src/FDM/UIUCModel/uiuc_controlInput.cpp

src/FDM/UIUCModel/uiuc_controlInput.h

src/FDM/UIUCModel/uiuc_convert.cpp

src/FDM/UIUCModel/uiuc_convert.h

src/FDM/UIUCModel/uiuc_engine.cpp

src/FDM/UIUCModel/uiuc_engine.h

src/FDM/UIUCModel/uiuc_fog.cpp

src/FDM/UIUCModel/uiuc_fog.h

src/FDM/UIUCModel/uiuc_gear.cpp

src/FDM/UIUCModel/uiuc_gear.h

src/FDM/UIUCModel/uiuc_ice.cpp

src/FDM/UIUCModel/uiuc_ice.h

src/FDM/UIUCModel/uiuc_initializemaps.cpp

src/FDM/UIUCModel/uiuc_initializemaps.h

src/FDM/UIUCModel/uiuc_map_CD.cpp

src/FDM/UIUCModel/uiuc_map_CD.h

src/FDM/UIUCModel/uiuc_map_CL.cpp

src/FDM/UIUCModel/uiuc_map_CL.h

src/FDM/UIUCModel/uiuc_map_CY.cpp

src/FDM/UIUCModel/uiuc_map_CY.h

src/FDM/UIUCModel/uiuc_map_Cm.cpp

src/FDM/UIUCModel/uiuc_map_Cm.h

src/FDM/UIUCModel/uiuc_map_Cn.cpp

src/FDM/UIUCModel/uiuc_map_Cn.h

src/FDM/UIUCModel/uiuc_map_Croll.cpp

src/FDM/UIUCModel/uiuc_map_Croll.h

src/FDM/UIUCModel/uiuc_map_controlSurface.cpp

src/FDM/UIUCModel/uiuc_map_controlSurface.h

src/FDM/UIUCModel/uiuc_map_engine.cpp

src/FDM/UIUCModel/uiuc_map_engine.h

src/FDM/UIUCModel/uiuc_map_fog.cpp

src/FDM/UIUCModel/uiuc_map_fog.h

src/FDM/UIUCModel/uiuc_map_gear.cpp

src/FDM/UIUCModel/uiuc_map_gear.h

src/FDM/UIUCModel/uiuc_map_geometry.cpp

src/FDM/UIUCModel/uiuc_map_geometry.h

src/FDM/UIUCModel/uiuc_map_ice.cpp

src/FDM/UIUCModel/uiuc_map_ice.h

src/FDM/UIUCModel/uiuc_map_init.cpp

src/FDM/UIUCModel/uiuc_map_init.h

src/FDM/UIUCModel/uiuc_map_keyword.cpp

src/FDM/UIUCModel/uiuc_map_keyword.h

src/FDM/UIUCModel/uiuc_map_mass.cpp

src/FDM/UIUCModel/uiuc_map_mass.h

src/FDM/UIUCModel/uiuc_map_misc.cpp

src/FDM/UIUCModel/uiuc_map_misc.h

src/FDM/UIUCModel/uiuc_map_record1.cpp

src/FDM/UIUCModel/uiuc_map_record1.h

src/FDM/UIUCModel/uiuc_map_record2.cpp

src/FDM/UIUCModel/uiuc_map_record2.h

src/FDM/UIUCModel/uiuc_map_record3.cpp

src/FDM/UIUCModel/uiuc_map_record3.h

src/FDM/UIUCModel/uiuc_map_record4.cpp

src/FDM/UIUCModel/uiuc_map_record4.h

src/FDM/UIUCModel/uiuc_map_record5.cpp

src/FDM/UIUCModel/uiuc_map_record5.h

src/FDM/UIUCModel/uiuc_menu.cpp

src/FDM/UIUCModel/uiuc_menu.h

src/FDM/UIUCModel/uiuc_parsefile.cpp

src/FDM/UIUCModel/uiuc_parsefile.h

src/FDM/UIUCModel/uiuc_recorder.cpp

src/FDM/UIUCModel/uiuc_recorder.h

src/FDM/UIUCModel/uiuc_warnings_errors.cpp

src/FDM/UIUCModel/uiuc_warnings_errors.h

src/FDM/UIUCModel/uiuc_wrapper.cpp

src/FDM/UIUCModel/uiuc_wrapper.h

src/FDM/YASim

src/FDM/YASim/Airplane.cpp

src/FDM/YASim/Airplane.hpp

src/FDM/YASim/Atmosphere.cpp

src/FDM/YASim/Atmosphere.hpp

src/FDM/YASim/BodyEnvironment.hpp

src/FDM/YASim/ControlMap.cpp

src/FDM/YASim/ControlMap.hpp

src/FDM/YASim/FGFDM.cpp

src/FDM/YASim/FGFDM.hpp

src/FDM/YASim/Gear.cpp

src/FDM/YASim/Gear.hpp

src/FDM/YASim/Glue.cpp

src/FDM/YASim/Glue.hpp

src/FDM/YASim/Integrator.cpp

src/FDM/YASim/Integrator.hpp

src/FDM/YASim/Jet.cpp

src/FDM/YASim/Jet.hpp

src/FDM/YASim/Makefile.am

src/FDM/YASim/Makefile.in

src/FDM/YASim/Math.cpp

src/FDM/YASim/Math.hpp

src/FDM/YASim/Model.cpp

src/FDM/YASim/Model.hpp

src/FDM/YASim/PistonEngine.cpp

src/FDM/YASim/PistonEngine.hpp

src/FDM/YASim/PropEngine.cpp

src/FDM/YASim/PropEngine.hpp

src/FDM/YASim/Propeller.cpp

src/FDM/YASim/Propeller.hpp

src/FDM/YASim/RigidBody.cpp

src/FDM/YASim/RigidBody.hpp

src/FDM/YASim/SimpleJet.cpp

src/FDM/YASim/SimpleJet.hpp

src/FDM/YASim/Surface.cpp

src/FDM/YASim/Surface.hpp

src/FDM/YASim/Thruster.cpp

src/FDM/YASim/Thruster.hpp

src/FDM/YASim/Vector.hpp

src/FDM/YASim/Wing.cpp

src/FDM/YASim/Wing.hpp

src/FDM/YASim/YASim.cxx

src/FDM/YASim/YASim.hxx

src/FDM/flight.cxx

src/FDM/flight.hxx

src/FDM/ps-10520c.cxx

src/GUI

src/GUI/Makefile.am

src/GUI/Makefile.in

src/GUI/apt_dlg.cxx

src/GUI/apt_dlg.hxx

src/GUI/gui.cxx

src/GUI/gui.h

src/GUI/gui_local.cxx

src/GUI/gui_local.hxx

src/GUI/mouse.cxx

src/GUI/net_dlg.cxx

src/GUI/net_dlg.hxx

src/GUI/prop_picker.cxx

src/GUI/prop_picker.hxx

src/GUI/sgVec3Slider.cxx

src/GUI/sgVec3Slider.hxx

src/GUI/trackball.c

src/GUI/trackball.h

src/Include

src/Include/Makefile.am

src/Include/Makefile.in

src/Include/auto_ptr.hxx

src/Include/cmdargs.h

src/Include/config.h-msvc6

src/Include/config.h.in

src/Include/fg_callback.hxx

src/Include/fg_stl_config.h

src/Include/fg_typedefs.h

src/Include/general.hxx

src/Include/stamp-h.in

src/Include/version.h.in

src/Input

src/Input/Makefile.am

src/Input/Makefile.in

src/Input/fgjs.cxx

src/Input/input.cxx

src/Input/input.hxx

src/Input/js_demo.cxx

src/Input/jsinput.cxx

src/Input/jsinput.h

src/Input/jssuper.cxx

src/Input/jssuper.h

src/Main

src/Main/3dfx.sh

src/Main/Makefile.am

src/Main/Makefile.in

src/Main/fg_commands.cxx

src/Main/fg_commands.hxx

src/Main/fg_init.cxx

src/Main/fg_init.hxx

src/Main/fg_io.cxx

src/Main/fg_io.hxx

src/Main/fg_props.cxx

src/Main/fg_props.hxx

src/Main/fgfs.cxx

src/Main/fgfs.hxx

src/Main/globals.cxx

src/Main/globals.hxx

src/Main/main.cxx

src/Main/options.cxx

src/Main/options.hxx

src/Main/runfgfs.bat.in

src/Main/runfgfs.in

src/Main/splash.cxx

src/Main/splash.hxx

src/Main/viewer.cxx

src/Main/viewer.hxx

src/Main/viewer_lookat.cxx

src/Main/viewer_lookat.hxx

src/Main/viewer_rph.cxx

src/Main/viewer_rph.hxx

src/Main/viewmgr.cxx

src/Main/viewmgr.hxx

src/Makefile.am

src/Makefile.in

src/Navaids

src/Navaids/Makefile.am

src/Navaids/Makefile.in

src/Navaids/fix.hxx

src/Navaids/fixlist.cxx

src/Navaids/fixlist.hxx

src/Navaids/ils.hxx

src/Navaids/ilslist.cxx

src/Navaids/ilslist.hxx

src/Navaids/mkrbeacons.cxx

src/Navaids/mkrbeacons.hxx

src/Navaids/nav.hxx

src/Navaids/navlist.cxx

src/Navaids/navlist.hxx

src/Navaids/testnavs.cxx

src/Network

src/Network/Makefile.am

src/Network/Makefile.in

src/Network/atc610x.cxx

src/Network/atc610x.hxx

src/Network/atlas.cxx

src/Network/atlas.hxx

src/Network/garmin.cxx

src/Network/garmin.hxx

src/Network/httpd.cxx

src/Network/httpd.hxx

src/Network/joyclient.cxx

src/Network/joyclient.hxx

src/Network/jpg-httpd.cxx

src/Network/jpg-httpd.hxx

src/Network/native.cxx

src/Network/native.hxx

src/Network/native_ctrls.cxx

src/Network/native_ctrls.hxx

src/Network/native_fdm.cxx

src/Network/native_fdm.hxx

src/Network/net_fdm.hxx

src/Network/nmea.cxx

src/Network/nmea.hxx

src/Network/opengc.cxx

src/Network/opengc.hxx

src/Network/opengc_data.hxx

src/Network/props.cxx

src/Network/props.hxx

src/Network/protocol.cxx

src/Network/protocol.hxx

src/Network/pve.cxx

src/Network/pve.hxx

src/Network/raw_ctrls.hxx

src/Network/ray.cxx

src/Network/ray.hxx

src/Network/rul.cxx

src/Network/rul.hxx

src/NetworkOLK

src/NetworkOLK/Makefile.am

src/NetworkOLK/Makefile.in

src/NetworkOLK/README

src/NetworkOLK/fgd.h

src/NetworkOLK/net_hud.cxx

src/NetworkOLK/net_send.cxx

src/NetworkOLK/network.cxx

src/NetworkOLK/network.h

src/Objects

src/Objects/Makefile.am

src/Objects/Makefile.in

src/Objects/apt_signs.cxx

src/Objects/apt_signs.hxx

src/Objects/colours.h

src/Objects/matlib.cxx

src/Objects/matlib.hxx

src/Objects/newmat.cxx

src/Objects/newmat.hxx

src/Objects/obj.cxx

src/Objects/obj.hxx

src/Objects/texload.c

src/Objects/texload.h

src/Scenery

src/Scenery/FGTileLoader.cxx

src/Scenery/FGTileLoader.hxx

src/Scenery/Makefile.am

src/Scenery/Makefile.in

src/Scenery/hitlist.cxx

src/Scenery/hitlist.hxx

src/Scenery/newcache.cxx

src/Scenery/newcache.hxx

src/Scenery/scenery.cxx

src/Scenery/scenery.hxx

src/Scenery/tileentry.cxx

src/Scenery/tileentry.hxx

src/Scenery/tilemgr.cxx

src/Scenery/tilemgr.hxx

src/Sound

src/Sound/Makefile.am

src/Sound/Makefile.in

src/Sound/beacon.cxx

src/Sound/beacon.hxx

src/Sound/fg_fx.cxx

src/Sound/fg_fx.hxx

src/Sound/morse.cxx

src/Sound/morse.hxx

src/Sound/soundmgr.cxx

src/Sound/soundmgr.hxx

src/Time

src/Time/Makefile.am

src/Time/Makefile.in

src/Time/event.cxx

src/Time/event.hxx

src/Time/fg_timer.cxx

src/Time/fg_timer.hxx

src/Time/light.cxx

src/Time/light.hxx

src/Time/moonpos.cxx

src/Time/moonpos.hxx

src/Time/sunpos.cxx

src/Time/sunpos.hxx

src/Time/tmp.cxx

src/Time/tmp.hxx

src/Weather

src/Weather/Makefile.am

src/Weather/Makefile.in

src/Weather/weather.cxx

src/Weather/weather.hxx

src/WeatherCM

src/WeatherCM/FGAirPressureItem.cpp

src/WeatherCM/FGAirPressureItem.h

src/WeatherCM/FGCloud.h

src/WeatherCM/FGCloudItem.cpp

src/WeatherCM/FGCloudItem.h

src/WeatherCM/FGLocalWeatherDatabase.cpp

src/WeatherCM/FGLocalWeatherDatabase.h

src/WeatherCM/FGPhysicalProperties.cpp

src/WeatherCM/FGPhysicalProperties.h

src/WeatherCM/FGPhysicalProperty.cpp

src/WeatherCM/FGPhysicalProperty.h

src/WeatherCM/FGSnowRain.h

src/WeatherCM/FGTemperatureItem.cpp

src/WeatherCM/FGTemperatureItem.h

src/WeatherCM/FGThunderstorm.cpp

src/WeatherCM/FGThunderstorm.h

src/WeatherCM/FGTurbulenceItem.cpp

src/WeatherCM/FGTurbulenceItem.h

src/WeatherCM/FGVaporPressureItem.cpp

src/WeatherCM/FGVaporPressureItem.h

src/WeatherCM/FGWeatherDefs.h

src/WeatherCM/FGWeatherFeature.h

src/WeatherCM/FGWeatherParse.cpp

src/WeatherCM/FGWeatherParse.h

src/WeatherCM/FGWeatherUtils.h

src/WeatherCM/FGWeatherVectorWrap.h

src/WeatherCM/FGWindItem.cpp

src/WeatherCM/FGWindItem.h

src/WeatherCM/Makefile.am

src/WeatherCM/Makefile.in

src/WeatherCM/linintp2.h

src/WeatherCM/linintp2.inl

src/WeatherCM/sphrintp.h

src/WeatherCM/sphrintp.inl

tests

tests/Makefile.am

tests/Makefile.in

tests/est-epsilon.c

tests/gl-info.c

tests/test-gethostname.cxx

tests/test-mktime.cxx

tests/test-text.cxx

tests/test-up.cxx

Show diffs side-by-side

added added

removed removed

src/FDM/UIUCModel/uiuc_menu.cpp

/**********************************************************************

FILENAME: uiuc_menu.cpp

----------------------------------------------------------------------

DESCRIPTION: reads input file for specified aircraft and creates

approporiate data storage space

----------------------------------------------------------------------

STATUS: alpha version

----------------------------------------------------------------------

REFERENCES: based on "menu reader" format of Michael Selig

----------------------------------------------------------------------

HISTORY: 01/29/2000 initial release

02/18/2000 (JS) added 1D data file capability for

CL(a) and CD(a) -- calls

uiuc_1DdataFileReader

02/22/2000 (JS) added ice map functions

02/29/2000 (JS) added 2D data file capability for

CL(a,de), CD(a,de), Cm(a,de), CY(a,da),

CY(beta,dr), Cl(a,da), Cl(beta,dr),

Cn(a,da), Cn(beta,dr) -- calls

uiuc_2DdataFileReader

02/02/2000 (JS) added record options for 1D and

2D interpolated variables

03/28/2000 (JS) streamlined conversion factors for

file readers -- since they are global

variables, it is not necessary to put

them in the function calls

03/29/2000 (JS) added Cmfa and Weight flags;

added misc map; added Dx_cg (etc) to init

map

04/01/2000 (JS) added throttle, longitudinal, lateral,

and rudder inputs to record map

04/05/2000 (JS) added Altitude to init and record

maps; added zero_Long_trim to

controlSurface map

03/09/2001 (DPM) added support for gear.

06/18/2001 (RD) Added Alpha, Beta, U_body,

V_body, and W_body to init map. Added

aileron_input, rudder_input, pilot_elev_no,

pilot_ail_no, and pilot_rud_no to

controlSurface map. Added Throttle_pct_input

to engine map. Added CZfa to CL map.

07/05/2001 (RD) Changed pilot_elev_no = true to pilot_

elev_no_check=false. This is to allow pilot

to fly aircraft after input files have been

used.

08/27/2001 (RD) Added xxx_init_true and xxx_init for

P_body, Q_body, R_body, Phi, Theta, Psi,

U_body, V_body, and W_body to help in

starting the A/C at an initial condition.

----------------------------------------------------------------------

AUTHOR(S): Bipin Sehgal <bsehgal@uiuc.edu>

Jeff Scott <jscott@mail.com>

Robert Deters <rdeters@uiuc.edu>

Michael Selig <m-selig@uiuc.edu>

David Megginson <david@megginson.com>

----------------------------------------------------------------------

VARIABLES:

----------------------------------------------------------------------

INPUTS: n/a

----------------------------------------------------------------------

OUTPUTS: n/a

----------------------------------------------------------------------

CALLED BY: uiuc_wrapper.cpp

----------------------------------------------------------------------

CALLS TO: aircraft.dat

tabulated data files (if needed)

----------------------------------------------------------------------

This program is free software; you can redistribute it and/or

modify it under the terms of the GNU General Public License

as published by the Free Software Foundation.

This program is distributed in the hope that it will be useful,

but WITHOUT ANY WARRANTY; without even the implied warranty of

MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the

100

GNU General Public License for more details.

101

102

You should have received a copy of the GNU General Public License

103

along with this program; if not, write to the Free Software

104

Foundation, Inc., 59 Temple Place - Suite 330, Boston, MA 02111-1307,

105

USA or view http://www.gnu.org/copyleft/gpl.html.

106

107

**********************************************************************/

108

109

#include <simgear/compiler.h>

110

111

#if defined( __MWERKS__ )

112

// -dw- optimizer chokes (big-time) trying to optimize humongous

113

// loop/switch statements

114

#pragma optimization_level 0

115

#endif

116

117

#include <stdlib.h>

118

#include STL_IOSTREAM

119

120

#include "uiuc_menu.h"

121

122

#if !defined (SG_HAVE_NATIVE_SGI_COMPILERS)

123

SG_USING_STD(cerr);

124

SG_USING_STD(cout);

125

SG_USING_STD(endl);

126

127

# ifndef _MSC_VER

128

SG_USING_STD(exit);

129

# endif

130

#endif

131

132

bool check_float(string &token)

133

{

134

float value;

135

istrstream stream(token.c_str());

136

return (stream >> value);

137

}

138

139

140

void uiuc_menu( string aircraft_name )

141

{

142

stack command_list;

143

double token_value;

144

int token_value_recordRate;

145

int token_value_convert1, token_value_convert2, token_value_convert3;

146

147

string linetoken1;

148

string linetoken2;

149

string linetoken3;

150

string linetoken4;

151

string linetoken5;

152

string linetoken6;

153

154

155

/* the following default setting should eventually be moved to a default or uiuc_init routine */

156

157

recordRate = 1; /* record every time step, default */

158

recordStartTime = 0; /* record from beginning of simulation */

159

160

/* set speed at which dynamic pressure terms will be accounted for,

161

since if velocity is too small, coefficients will go to infinity */

162

dyn_on_speed = 33; /* 20 kts, default */

163

164

165

166

/* Read the file and get the list of commands */

167

airplane = new ParseFile(aircraft_name); /* struct that includes all lines of the input file */

168

command_list = airplane -> getCommands();

169

/* structs to include all parts included in the input file for specific keyword groups */

170

initParts = new ParseFile();

171

geometryParts = new ParseFile();

172

massParts = new ParseFile();

173

engineParts = new ParseFile();

174

aeroDragParts = new ParseFile();

175

aeroLiftParts = new ParseFile();

176

aeroPitchParts = new ParseFile();

177

aeroSideforceParts = new ParseFile();

178

aeroRollParts = new ParseFile();

179

aeroYawParts = new ParseFile();

180

gearParts = new ParseFile();

181

recordParts = new ParseFile();

182

183

if (command_list.begin() == command_list.end())

184

{

185

cerr << "UIUC ERROR: File " << aircraft_name <<" does not exist" << endl;

186

exit(-1);

187

}

188

189

for (LIST command_line = command_list.begin(); command_line!=command_list.end(); ++command_line)

190

{

191

cout << *command_line << endl;

192

193

linetoken1 = airplane -> getToken (*command_line, 1);

194

linetoken2 = airplane -> getToken (*command_line, 2);

195

linetoken3 = airplane -> getToken (*command_line, 3);

196

linetoken4 = airplane -> getToken (*command_line, 4);

197

linetoken5 = airplane -> getToken (*command_line, 5);

198

linetoken6 = airplane -> getToken (*command_line, 6);

199

200

istrstream token3(linetoken3.c_str());

201

istrstream token4(linetoken4.c_str());

202

istrstream token5(linetoken5.c_str());

203

istrstream token6(linetoken6.c_str());

204

205

switch (Keyword_map[linetoken1])

206

{

207

case init_flag:

208

{

209

switch(init_map[linetoken2])

210

{

211

case Dx_pilot_flag:

212

{

213

if (check_float(linetoken3))

214

token3 >> token_value;

215

else

216

uiuc_warnings_errors(1, *command_line);

217

218

Dx_pilot = token_value;

219

initParts -> storeCommands (*command_line);

220

break;

221

}

222

case Dy_pilot_flag:

223

{

224

if (check_float(linetoken3))

225

token3 >> token_value;

226

else

227

uiuc_warnings_errors(1, *command_line);

228

229

Dy_pilot = token_value;

230

initParts -> storeCommands (*command_line);

231

break;

232

}

233

case Dz_pilot_flag:

234

{

235

if (check_float(linetoken3))

236

token3 >> token_value;

237

else

238

uiuc_warnings_errors(1, *command_line);

239

240

Dz_pilot = token_value;

241

initParts -> storeCommands (*command_line);

242

break;

243

}

244

case Dx_cg_flag:

245

{

246

if (check_float(linetoken3))

247

token3 >> token_value;

248

else

249

uiuc_warnings_errors(1, *command_line);

250

251

Dx_cg = token_value;

252

initParts -> storeCommands (*command_line);

253

break;

254

}

255

case Dy_cg_flag:

256

{

257

if (check_float(linetoken3))

258

token3 >> token_value;

259

else

260

uiuc_warnings_errors(1, *command_line);

261

262

Dy_cg = token_value;

263

initParts -> storeCommands (*command_line);

264

break;

265

}

266

case Dz_cg_flag:

267

{

268

if (check_float(linetoken3))

269

token3 >> token_value;

270

else

271

uiuc_warnings_errors(1, *command_line);

272

273

Dz_cg = token_value;

274

initParts -> storeCommands (*command_line);

275

break;

276

}

277

case Altitude_flag:

278

{

279

if (check_float(linetoken3))

280

token3 >> token_value;

281

else

282

uiuc_warnings_errors(1, *command_line);

283

284

Altitude = token_value;

285

initParts -> storeCommands (*command_line);

286

break;

287

}

288

case V_north_flag:

289

{

290

if (check_float(linetoken3))

291

token3 >> token_value;

292

else

293

uiuc_warnings_errors(1, *command_line);

294

295

V_north = token_value;

296

initParts -> storeCommands (*command_line);

297

break;

298

}

299

case V_east_flag:

300

{

301

initParts -> storeCommands (*command_line);

302

if (check_float(linetoken3))

303

token3 >> token_value;

304

else

305

uiuc_warnings_errors(1, *command_line);

306

307

V_east = token_value;

308

break;

309

}

310

case V_down_flag:

311

{

312

if (check_float(linetoken3))

313

token3 >> token_value;

314

else

315

uiuc_warnings_errors(1, *command_line);

316

317

V_down = token_value;

318

initParts -> storeCommands (*command_line);

319

break;

320

}

321

case P_body_flag:

322

{

323

if (check_float(linetoken3))

324

token3 >> token_value;

325

else

326

uiuc_warnings_errors(1, *command_line);

327

328

P_body_init_true = true;

329

P_body_init = token_value;

330

initParts -> storeCommands (*command_line);

331

break;

332

}

333

case Q_body_flag:

334

{

335

if (check_float(linetoken3))

336

token3 >> token_value;

337

else

338

uiuc_warnings_errors(1, *command_line);

339

340

Q_body_init_true = true;

341

Q_body_init = token_value;

342

initParts -> storeCommands (*command_line);

343

break;

344

}

345

case R_body_flag:

346

{

347

if (check_float(linetoken3))

348

token3 >> token_value;

349

else

350

uiuc_warnings_errors(1, *command_line);

351

352

R_body_init_true = true;

353

R_body_init = token_value;

354

initParts -> storeCommands (*command_line);

355

break;

356

}

357

case Phi_flag:

358

{

359

if (check_float(linetoken3))

360

token3 >> token_value;

361

else

362

uiuc_warnings_errors(1, *command_line);

363

364

Phi_init_true = true;

365

Phi_init = token_value;

366

initParts -> storeCommands (*command_line);

367

break;

368

}

369

case Theta_flag:

370

{

371

if (check_float(linetoken3))

372

token3 >> token_value;

373

else

374

uiuc_warnings_errors(1, *command_line);

375

376

Theta_init_true = true;

377

Theta_init = token_value;

378

initParts -> storeCommands (*command_line);

379

break;

380

}

381

case Psi_flag:

382

{

383

if (check_float(linetoken3))

384

token3 >> token_value;

385

else

386

uiuc_warnings_errors(1, *command_line);

387

388

Psi_init_true = true;

389

Psi_init = token_value;

390

initParts -> storeCommands (*command_line);

391

break;

392

}

393

case Long_trim_flag:

394

{

395

if (check_float(linetoken3))

396

token3 >> token_value;

397

else

398

uiuc_warnings_errors(1, *command_line);

399

400

Long_trim = token_value;

401

initParts -> storeCommands (*command_line);

402

break;

403

}

404

case recordRate_flag:

405

{

406

//can't use check_float since variable is integer

407

token3 >> token_value_recordRate;

408

recordRate = 120 / token_value_recordRate;

409

break;

410

}

411

case recordStartTime_flag:

412

{

413

if (check_float(linetoken3))

414

token3 >> token_value;

415

else

416

uiuc_warnings_errors(1, *command_line);

417

418

recordStartTime = token_value;

419

break;

420

}

421

case nondim_rate_V_rel_wind_flag:

422

{

423

nondim_rate_V_rel_wind = true;

424

break;

425

}

426

case dyn_on_speed_flag:

427

{

428

if (check_float(linetoken3))

429

token3 >> token_value;

430

else

431

uiuc_warnings_errors(1, *command_line);

432

433

dyn_on_speed = token_value;

434

break;

435

}

436

case Alpha_flag:

437

{

438

if (check_float(linetoken3))

439

token3 >> token_value;

440

else

441

uiuc_warnings_errors(1, *command_line);

442

443

Alpha_init_true = true;

444

Alpha_init = token_value * DEG_TO_RAD;

445

break;

446

}

447

case Beta_flag:

448

{

449

if (check_float(linetoken3))

450

token3 >> token_value;

451

else

452

uiuc_warnings_errors(1, *command_line);

453

454

Beta_init_true = true;

455

Beta_init = token_value * DEG_TO_RAD;

456

break;

457

}

458

case U_body_flag:

459

{

460

if (check_float(linetoken3))

461

token3 >> token_value;

462

else

463

uiuc_warnings_errors(1, *command_line);

464

465

U_body_init_true = true;

466

U_body_init = token_value;

467

break;

468

}

469

case V_body_flag:

470

{

471

if (check_float(linetoken3))

472

token3 >> token_value;

473

else

474

uiuc_warnings_errors(1, *command_line);

475

476

V_body_init_true = true;

477

V_body_init = token_value;

478

break;

479

}

480

case W_body_flag:

481

{

482

if (check_float(linetoken3))

483

token3 >> token_value;

484

else

485

uiuc_warnings_errors(1, *command_line);

486

487

W_body_init_true = true;

488

W_body_init = token_value;

489

break;

490

}

491

default:

492

{

493

uiuc_warnings_errors(2, *command_line);

494

break;

495

}

496

};

497

break;

498

} // end init map

499

500

501

case geometry_flag:

502

{

503

switch(geometry_map[linetoken2])

504

{

505

case bw_flag:

506

{

507

if (check_float(linetoken3))

508

token3 >> token_value;

509

else

510

uiuc_warnings_errors(1, *command_line);

511

512

bw = token_value;

513

geometryParts -> storeCommands (*command_line);

514

break;

515

}

516

case cbar_flag:

517

{

518

if (check_float(linetoken3))

519

token3 >> token_value;

520

else

521

uiuc_warnings_errors(1, *command_line);

522

523

cbar = token_value;

524

geometryParts -> storeCommands (*command_line);

525

break;

526

}

527

case Sw_flag:

528

{

529

if (check_float(linetoken3))

530

token3 >> token_value;

531

else

532

uiuc_warnings_errors(1, *command_line);

533

534

Sw = token_value;

535

geometryParts -> storeCommands (*command_line);

536

break;

537

}

538

case ih_flag:

539

{

540

if (check_float(linetoken3))

541

token3 >> token_value;

542

else

543

uiuc_warnings_errors(1, *command_line);

544

545

ih = token_value;

546

geometryParts -> storeCommands (*command_line);

547

break;

548

}

549

case bh_flag:

550

{

551

if (check_float(linetoken3))

552

token3 >> token_value;

553

else

554

uiuc_warnings_errors(1, *command_line);

555

556

bh = token_value;

557

geometryParts -> storeCommands (*command_line);

558

break;

559

}

560

case ch_flag:

561

{

562

if (check_float(linetoken3))

563

token3 >> token_value;

564

else

565

uiuc_warnings_errors(1, *command_line);

566

567

ch = token_value;

568

geometryParts -> storeCommands (*command_line);

569

break;

570

}

571

case Sh_flag:

572

{

573

if (check_float(linetoken3))

574

token3 >> token_value;

575

else

576

uiuc_warnings_errors(1, *command_line);

577

578

Sh = token_value;

579

geometryParts -> storeCommands (*command_line);

580

break;

581

}

582

default:

583

{

584

uiuc_warnings_errors(2, *command_line);

585

break;

586

}

587

};

588

break;

589

} // end geometry map

590

591

592

case controlSurface_flag:

593

{

594

switch(controlSurface_map[linetoken2])

595

{

596

case de_flag:

597

{

598

if (check_float(linetoken3))

599

token3 >> token_value;

600

else

601

uiuc_warnings_errors(1, *command_line);

602

603

demax = token_value;

604

605

if (check_float(linetoken4))

606

token4 >> token_value;

607

else

608

uiuc_warnings_errors(1, *command_line);

609

610

demin = token_value;

611

break;

612

}

613

case da_flag:

614

{

615

if (check_float(linetoken3))

616

token3 >> token_value;

617

else

618

uiuc_warnings_errors(1, *command_line);

619

620

damax = token_value;

621

622

if (check_float(linetoken4))

623

token4 >> token_value;

624

else

625

uiuc_warnings_errors(1, *command_line);

626

627

damin = token_value;

628

break;

629

}

630

case dr_flag:

631

{

632

if (check_float(linetoken3))

633

token3 >> token_value;

634

else

635

uiuc_warnings_errors(1, *command_line);

636

637

drmax = token_value;

638

639

if (check_float(linetoken4))

640

token4 >> token_value;

641

else

642

uiuc_warnings_errors(1, *command_line);

643

644

drmin = token_value;

645

break;

646

}

647

case set_Long_trim_flag:

648

{

649

if (check_float(linetoken3))

650

token3 >> token_value;

651

else

652

uiuc_warnings_errors(1, *command_line);

653

654

set_Long_trim = true;

655

elevator_tab = token_value;

656

break;

657

}

658

case set_Long_trim_deg_flag:

659

{

660

if (check_float(linetoken3))

661

token3 >> token_value;

662

else

663

uiuc_warnings_errors(1, *command_line);

664

665

set_Long_trim = true;

666

elevator_tab = token_value * DEG_TO_RAD;

667

break;

668

}

669

case zero_Long_trim_flag:

670

{

671

zero_Long_trim = true;

672

break;

673

}

674

case elevator_step_flag:

675

{

676

// set step input flag

677

elevator_step = true;

678

679

// read in step angle in degrees and convert

680

if (check_float(linetoken3))

681

token3 >> token_value;

682

else

683

uiuc_warnings_errors(1, *command_line);

684

685

elevator_step_angle = token_value * DEG_TO_RAD;

686

687

// read in step start time

688

if (check_float(linetoken4))

689

token4 >> token_value;

690

else

691

uiuc_warnings_errors(1, *command_line);

692

693

elevator_step_startTime = token_value;

694

break;

695

}

696

case elevator_singlet_flag:

697

{

698

// set singlet input flag

699

elevator_singlet = true;

700

701

// read in singlet angle in degrees and convert

702

if (check_float(linetoken3))

703

token3 >> token_value;

704

else

705

uiuc_warnings_errors(1, *command_line);

706

707

elevator_singlet_angle = token_value * DEG_TO_RAD;

708

709

// read in singlet start time

710

if (check_float(linetoken4))

711

token4 >> token_value;

712

else

713

uiuc_warnings_errors(1, *command_line);

714

715

elevator_singlet_startTime = token_value;

716

717

// read in singlet duration

718

if (check_float(linetoken5))

719

token5 >> token_value;

720

else

721

uiuc_warnings_errors(1, *command_line);

722

723

elevator_singlet_duration = token_value;

724

break;

725

}

726

case elevator_doublet_flag:

727

{

728

// set doublet input flag

729

elevator_doublet = true;

730

731

// read in doublet angle in degrees and convert

732

if (check_float(linetoken3))

733

token3 >> token_value;

734

else

735

uiuc_warnings_errors(1, *command_line);

736

737

elevator_doublet_angle = token_value * DEG_TO_RAD;

738

739

// read in doublet start time

740

if (check_float(linetoken4))

741

token4 >> token_value;

742

else

743

uiuc_warnings_errors(1, *command_line);

744

745

elevator_doublet_startTime = token_value;

746

747

// read in doublet duration

748

if (check_float(linetoken5))

749

token5 >> token_value;

750

else

751

uiuc_warnings_errors(1, *command_line);

752

753

elevator_doublet_duration = token_value;

754

break;

755

}

756

case elevator_input_flag:

757

{

758

elevator_input = true;

759

elevator_input_file = linetoken3;

760

token4 >> token_value_convert1;

761

token5 >> token_value_convert2;

762

convert_y = uiuc_convert(token_value_convert1);

763

convert_x = uiuc_convert(token_value_convert2);

764

uiuc_1DdataFileReader(elevator_input_file,

765

elevator_input_timeArray,

766

elevator_input_deArray,

767

elevator_input_ntime);

768

token6 >> token_value;

769

elevator_input_startTime = token_value;

770

break;

771

}

772

case aileron_input_flag:

773

{

774

aileron_input = true;

775

aileron_input_file = linetoken3;

776

token4 >> token_value_convert1;

777

token5 >> token_value_convert2;

778

convert_y = uiuc_convert(token_value_convert1);

779

convert_x = uiuc_convert(token_value_convert2);

780

uiuc_1DdataFileReader(aileron_input_file,

781

aileron_input_timeArray,

782

aileron_input_daArray,

783

aileron_input_ntime);

784

token6 >> token_value;

785

aileron_input_startTime = token_value;

786

break;

787

}

788

case rudder_input_flag:

789

{

790

rudder_input = true;

791

rudder_input_file = linetoken3;

792

token4 >> token_value_convert1;

793

token5 >> token_value_convert2;

794

convert_y = uiuc_convert(token_value_convert1);

795

convert_x = uiuc_convert(token_value_convert2);

796

uiuc_1DdataFileReader(rudder_input_file,

797

rudder_input_timeArray,

798

rudder_input_drArray,

799

rudder_input_ntime);

800

token6 >> token_value;

801

rudder_input_startTime = token_value;

802

break;

803

}

804

case pilot_elev_no_flag:

805

{

806

pilot_elev_no_check = true;

807

break;

808

}

809

case pilot_ail_no_flag:

810

{

811

pilot_ail_no_check = true;

812

break;

813

}

814

case pilot_rud_no_flag:

815

{

816

pilot_rud_no_check = true;

817

break;

818

}

819

default:

820

{

821

uiuc_warnings_errors(2, *command_line);

822

break;

823

}

824

};

825

break;

826

} // end controlSurface map

827

828

829

case mass_flag:

830

{

831

switch(mass_map[linetoken2])

832

{

833

case Weight_flag:

834

{

835

if (check_float(linetoken3))

836

token3 >> token_value;

837

else

838

uiuc_warnings_errors(1, *command_line);

839

840

Weight = token_value;

841

Mass = Weight * INVG;

842

massParts -> storeCommands (*command_line);

843

break;

844

}

845

case Mass_flag:

846

{

847

if (check_float(linetoken3))

848

token3 >> token_value;

849

else

850

uiuc_warnings_errors(1, *command_line);

851

852

Mass = token_value;

853

massParts -> storeCommands (*command_line);

854

break;

855

}

856

case I_xx_flag:

857

{

858

if (check_float(linetoken3))

859

token3 >> token_value;

860

else

861

uiuc_warnings_errors(1, *command_line);

862

863

I_xx = token_value;

864

massParts -> storeCommands (*command_line);

865

break;

866

}

867

case I_yy_flag:

868

{

869

if (check_float(linetoken3))

870

token3 >> token_value;

871

else

872

uiuc_warnings_errors(1, *command_line);

873

874

I_yy = token_value;

875

massParts -> storeCommands (*command_line);

876

break;

877

}

878

case I_zz_flag:

879

{

880

if (check_float(linetoken3))

881

token3 >> token_value;

882

else

883

uiuc_warnings_errors(1, *command_line);

884

885

I_zz = token_value;

886

massParts -> storeCommands (*command_line);

887

break;

888

}

889

case I_xz_flag:

890

{

891

if (check_float(linetoken3))

892

token3 >> token_value;

893

else

894

uiuc_warnings_errors(1, *command_line);

895

896

I_xz = token_value;

897

massParts -> storeCommands (*command_line);

898

break;

899

}

900

default:

901

{

902

uiuc_warnings_errors(2, *command_line);

903

break;

904

}

905

};

906

break;

907

} // end mass map

908

909

910

case engine_flag:

911

{

912

switch(engine_map[linetoken2])

913

{

914

case simpleSingle_flag:

915

{

916

if (check_float(linetoken3))

917

token3 >> token_value;

918

else

919

uiuc_warnings_errors(1, *command_line);

920

921

simpleSingleMaxThrust = token_value;

922

engineParts -> storeCommands (*command_line);

923

break;

924

}

925

case c172_flag:

926

{

927

engineParts -> storeCommands (*command_line);

928

break;

929

}

930

case cherokee_flag:

931

{

932

engineParts -> storeCommands (*command_line);

933

break;

934

}

935

case Throttle_pct_input_flag:

936

{

937

Throttle_pct_input = true;

938

Throttle_pct_input_file = linetoken3;

939

token4 >> token_value_convert1;

940

token5 >> token_value_convert2;

941

convert_y = uiuc_convert(token_value_convert1);

942

convert_x = uiuc_convert(token_value_convert2);

943

uiuc_1DdataFileReader(Throttle_pct_input_file,

944

Throttle_pct_input_timeArray,

945

Throttle_pct_input_dTArray,

946

Throttle_pct_input_ntime);

947

token6 >> token_value;

948

Throttle_pct_input_startTime = token_value;

949

break;

950

}

951

default:

952

{

953

uiuc_warnings_errors(2, *command_line);

954

break;

955

}

956

};

957

break;

958

} // end engine map

959

960

961

case CD_flag:

962

{

963

switch(CD_map[linetoken2])

964

{

965

case CDo_flag:

966

{

967

if (check_float(linetoken3))

968

token3 >> token_value;

969

else

970

uiuc_warnings_errors(1, *command_line);

971

972

CDo = token_value;

973

CDo_clean = CDo;

974

aeroDragParts -> storeCommands (*command_line);

975

break;

976

}

977

case CDK_flag:

978

{

979

if (check_float(linetoken3))

980

token3 >> token_value;

981

else

982

uiuc_warnings_errors(1, *command_line);

983

984

CDK = token_value;

985

CDK_clean = CDK;

986

aeroDragParts -> storeCommands (*command_line);

987

break;

988

}

989

case CD_a_flag:

990

{

991

if (check_float(linetoken3))

992

token3 >> token_value;

993

else

994

uiuc_warnings_errors(1, *command_line);

995

996

CD_a = token_value;

997

CD_a_clean = CD_a;

998

aeroDragParts -> storeCommands (*command_line);

999

break;

1000

}

1001

case CD_adot_flag:

1002

{

1003

if (check_float(linetoken3))

1004

token3 >> token_value;

1005

else

1006

uiuc_warnings_errors(1, *command_line);

1007

1008

CD_adot = token_value;

1009

CD_adot_clean = CD_adot;

1010

aeroDragParts -> storeCommands (*command_line);

1011

break;

1012

}

1013

case CD_q_flag:

1014

{

1015

if (check_float(linetoken3))

1016

token3 >> token_value;

1017

else

1018

uiuc_warnings_errors(1, *command_line);

1019

1020

CD_q = token_value;

1021

CD_q_clean = CD_q;

1022

aeroDragParts -> storeCommands (*command_line);

1023

break;

1024

}

1025

case CD_ih_flag:

1026

{

1027

if (check_float(linetoken3))

1028

token3 >> token_value;

1029

else

1030

uiuc_warnings_errors(1, *command_line);

1031

1032

CD_ih = token_value;

1033

aeroDragParts -> storeCommands (*command_line);

1034

break;

1035

}

1036

case CD_de_flag:

1037

{

1038

if (check_float(linetoken3))

1039

token3 >> token_value;

1040

else

1041

uiuc_warnings_errors(1, *command_line);

1042

1043

CD_de = token_value;

1044

CD_de_clean = CD_de;

1045

aeroDragParts -> storeCommands (*command_line);

1046

break;

1047

}

1048

case CDfa_flag:

1049

{

1050

CDfa = linetoken3;

1051

token4 >> token_value_convert1;

1052

token5 >> token_value_convert2;

1053

convert_y = uiuc_convert(token_value_convert1);

1054

convert_x = uiuc_convert(token_value_convert2);

1055

/* call 1D File Reader with file name (CDfa) and conversion

1056

factors; function returns array of alphas (aArray) and

1057

corresponding CD values (CDArray) and max number of

1058

terms in arrays (nAlpha) */

1059

uiuc_1DdataFileReader(CDfa,

1060

CDfa_aArray,

1061

CDfa_CDArray,

1062

CDfa_nAlpha);

1063

aeroDragParts -> storeCommands (*command_line);

1064

break;

1065

}

1066

case CDfCL_flag:

1067

{

1068

CDfCL = linetoken3;

1069

token4 >> token_value_convert1;

1070

token5 >> token_value_convert2;

1071

convert_y = uiuc_convert(token_value_convert1);

1072

convert_x = uiuc_convert(token_value_convert2);

1073

/* call 1D File Reader with file name (CDfCL) and conversion

1074

factors; function returns array of CLs (CLArray) and

1075

corresponding CD values (CDArray) and max number of

1076

terms in arrays (nCL) */

1077

uiuc_1DdataFileReader(CDfCL,

1078

CDfCL_CLArray,

1079

CDfCL_CDArray,

1080

CDfCL_nCL);

1081

aeroDragParts -> storeCommands (*command_line);

1082

break;

1083

}

1084

case CDfade_flag:

1085

{

1086

CDfade = linetoken3;

1087

token4 >> token_value_convert1;

1088

token5 >> token_value_convert2;

1089

token6 >> token_value_convert3;

1090

convert_z = uiuc_convert(token_value_convert1);

1091

convert_x = uiuc_convert(token_value_convert2);

1092

convert_y = uiuc_convert(token_value_convert3);

1093

/* call 2D File Reader with file name (CDfade) and

1094

conversion factors; function returns array of

1095

elevator deflections (deArray) and corresponding

1096

alpha (aArray) and delta CD (CDArray) values and

1097

max number of terms in alpha arrays (nAlphaArray)

1098

and deflection array (nde) */

1099

uiuc_2DdataFileReader(CDfade,

1100

CDfade_aArray,

1101

CDfade_deArray,

1102

CDfade_CDArray,

1103

CDfade_nAlphaArray,

1104

CDfade_nde);

1105

aeroDragParts -> storeCommands (*command_line);

1106

break;

1107

}

1108

case CDfdf_flag:

1109

{

1110

CDfdf = linetoken3;

1111

token4 >> token_value_convert1;

1112

token5 >> token_value_convert2;

1113

convert_y = uiuc_convert(token_value_convert1);

1114

convert_x = uiuc_convert(token_value_convert2);

1115

/* call 1D File Reader with file name (CDfdf) and conversion

1116

factors; function returns array of dfs (dfArray) and

1117

corresponding CD values (CDArray) and max number of

1118

terms in arrays (ndf) */

1119

uiuc_1DdataFileReader(CDfdf,

1120

CDfdf_dfArray,

1121

CDfdf_CDArray,

1122

CDfdf_ndf);

1123

aeroDragParts -> storeCommands (*command_line);

1124

break;

1125

}

1126

case CDfadf_flag:

1127

{

1128

CDfadf = linetoken3;

1129

token4 >> token_value_convert1;

1130

token5 >> token_value_convert2;

1131

token6 >> token_value_convert3;

1132

convert_z = uiuc_convert(token_value_convert1);

1133

convert_x = uiuc_convert(token_value_convert2);

1134

convert_y = uiuc_convert(token_value_convert3);

1135

/* call 2D File Reader with file name (CDfadf) and

1136

conversion factors; function returns array of

1137

flap deflections (dfArray) and corresponding

1138

alpha (aArray) and delta CD (CDArray) values and

1139

max number of terms in alpha arrays (nAlphaArray)

1140

and deflection array (ndf) */

1141

uiuc_2DdataFileReader(CDfadf,

1142

CDfadf_aArray,

1143

CDfadf_dfArray,

1144

CDfadf_CDArray,

1145

CDfadf_nAlphaArray,

1146

CDfadf_ndf);

1147

aeroDragParts -> storeCommands (*command_line);

1148

break;

1149

}

1150

case CXo_flag:

1151

{

1152

if (check_float(linetoken3))

1153

token3 >> token_value;

1154

else

1155

uiuc_warnings_errors(1, *command_line);

1156

1157

CXo = token_value;

1158

CXo_clean = CXo;

1159

aeroDragParts -> storeCommands (*command_line);

1160

break;

1161

}

1162

case CXK_flag:

1163

{

1164

if (check_float(linetoken3))

1165

token3 >> token_value;

1166

else

1167

uiuc_warnings_errors(1, *command_line);

1168

1169

CXK = token_value;

1170

CXK_clean = CXK;

1171

aeroDragParts -> storeCommands (*command_line);

1172

break;

1173

}

1174

case CX_a_flag:

1175

{

1176

if (check_float(linetoken3))

1177

token3 >> token_value;

1178

else

1179

uiuc_warnings_errors(1, *command_line);

1180

1181

CX_a = token_value;

1182

CX_a_clean = CX_a;

1183

aeroDragParts -> storeCommands (*command_line);

1184

break;

1185

}

1186

case CX_a2_flag:

1187

{

1188

if (check_float(linetoken3))

1189

token3 >> token_value;

1190

else

1191

uiuc_warnings_errors(1, *command_line);

1192

1193

CX_a2 = token_value;

1194

CX_a2_clean = CX_a2;

1195

aeroDragParts -> storeCommands (*command_line);

1196

break;

1197

}

1198

case CX_a3_flag:

1199

{

1200

if (check_float(linetoken3))

1201

token3 >> token_value;

1202

else

1203

uiuc_warnings_errors(1, *command_line);

1204

1205

CX_a3 = token_value;

1206

CX_a3_clean = CX_a3;

1207

aeroDragParts -> storeCommands (*command_line);

1208

break;

1209

}

1210

case CX_adot_flag:

1211

{

1212

if (check_float(linetoken3))

1213

token3 >> token_value;

1214

else

1215

uiuc_warnings_errors(1, *command_line);

1216

1217

CX_adot = token_value;

1218

CX_adot_clean = CX_adot;

1219

aeroDragParts -> storeCommands (*command_line);

1220

break;

1221

}

1222

case CX_q_flag:

1223

{

1224

if (check_float(linetoken3))

1225

token3 >> token_value;

1226

else

1227

uiuc_warnings_errors(1, *command_line);

1228

1229

CX_q = token_value;

1230

CX_q_clean = CX_q;

1231

aeroDragParts -> storeCommands (*command_line);

1232

break;

1233

}

1234

case CX_de_flag:

1235

{

1236

if (check_float(linetoken3))

1237

token3 >> token_value;

1238

else

1239

uiuc_warnings_errors(1, *command_line);

1240

1241

CX_de = token_value;

1242

CX_de_clean = CX_de;

1243

aeroDragParts -> storeCommands (*command_line);

1244

break;

1245

}

1246

case CX_dr_flag:

1247

{

1248

if (check_float(linetoken3))

1249

token3 >> token_value;

1250

else

1251

uiuc_warnings_errors(1, *command_line);

1252

1253

CX_dr = token_value;

1254

CX_dr_clean = CX_dr;

1255

aeroDragParts -> storeCommands (*command_line);

1256

break;

1257

}

1258

case CX_df_flag:

1259

{

1260

if (check_float(linetoken3))

1261

token3 >> token_value;

1262

else

1263

uiuc_warnings_errors(1, *command_line);

1264

1265

CX_df = token_value;

1266

CX_df_clean = CX_df;

1267

aeroDragParts -> storeCommands (*command_line);

1268

break;

1269

}

1270

case CX_adf_flag:

1271

{

1272

if (check_float(linetoken3))

1273

token3 >> token_value;

1274

else

1275

uiuc_warnings_errors(1, *command_line);

1276

1277

CX_adf = token_value;

1278

CX_adf_clean = CX_adf;

1279

aeroDragParts -> storeCommands (*command_line);

1280

break;

1281

}

1282

default:

1283

{

1284

uiuc_warnings_errors(2, *command_line);

1285

break;

1286

}

1287

};

1288

break;

1289

} // end CD map

1290

1291

1292

case CL_flag:

1293

{

1294

switch(CL_map[linetoken2])

1295

{

1296

case CLo_flag:

1297

{

1298

if (check_float(linetoken3))

1299

token3 >> token_value;

1300

else

1301

uiuc_warnings_errors(1, *command_line);

1302

1303

CLo = token_value;

1304

CLo_clean = CLo;

1305

aeroLiftParts -> storeCommands (*command_line);

1306

break;

1307

}

1308

case CL_a_flag:

1309

{

1310

if (check_float(linetoken3))

1311

token3 >> token_value;

1312

else

1313

uiuc_warnings_errors(1, *command_line);

1314

1315

CL_a = token_value;

1316

CL_a_clean = CL_a;

1317

aeroLiftParts -> storeCommands (*command_line);

1318

break;

1319

}

1320

case CL_adot_flag:

1321

{

1322

if (check_float(linetoken3))

1323

token3 >> token_value;

1324

else

1325

uiuc_warnings_errors(1, *command_line);

1326

1327

CL_adot = token_value;

1328

CL_adot_clean = CL_adot;

1329

aeroLiftParts -> storeCommands (*command_line);

1330

break;

1331

}

1332

case CL_q_flag:

1333

{

1334

if (check_float(linetoken3))

1335

token3 >> token_value;

1336

else

1337

uiuc_warnings_errors(1, *command_line);

1338

1339

CL_q = token_value;

1340

CL_q_clean = CL_q;

1341

aeroLiftParts -> storeCommands (*command_line);

1342

break;

1343

}

1344

case CL_ih_flag:

1345

{

1346

if (check_float(linetoken3))

1347

token3 >> token_value;

1348

else

1349

uiuc_warnings_errors(1, *command_line);

1350

1351

CL_ih = token_value;

1352

aeroLiftParts -> storeCommands (*command_line);

1353

break;

1354

}

1355

case CL_de_flag:

1356

{

1357

if (check_float(linetoken3))

1358

token3 >> token_value;

1359

else

1360

uiuc_warnings_errors(1, *command_line);

1361

1362

CL_de = token_value;

1363

CL_de_clean = CL_de;

1364

aeroLiftParts -> storeCommands (*command_line);

1365

break;

1366

}

1367

case CLfa_flag:

1368

{

1369

CLfa = linetoken3;

1370

token4 >> token_value_convert1;

1371

token5 >> token_value_convert2;

1372

convert_y = uiuc_convert(token_value_convert1);

1373

convert_x = uiuc_convert(token_value_convert2);

1374

/* call 1D File Reader with file name (CLfa) and conversion

1375

factors; function returns array of alphas (aArray) and

1376

corresponding CL values (CLArray) and max number of

1377

terms in arrays (nAlpha) */

1378

uiuc_1DdataFileReader(CLfa,

1379

CLfa_aArray,

1380

CLfa_CLArray,

1381

CLfa_nAlpha);

1382

aeroLiftParts -> storeCommands (*command_line);

1383

break;

1384

}

1385

case CLfade_flag:

1386

{

1387

CLfade = linetoken3;

1388

token4 >> token_value_convert1;

1389

token5 >> token_value_convert2;

1390

token6 >> token_value_convert3;

1391

convert_z = uiuc_convert(token_value_convert1);

1392

convert_x = uiuc_convert(token_value_convert2);

1393

convert_y = uiuc_convert(token_value_convert3);

1394

/* call 2D File Reader with file name (CLfade) and

1395

conversion factors; function returns array of

1396

elevator deflections (deArray) and corresponding

1397

alpha (aArray) and delta CL (CLArray) values and

1398

max number of terms in alpha arrays (nAlphaArray)

1399

and deflection array (nde) */

1400

uiuc_2DdataFileReader(CLfade,

1401

CLfade_aArray,

1402

CLfade_deArray,

1403

CLfade_CLArray,

1404

CLfade_nAlphaArray,

1405

CLfade_nde);

1406

aeroLiftParts -> storeCommands (*command_line);

1407

break;

1408

}

1409

case CLfdf_flag:

1410

{

1411

CLfdf = linetoken3;

1412

token4 >> token_value_convert1;

1413

token5 >> token_value_convert2;

1414

convert_y = uiuc_convert(token_value_convert1);

1415

convert_x = uiuc_convert(token_value_convert2);

1416

/* call 1D File Reader with file name (CLfdf) and conversion

1417

factors; function returns array of dfs (dfArray) and

1418

corresponding CL values (CLArray) and max number of

1419

terms in arrays (ndf) */

1420

uiuc_1DdataFileReader(CLfdf,

1421

CLfdf_dfArray,

1422

CLfdf_CLArray,

1423

CLfdf_ndf);

1424

aeroLiftParts -> storeCommands (*command_line);

1425

1426

// additional variables to streamline flap routine in aerodeflections

1427

ndf = CLfdf_ndf;

1428

int temp_counter = 1;

1429

while (temp_counter <= ndf)

1430

{

1431

dfArray[temp_counter] = CLfdf_dfArray[temp_counter];

1432

TimeArray[temp_counter] = dfTimefdf_TimeArray[temp_counter];

1433

temp_counter++;

1434

}

1435

break;

1436

}

1437

case CLfadf_flag:

1438

{

1439

CLfadf = linetoken3;

1440

token4 >> token_value_convert1;

1441

token5 >> token_value_convert2;

1442

token6 >> token_value_convert3;

1443

convert_z = uiuc_convert(token_value_convert1);

1444

convert_x = uiuc_convert(token_value_convert2);

1445

convert_y = uiuc_convert(token_value_convert3);

1446

/* call 2D File Reader with file name (CLfadf) and

1447

conversion factors; function returns array of

1448

flap deflections (dfArray) and corresponding

1449

alpha (aArray) and delta CL (CLArray) values and

1450

max number of terms in alpha arrays (nAlphaArray)

1451

and deflection array (ndf) */

1452

uiuc_2DdataFileReader(CLfadf,

1453

CLfadf_aArray,

1454

CLfadf_dfArray,

1455

CLfadf_CLArray,

1456

CLfadf_nAlphaArray,

1457

CLfadf_ndf);

1458

aeroLiftParts -> storeCommands (*command_line);

1459

break;

1460

}

1461

case CZo_flag:

1462

{

1463

if (check_float(linetoken3))

1464

token3 >> token_value;

1465

else

1466

uiuc_warnings_errors(1, *command_line);

1467

1468

CZo = token_value;

1469

CZo_clean = CZo;

1470

aeroLiftParts -> storeCommands (*command_line);

1471

break;

1472

}

1473

case CZ_a_flag:

1474

{

1475

if (check_float(linetoken3))

1476

token3 >> token_value;

1477

else

1478

uiuc_warnings_errors(1, *command_line);

1479

1480

CZ_a = token_value;

1481

CZ_a_clean = CZ_a;

1482

aeroLiftParts -> storeCommands (*command_line);

1483

break;

1484

}

1485

case CZ_a2_flag:

1486

{

1487

if (check_float(linetoken3))

1488

token3 >> token_value;

1489

else

1490

uiuc_warnings_errors(1, *command_line);

1491

1492

CZ_a2 = token_value;

1493

CZ_a2_clean = CZ_a2;

1494

aeroLiftParts -> storeCommands (*command_line);

1495

break;

1496

}

1497

case CZ_a3_flag:

1498

{

1499

if (check_float(linetoken3))

1500

token3 >> token_value;

1501

else

1502

uiuc_warnings_errors(1, *command_line);

1503

1504

CZ_a3 = token_value;

1505

CZ_a3_clean = CZ_a3;

1506

aeroLiftParts -> storeCommands (*command_line);

1507

break;

1508

}

1509

case CZ_adot_flag:

1510

{

1511

if (check_float(linetoken3))

1512

token3 >> token_value;

1513

else

1514

uiuc_warnings_errors(1, *command_line);

1515

1516

CZ_adot = token_value;

1517

CZ_adot_clean = CZ_adot;

1518

aeroLiftParts -> storeCommands (*command_line);

1519

break;

1520

}

1521

case CZ_q_flag:

1522

{

1523

if (check_float(linetoken3))

1524

token3 >> token_value;

1525

else

1526

uiuc_warnings_errors(1, *command_line);

1527

1528

CZ_q = token_value;

1529

CZ_q_clean = CZ_q;

1530

aeroLiftParts -> storeCommands (*command_line);

1531

break;

1532

}

1533

case CZ_de_flag:

1534

{

1535

if (check_float(linetoken3))

1536

token3 >> token_value;

1537

else

1538

uiuc_warnings_errors(1, *command_line);

1539

1540

CZ_de = token_value;

1541

CZ_de_clean = CZ_de;

1542

aeroLiftParts -> storeCommands (*command_line);

1543

break;

1544

}

1545

case CZ_deb2_flag:

1546

{

1547

if (check_float(linetoken3))

1548

token3 >> token_value;

1549

else

1550

uiuc_warnings_errors(1, *command_line);

1551

1552

CZ_deb2 = token_value;

1553

CZ_deb2_clean = CZ_deb2;

1554

aeroLiftParts -> storeCommands (*command_line);

1555

break;

1556

}

1557

case CZ_df_flag:

1558

{

1559

if (check_float(linetoken3))

1560

token3 >> token_value;

1561

else

1562

uiuc_warnings_errors(1, *command_line);

1563

1564

CZ_df = token_value;

1565

CZ_df_clean = CZ_df;

1566

aeroLiftParts -> storeCommands (*command_line);

1567

break;

1568

}

1569

case CZ_adf_flag:

1570

{

1571

if (check_float(linetoken3))

1572

token3 >> token_value;

1573

else

1574

uiuc_warnings_errors(1, *command_line);

1575

1576

CZ_adf = token_value;

1577

CZ_adf_clean = CZ_adf;

1578

aeroLiftParts -> storeCommands (*command_line);

1579

break;

1580

}

1581

case CZfa_flag:

1582

{

1583

CZfa = linetoken3;

1584

token4 >> token_value_convert1;

1585

token5 >> token_value_convert2;

1586

convert_y = uiuc_convert(token_value_convert1);

1587

convert_x = uiuc_convert(token_value_convert2);

1588

/* call 1D File Reader with file name (CZfa) and conversion

1589

factors; function returns array of alphas (aArray) and

1590

corresponding CZ values (CZArray) and max number of

1591

terms in arrays (nAlpha) */

1592

uiuc_1DdataFileReader(CZfa,

1593

CZfa_aArray,

1594

CZfa_CZArray,

1595

CZfa_nAlpha);

1596

aeroLiftParts -> storeCommands (*command_line);

1597

break;

1598

}

1599

default:

1600

{

1601

uiuc_warnings_errors(2, *command_line);

1602

break;

1603

}

1604

};

1605

break;

1606

} // end CL map

1607

1608

1609

case Cm_flag:

1610

{

1611

switch(Cm_map[linetoken2])

1612

{

1613

case Cmo_flag:

1614

{

1615

if (check_float(linetoken3))

1616

token3 >> token_value;

1617

else

1618

uiuc_warnings_errors(1, *command_line);

1619

1620

Cmo = token_value;

1621

Cmo_clean = Cmo;

1622

aeroPitchParts -> storeCommands (*command_line);

1623

break;

1624

}

1625

case Cm_a_flag:

1626

{

1627

if (check_float(linetoken3))

1628

token3 >> token_value;

1629

else

1630

uiuc_warnings_errors(1, *command_line);

1631

1632

Cm_a = token_value;

1633

Cm_a_clean = Cm_a;

1634

aeroPitchParts -> storeCommands (*command_line);

1635

break;

1636

}

1637

case Cm_a2_flag:

1638

{

1639

if (check_float(linetoken3))

1640

token3 >> token_value;

1641

else

1642

uiuc_warnings_errors(1, *command_line);

1643

1644

Cm_a2 = token_value;

1645

Cm_a2_clean = Cm_a2;

1646

aeroPitchParts -> storeCommands (*command_line);

1647

break;

1648

}

1649

case Cm_adot_flag:

1650

{

1651

if (check_float(linetoken3))

1652

token3 >> token_value;

1653

else

1654

uiuc_warnings_errors(1, *command_line);

1655

1656

Cm_adot = token_value;

1657

Cm_adot_clean = Cm_adot;

1658

aeroPitchParts -> storeCommands (*command_line);

1659

break;

1660

}

1661

case Cm_q_flag:

1662

{

1663

if (check_float(linetoken3))

1664

token3 >> token_value;

1665

else

1666

uiuc_warnings_errors(1, *command_line);

1667

1668

Cm_q = token_value;

1669

Cm_q_clean = Cm_q;

1670

aeroPitchParts -> storeCommands (*command_line);

1671

break;

1672

}

1673

case Cm_ih_flag:

1674

{

1675

if (check_float(linetoken3))

1676

token3 >> token_value;

1677

else

1678

uiuc_warnings_errors(1, *command_line);

1679

1680

Cm_ih = token_value;

1681

aeroPitchParts -> storeCommands (*command_line);

1682

break;

1683

}

1684

case Cm_de_flag:

1685

{

1686

if (check_float(linetoken3))

1687

token3 >> token_value;

1688

else

1689

uiuc_warnings_errors(1, *command_line);

1690

1691

Cm_de = token_value;

1692

Cm_de_clean = Cm_de;

1693

aeroPitchParts -> storeCommands (*command_line);

1694

break;

1695

}

1696

case Cm_b2_flag:

1697

{

1698

if (check_float(linetoken3))

1699

token3 >> token_value;

1700

else

1701

uiuc_warnings_errors(1, *command_line);

1702

1703

Cm_b2 = token_value;

1704

Cm_b2_clean = Cm_b2;

1705

aeroPitchParts -> storeCommands (*command_line);

1706

break;

1707

}

1708

case Cm_r_flag:

1709

{

1710

if (check_float(linetoken3))

1711

token3 >> token_value;

1712

else

1713

uiuc_warnings_errors(1, *command_line);

1714

1715

Cm_r = token_value;

1716

Cm_r_clean = Cm_r;

1717

aeroPitchParts -> storeCommands (*command_line);

1718

break;

1719

}

1720

case Cm_df_flag:

1721

{

1722

if (check_float(linetoken3))

1723

token3 >> token_value;

1724

else

1725

uiuc_warnings_errors(1, *command_line);

1726

1727

Cm_df = token_value;

1728

Cm_df_clean = Cm_df;

1729

aeroPitchParts -> storeCommands (*command_line);

1730

break;

1731

}

1732

case Cmfa_flag:

1733

{

1734

Cmfa = linetoken3;

1735

token4 >> token_value_convert1;

1736

token5 >> token_value_convert2;

1737

convert_y = uiuc_convert(token_value_convert1);

1738

convert_x = uiuc_convert(token_value_convert2);

1739

/* call 1D File Reader with file name (Cmfa) and conversion

1740

factors; function returns array of alphas (aArray) and

1741

corresponding Cm values (CmArray) and max number of

1742

terms in arrays (nAlpha) */

1743

uiuc_1DdataFileReader(Cmfa,

1744

Cmfa_aArray,

1745

Cmfa_CmArray,

1746

Cmfa_nAlpha);

1747

aeroPitchParts -> storeCommands (*command_line);

1748

break;

1749

}

1750

case Cmfade_flag:

1751

{

1752

Cmfade = linetoken3;

1753

token4 >> token_value_convert1;

1754

token5 >> token_value_convert2;

1755

token6 >> token_value_convert3;

1756

convert_z = uiuc_convert(token_value_convert1);

1757

convert_x = uiuc_convert(token_value_convert2);

1758

convert_y = uiuc_convert(token_value_convert3);

1759

/* call 2D File Reader with file name (Cmfade) and

1760

conversion factors; function returns array of

1761

elevator deflections (deArray) and corresponding

1762

alpha (aArray) and delta Cm (CmArray) values and

1763

max number of terms in alpha arrays (nAlphaArray)

1764

and deflection array (nde) */

1765

uiuc_2DdataFileReader(Cmfade,

1766

Cmfade_aArray,

1767

Cmfade_deArray,

1768

Cmfade_CmArray,

1769

Cmfade_nAlphaArray,

1770

Cmfade_nde);

1771

aeroPitchParts -> storeCommands (*command_line);

1772

break;

1773

}

1774

case Cmfdf_flag:

1775

{

1776

Cmfdf = linetoken3;

1777

token4 >> token_value_convert1;

1778

token5 >> token_value_convert2;

1779

convert_y = uiuc_convert(token_value_convert1);

1780

convert_x = uiuc_convert(token_value_convert2);

1781

/* call 1D File Reader with file name (Cmfdf) and conversion

1782

factors; function returns array of dfs (dfArray) and

1783

corresponding Cm values (CmArray) and max number of

1784

terms in arrays (ndf) */

1785

uiuc_1DdataFileReader(Cmfdf,

1786

Cmfdf_dfArray,

1787

Cmfdf_CmArray,

1788

Cmfdf_ndf);

1789

aeroPitchParts -> storeCommands (*command_line);

1790

break;

1791

}

1792

case Cmfadf_flag:

1793

{

1794

Cmfadf = linetoken3;

1795

token4 >> token_value_convert1;

1796

token5 >> token_value_convert2;

1797

token6 >> token_value_convert3;

1798

convert_z = uiuc_convert(token_value_convert1);

1799

convert_x = uiuc_convert(token_value_convert2);

1800

convert_y = uiuc_convert(token_value_convert3);

1801

/* call 2D File Reader with file name (Cmfadf) and

1802

conversion factors; function returns array of

1803

flap deflections (dfArray) and corresponding

1804

alpha (aArray) and delta Cm (CmArray) values and

1805

max number of terms in alpha arrays (nAlphaArray)

1806

and deflection array (ndf) */

1807

uiuc_2DdataFileReader(Cmfadf,

1808

Cmfadf_aArray,

1809

Cmfadf_dfArray,

1810

Cmfadf_CmArray,

1811

Cmfadf_nAlphaArray,

1812

Cmfadf_ndf);

1813

aeroPitchParts -> storeCommands (*command_line);

1814

break;

1815

}

1816

default:

1817

{

1818

uiuc_warnings_errors(2, *command_line);

1819

break;

1820

}

1821

};

1822

break;

1823

} // end Cm map

1824

1825

1826

case CY_flag:

1827

{

1828

switch(CY_map[linetoken2])

1829

{

1830

case CYo_flag:

1831

{

1832

if (check_float(linetoken3))

1833

token3 >> token_value;

1834

else

1835

uiuc_warnings_errors(1, *command_line);

1836

1837

CYo = token_value;

1838

CYo_clean = CYo;

1839

aeroSideforceParts -> storeCommands (*command_line);

1840

break;

1841

}

1842

case CY_beta_flag:

1843

{

1844

if (check_float(linetoken3))

1845

token3 >> token_value;

1846

else

1847

uiuc_warnings_errors(1, *command_line);

1848

1849

CY_beta = token_value;

1850

CY_beta_clean = CY_beta;

1851

aeroSideforceParts -> storeCommands (*command_line);

1852

break;

1853

}

1854

case CY_p_flag:

1855

{

1856

if (check_float(linetoken3))

1857

token3 >> token_value;

1858

else

1859

uiuc_warnings_errors(1, *command_line);

1860

1861

CY_p = token_value;

1862

CY_p_clean = CY_p;

1863

aeroSideforceParts -> storeCommands (*command_line);

1864

break;

1865

}

1866

case CY_r_flag:

1867

{

1868

if (check_float(linetoken3))

1869

token3 >> token_value;

1870

else

1871

uiuc_warnings_errors(1, *command_line);

1872

1873

CY_r = token_value;

1874

CY_r_clean = CY_r;

1875

aeroSideforceParts -> storeCommands (*command_line);

1876

break;

1877

}

1878

case CY_da_flag:

1879

{

1880

if (check_float(linetoken3))

1881

token3 >> token_value;

1882

else

1883

uiuc_warnings_errors(1, *command_line);

1884

1885

CY_da = token_value;

1886

CY_da_clean = CY_da;

1887

aeroSideforceParts -> storeCommands (*command_line);

1888

break;

1889

}

1890

case CY_dr_flag:

1891

{

1892

if (check_float(linetoken3))

1893

token3 >> token_value;

1894

else

1895

uiuc_warnings_errors(2, *command_line);

1896

1897

CY_dr = token_value;

1898

CY_dr_clean = CY_dr;

1899

aeroSideforceParts -> storeCommands (*command_line);

1900

break;

1901

}

1902

case CY_dra_flag:

1903

{

1904

if (check_float(linetoken3))

1905

token3 >> token_value;

1906

else

1907

uiuc_warnings_errors(2, *command_line);

1908

1909

CY_dra = token_value;

1910

CY_dra_clean = CY_dra;

1911

aeroSideforceParts -> storeCommands (*command_line);

1912

break;

1913

}

1914

case CY_bdot_flag:

1915

{

1916

if (check_float(linetoken3))

1917

token3 >> token_value;

1918

else

1919

uiuc_warnings_errors(2, *command_line);

1920

1921

CY_bdot = token_value;

1922

CY_bdot_clean = CY_bdot;

1923

aeroSideforceParts -> storeCommands (*command_line);

1924

break;

1925

}

1926

case CYfada_flag:

1927

{

1928

CYfada = linetoken3;

1929

token4 >> token_value_convert1;

1930

token5 >> token_value_convert2;

1931

token6 >> token_value_convert3;

1932

convert_z = uiuc_convert(token_value_convert1);

1933

convert_x = uiuc_convert(token_value_convert2);

1934

convert_y = uiuc_convert(token_value_convert3);

1935

/* call 2D File Reader with file name (CYfada) and

1936

conversion factors; function returns array of

1937

aileron deflections (daArray) and corresponding

1938

alpha (aArray) and delta CY (CYArray) values and

1939

max number of terms in alpha arrays (nAlphaArray)

1940

and deflection array (nda) */

1941

uiuc_2DdataFileReader(CYfada,

1942

CYfada_aArray,

1943

CYfada_daArray,

1944

CYfada_CYArray,

1945

CYfada_nAlphaArray,

1946

CYfada_nda);

1947

aeroSideforceParts -> storeCommands (*command_line);

1948

break;

1949

}

1950

case CYfbetadr_flag:

1951

{

1952

CYfbetadr = linetoken3;

1953

token4 >> token_value_convert1;

1954

token5 >> token_value_convert2;

1955

token6 >> token_value_convert3;

1956

convert_z = uiuc_convert(token_value_convert1);

1957

convert_x = uiuc_convert(token_value_convert2);

1958

convert_y = uiuc_convert(token_value_convert3);

1959

/* call 2D File Reader with file name (CYfbetadr) and

1960

conversion factors; function returns array of

1961

rudder deflections (drArray) and corresponding

1962

beta (betaArray) and delta CY (CYArray) values and

1963

max number of terms in beta arrays (nBetaArray)

1964

and deflection array (ndr) */

1965

uiuc_2DdataFileReader(CYfbetadr,

1966

CYfbetadr_betaArray,

1967

CYfbetadr_drArray,

1968

CYfbetadr_CYArray,

1969

CYfbetadr_nBetaArray,

1970

CYfbetadr_ndr);

1971

aeroSideforceParts -> storeCommands (*command_line);

1972

break;

1973

}

1974

default:

1975

{

1976

uiuc_warnings_errors(2, *command_line);

1977

break;

1978

}

1979

};

1980

break;

1981

} // end CY map

1982

1983

1984

case Cl_flag:

1985

{

1986

switch(Cl_map[linetoken2])

1987

{

1988

case Clo_flag:

1989

{

1990

if (check_float(linetoken3))

1991

token3 >> token_value;

1992

else

1993

uiuc_warnings_errors(1, *command_line);

1994

1995

Clo = token_value;

1996

Clo_clean = Clo;

1997

aeroRollParts -> storeCommands (*command_line);

1998

break;

1999

}

2000

case Cl_beta_flag:

2001

{

2002

if (check_float(linetoken3))

2003

token3 >> token_value;

2004

else

2005

uiuc_warnings_errors(1, *command_line);

2006

2007

Cl_beta = token_value;

2008

Cl_beta_clean = Cl_beta;

2009

aeroRollParts -> storeCommands (*command_line);

2010

break;

2011

}

2012

case Cl_p_flag:

2013

{

2014

if (check_float(linetoken3))

2015

token3 >> token_value;

2016

else

2017

uiuc_warnings_errors(1, *command_line);

2018

2019

Cl_p = token_value;

2020

Cl_p_clean = Cl_p;

2021

aeroRollParts -> storeCommands (*command_line);

2022

break;

2023

}

2024

case Cl_r_flag:

2025

{

2026

if (check_float(linetoken3))

2027

token3 >> token_value;

2028

else

2029

uiuc_warnings_errors(1, *command_line);

2030

2031

Cl_r = token_value;

2032

Cl_r_clean = Cl_r;

2033

aeroRollParts -> storeCommands (*command_line);

2034

break;

2035

}

2036

case Cl_da_flag:

2037

{

2038

if (check_float(linetoken3))

2039

token3 >> token_value;

2040

else

2041

uiuc_warnings_errors(1, *command_line);

2042

2043

Cl_da = token_value;

2044

Cl_da_clean = Cl_da;

2045

aeroRollParts -> storeCommands (*command_line);

2046

break;

2047

}

2048

case Cl_dr_flag:

2049

{

2050

if (check_float(linetoken3))

2051

token3 >> token_value;

2052

else

2053

uiuc_warnings_errors(1, *command_line);

2054

2055

Cl_dr = token_value;

2056

Cl_dr_clean = Cl_dr;

2057

aeroRollParts -> storeCommands (*command_line);

2058

break;

2059

}

2060

case Cl_daa_flag:

2061

{

2062

if (check_float(linetoken3))

2063

token3 >> token_value;

2064

else

2065

uiuc_warnings_errors(1, *command_line);

2066

2067

Cl_daa = token_value;

2068

Cl_daa_clean = Cl_daa;

2069

aeroRollParts -> storeCommands (*command_line);

2070

break;

2071

}

2072

case Clfada_flag:

2073

{

2074

Clfada = linetoken3;

2075

token4 >> token_value_convert1;

2076

token5 >> token_value_convert2;

2077

token6 >> token_value_convert3;

2078

convert_z = uiuc_convert(token_value_convert1);

2079

convert_x = uiuc_convert(token_value_convert2);

2080

convert_y = uiuc_convert(token_value_convert3);

2081

/* call 2D File Reader with file name (Clfada) and

2082

conversion factors; function returns array of

2083

aileron deflections (daArray) and corresponding

2084

alpha (aArray) and delta Cl (ClArray) values and

2085

max number of terms in alpha arrays (nAlphaArray)

2086

and deflection array (nda) */

2087

uiuc_2DdataFileReader(Clfada,

2088

Clfada_aArray,

2089

Clfada_daArray,

2090

Clfada_ClArray,

2091

Clfada_nAlphaArray,

2092

Clfada_nda);

2093

aeroRollParts -> storeCommands (*command_line);

2094

break;

2095

}

2096

case Clfbetadr_flag:

2097

{

2098

Clfbetadr = linetoken3;

2099

token4 >> token_value_convert1;

2100

token5 >> token_value_convert2;

2101

token6 >> token_value_convert3;

2102

convert_z = uiuc_convert(token_value_convert1);

2103

convert_x = uiuc_convert(token_value_convert2);

2104

convert_y = uiuc_convert(token_value_convert3);

2105

/* call 2D File Reader with file name (Clfbetadr) and

2106

conversion factors; function returns array of

2107

rudder deflections (drArray) and corresponding

2108

beta (betaArray) and delta Cl (ClArray) values and

2109

max number of terms in beta arrays (nBetaArray)

2110

and deflection array (ndr) */

2111

uiuc_2DdataFileReader(Clfbetadr,

2112

Clfbetadr_betaArray,

2113

Clfbetadr_drArray,

2114

Clfbetadr_ClArray,

2115

Clfbetadr_nBetaArray,

2116

Clfbetadr_ndr);

2117

aeroRollParts -> storeCommands (*command_line);

2118

break;

2119

}

2120

default:

2121

{

2122

uiuc_warnings_errors(2, *command_line);

2123

break;

2124

}

2125

};

2126

break;

2127

} // end Cl map

2128

2129

2130

case Cn_flag:

2131

{

2132

switch(Cn_map[linetoken2])

2133

{

2134

case Cno_flag:

2135

{

2136

if (check_float(linetoken3))

2137

token3 >> token_value;

2138

else

2139

uiuc_warnings_errors(1, *command_line);

2140

2141

Cno = token_value;

2142

Cno_clean = Cno;

2143

aeroYawParts -> storeCommands (*command_line);

2144

break;

2145

}

2146

case Cn_beta_flag:

2147

{

2148

if (check_float(linetoken3))

2149

token3 >> token_value;

2150

else

2151

uiuc_warnings_errors(1, *command_line);

2152

2153

Cn_beta = token_value;

2154

Cn_beta_clean = Cn_beta;

2155

aeroYawParts -> storeCommands (*command_line);

2156

break;

2157

}

2158

case Cn_p_flag:

2159

{

2160

if (check_float(linetoken3))

2161

token3 >> token_value;

2162

else

2163

uiuc_warnings_errors(1, *command_line);

2164

2165

Cn_p = token_value;

2166

Cn_p_clean = Cn_p;

2167

aeroYawParts -> storeCommands (*command_line);

2168

break;

2169

}

2170

case Cn_r_flag:

2171

{

2172

if (check_float(linetoken3))

2173

token3 >> token_value;

2174

else

2175

uiuc_warnings_errors(1, *command_line);

2176

2177

Cn_r = token_value;

2178

Cn_r_clean = Cn_r;

2179

aeroYawParts -> storeCommands (*command_line);

2180

break;

2181

}

2182

case Cn_da_flag:

2183

{

2184

if (check_float(linetoken3))

2185

token3 >> token_value;

2186

else

2187

uiuc_warnings_errors(1, *command_line);

2188

2189

Cn_da = token_value;

2190

Cn_da_clean = Cn_da;

2191

aeroYawParts -> storeCommands (*command_line);

2192

break;

2193

}

2194

case Cn_dr_flag:

2195

{

2196

if (check_float(linetoken3))

2197

token3 >> token_value;

2198

else

2199

uiuc_warnings_errors(1, *command_line);

2200

2201

Cn_dr = token_value;

2202

Cn_dr_clean = Cn_dr;

2203

aeroYawParts -> storeCommands (*command_line);

2204

break;

2205

}

2206

case Cn_q_flag:

2207

{

2208

if (check_float(linetoken3))

2209

token3 >> token_value;

2210

else

2211

uiuc_warnings_errors(1, *command_line);

2212

2213

Cn_q = token_value;

2214

Cn_q_clean = Cn_q;

2215

aeroYawParts -> storeCommands (*command_line);

2216

break;

2217

}

2218

case Cn_b3_flag:

2219

{

2220

if (check_float(linetoken3))

2221

token3 >> token_value;

2222

else

2223

uiuc_warnings_errors(1, *command_line);

2224

2225

Cn_b3 = token_value;

2226

Cn_b3_clean = Cn_b3;

2227

aeroYawParts -> storeCommands (*command_line);

2228

break;

2229

}

2230

case Cnfada_flag:

2231

{

2232

Cnfada = linetoken3;

2233

token4 >> token_value_convert1;

2234

token5 >> token_value_convert2;

2235

token6 >> token_value_convert3;

2236

convert_z = uiuc_convert(token_value_convert1);

2237

convert_x = uiuc_convert(token_value_convert2);

2238

convert_y = uiuc_convert(token_value_convert3);

2239

/* call 2D File Reader with file name (Cnfada) and

2240

conversion factors; function returns array of

2241

aileron deflections (daArray) and corresponding

2242

alpha (aArray) and delta Cn (CnArray) values and

2243

max number of terms in alpha arrays (nAlphaArray)

2244

and deflection array (nda) */

2245

uiuc_2DdataFileReader(Cnfada,

2246

Cnfada_aArray,

2247

Cnfada_daArray,

2248

Cnfada_CnArray,

2249

Cnfada_nAlphaArray,

2250

Cnfada_nda);

2251

aeroYawParts -> storeCommands (*command_line);

2252

break;

2253

}

2254

case Cnfbetadr_flag:

2255

{

2256

Cnfbetadr = linetoken3;

2257

token4 >> token_value_convert1;

2258

token5 >> token_value_convert2;

2259

token6 >> token_value_convert3;

2260

convert_z = uiuc_convert(token_value_convert1);

2261

convert_x = uiuc_convert(token_value_convert2);

2262

convert_y = uiuc_convert(token_value_convert3);

2263

/* call 2D File Reader with file name (Cnfbetadr) and

2264

conversion factors; function returns array of

2265

rudder deflections (drArray) and corresponding

2266

beta (betaArray) and delta Cn (CnArray) values and

2267

max number of terms in beta arrays (nBetaArray)

2268

and deflection array (ndr) */

2269

uiuc_2DdataFileReader(Cnfbetadr,

2270

Cnfbetadr_betaArray,

2271

Cnfbetadr_drArray,

2272

Cnfbetadr_CnArray,

2273

Cnfbetadr_nBetaArray,

2274

Cnfbetadr_ndr);

2275

aeroYawParts -> storeCommands (*command_line);

2276

break;

2277

}

2278

default:

2279

{

2280

uiuc_warnings_errors(2, *command_line);

2281

break;

2282

}

2283

};

2284

break;

2285

} // end Cn map

2286

2287

2288

case gear_flag:

2289

{

2290

int index;

2291

token3 >> index;

2292

if (index < 0 || index >= 16)

2293

uiuc_warnings_errors(1, *command_line);

2294

switch(gear_map[linetoken2])

2295

{

2296

case Dx_gear_flag:

2297

{

2298

if (check_float(linetoken3))

2299

token4 >> token_value;

2300

else

2301

uiuc_warnings_errors(1, *command_line);

2302

D_gear_v[index][0] = token_value;

2303

gear_model[index] = true;

2304

break;

2305

}

2306

case Dy_gear_flag:

2307

{

2308

if (check_float(linetoken3))

2309

token4 >> token_value;

2310

else

2311

uiuc_warnings_errors(1, *command_line);

2312

D_gear_v[index][1] = token_value;

2313

gear_model[index] = true;

2314

break;

2315

}

2316

case Dz_gear_flag:

2317

{

2318

if (check_float(linetoken3))

2319

token4 >> token_value;

2320

else

2321

uiuc_warnings_errors(1, *command_line);

2322

D_gear_v[index][2] = token_value;

2323

gear_model[index] = true;

2324

break;

2325

}

2326

case cgear_flag:

2327

{

2328

if (check_float(linetoken3))

2329

token4 >> token_value;

2330

else

2331

uiuc_warnings_errors(1, *command_line);

2332

cgear[index] = token_value;

2333

gear_model[index] = true;

2334

break;

2335

}

2336

case kgear_flag:

2337

{

2338

if (check_float(linetoken3))

2339

token4 >> token_value;

2340

else

2341

uiuc_warnings_errors(1, *command_line);

2342

kgear[index] = token_value;

2343

gear_model[index] = true;

2344

break;

2345

}

2346

case muGear_flag:

2347

{

2348

if (check_float(linetoken3))

2349

token4 >> token_value;

2350

else

2351

uiuc_warnings_errors(1, *command_line);

2352

muGear[index] = token_value;

2353

gear_model[index] = true;

2354

break;

2355

}

2356

case strutLength_flag:

2357

{

2358

if (check_float(linetoken3))

2359

token4 >> token_value;

2360

else

2361

uiuc_warnings_errors(1, *command_line);

2362

strutLength[index] = token_value;

2363

gear_model[index] = true;

2364

break;

2365

}

2366

default:

2367

{

2368

uiuc_warnings_errors(2, *command_line);

2369

break;

2370

}

2371

};

2372

break;

2373

} // end gear map

2374

2375

2376

case ice_flag:

2377

{

2378

switch(ice_map[linetoken2])

2379

{

2380

case iceTime_flag:

2381

{

2382

if (check_float(linetoken3))

2383

token3 >> token_value;

2384

2385

else

2386

uiuc_warnings_errors(1, *command_line);

2387

2388

ice_model = true;

2389

iceTime = token_value;

2390

break;

2391

}

2392

case transientTime_flag:

2393

{

2394

if (check_float(linetoken3))

2395

token3 >> token_value;

2396

else

2397

uiuc_warnings_errors(1, *command_line);

2398

2399

transientTime = token_value;

2400

break;

2401

}

2402

case eta_ice_final_flag:

2403

{

2404

if (check_float(linetoken3))

2405

token3 >> token_value;

2406

else

2407

uiuc_warnings_errors(1, *command_line);

2408

2409

eta_ice_final = token_value;

2410

break;

2411

}

2412

case beta_probe_wing_flag:

2413

{

2414

if (check_float(linetoken3))

2415

token3 >> token_value;

2416

else

2417

uiuc_warnings_errors(1, *command_line);

2418

2419

beta_model = true;

2420

x_probe_wing = token_value;

2421

break;

2422

}

2423

case beta_probe_tail_flag:

2424

{

2425

if (check_float(linetoken3))

2426

token3 >> token_value;

2427

else

2428

uiuc_warnings_errors(1, *command_line);

2429

2430

beta_model = true;

2431

x_probe_tail = token_value;

2432

break;

2433

}

2434

case kCDo_flag:

2435

{

2436

if (check_float(linetoken3))

2437

token3 >> token_value;

2438

else

2439

uiuc_warnings_errors(1, *command_line);

2440

2441

kCDo = token_value;

2442

break;

2443

}

2444

case kCDK_flag:

2445

{

2446

if (check_float(linetoken3))

2447

token3 >> token_value;

2448

else

2449

uiuc_warnings_errors(1, *command_line);

2450

2451

kCDK = token_value;

2452

break;

2453

}

2454

case kCD_a_flag:

2455

{

2456

if (check_float(linetoken3))

2457

token3 >> token_value;

2458

else

2459

uiuc_warnings_errors(1, *command_line);

2460

2461

kCD_a = token_value;

2462

break;

2463

}

2464

case kCD_adot_flag:

2465

{

2466

if (check_float(linetoken3))

2467

token3 >> token_value;

2468

else

2469

uiuc_warnings_errors(1, *command_line);

2470

2471

kCD_adot = token_value;

2472

break;

2473

}

2474

case kCD_q_flag:

2475

{

2476

if (check_float(linetoken3))

2477

token3 >> token_value;

2478

else

2479

uiuc_warnings_errors(1, *command_line);

2480

2481

kCD_q = token_value;

2482

break;

2483

}

2484

case kCD_de_flag:

2485

{

2486

if (check_float(linetoken3))

2487

token3 >> token_value;

2488

else

2489

uiuc_warnings_errors(1, *command_line);

2490

2491

kCD_de = token_value;

2492

break;

2493

}

2494

case kCXo_flag:

2495

{

2496

if (check_float(linetoken3))

2497

token3 >> token_value;

2498

else

2499

uiuc_warnings_errors(1, *command_line);

2500

2501

kCXo = token_value;

2502

break;

2503

}

2504

case kCXK_flag:

2505

{

2506

if (check_float(linetoken3))

2507

token3 >> token_value;

2508

else

2509

uiuc_warnings_errors(1, *command_line);

2510

2511

kCXK = token_value;

2512

break;

2513

}

2514

case kCX_a_flag:

2515

{

2516

if (check_float(linetoken3))

2517

token3 >> token_value;

2518

else

2519

uiuc_warnings_errors(1, *command_line);

2520

2521

kCX_a = token_value;

2522

break;

2523

}

2524

case kCX_a2_flag:

2525

{

2526

if (check_float(linetoken3))

2527

token3 >> token_value;

2528

else

2529

uiuc_warnings_errors(1, *command_line);

2530

2531

kCX_a2 = token_value;

2532

break;

2533

}

2534

case kCX_a3_flag:

2535

{

2536

if (check_float(linetoken3))

2537

token3 >> token_value;

2538

else

2539

uiuc_warnings_errors(1, *command_line);

2540

2541

kCX_a3 = token_value;

2542

break;

2543

}

2544

case kCX_adot_flag:

2545

{

2546

if (check_float(linetoken3))

2547

token3 >> token_value;

2548

else

2549

uiuc_warnings_errors(1, *command_line);

2550

2551

kCX_adot = token_value;

2552

break;

2553

}

2554

case kCX_q_flag:

2555

{

2556

if (check_float(linetoken3))

2557

token3 >> token_value;

2558

else

2559

uiuc_warnings_errors(1, *command_line);

2560

2561

kCX_q = token_value;

2562

break;

2563

}

2564

case kCX_de_flag:

2565

{

2566

if (check_float(linetoken3))

2567

token3 >> token_value;

2568

else

2569

uiuc_warnings_errors(1, *command_line);

2570

2571

kCX_de = token_value;

2572

break;

2573

}

2574

case kCX_dr_flag:

2575

{

2576

if (check_float(linetoken3))

2577

token3 >> token_value;

2578

else

2579

uiuc_warnings_errors(1, *command_line);

2580

2581

kCX_dr = token_value;

2582

break;

2583

}

2584

case kCX_df_flag:

2585

{

2586

if (check_float(linetoken3))

2587

token3 >> token_value;

2588

else

2589

uiuc_warnings_errors(1, *command_line);

2590

2591

kCX_df = token_value;

2592

break;

2593

}

2594

case kCX_adf_flag:

2595

{

2596

if (check_float(linetoken3))

2597

token3 >> token_value;

2598

else

2599

uiuc_warnings_errors(1, *command_line);

2600

2601

kCX_adf = token_value;

2602

break;

2603

}

2604

case kCLo_flag:

2605

{

2606

if (check_float(linetoken3))

2607

token3 >> token_value;

2608

else

2609

uiuc_warnings_errors(1, *command_line);

2610

2611

kCLo = token_value;

2612

break;

2613

}

2614

case kCL_a_flag:

2615

{

2616

if (check_float(linetoken3))

2617

token3 >> token_value;

2618

else

2619

uiuc_warnings_errors(1, *command_line);

2620

2621

kCL_a = token_value;

2622

break;

2623

}

2624

case kCL_adot_flag:

2625

{

2626

if (check_float(linetoken3))

2627

token3 >> token_value;

2628

else

2629

uiuc_warnings_errors(1, *command_line);

2630

2631

kCL_adot = token_value;

2632

break;

2633

}

2634

case kCL_q_flag:

2635

{

2636

if (check_float(linetoken3))

2637

token3 >> token_value;

2638

else

2639

uiuc_warnings_errors(1, *command_line);

2640

2641

kCL_q = token_value;

2642

break;

2643

}

2644

case kCL_de_flag:

2645

{

2646

if (check_float(linetoken3))

2647

token3 >> token_value;

2648

else

2649

uiuc_warnings_errors(1, *command_line);

2650

2651

kCL_de = token_value;

2652

break;

2653

}

2654

case kCZo_flag:

2655

{

2656

if (check_float(linetoken3))

2657

token3 >> token_value;

2658

else

2659

uiuc_warnings_errors(1, *command_line);

2660

2661

kCZo = token_value;

2662

break;

2663

}

2664

case kCZ_a_flag:

2665

{

2666

if (check_float(linetoken3))

2667

token3 >> token_value;

2668

else

2669

uiuc_warnings_errors(1, *command_line);

2670

2671

kCZ_a = token_value;

2672

break;

2673

}

2674

case kCZ_a2_flag:

2675

{

2676

if (check_float(linetoken3))

2677

token3 >> token_value;

2678

else

2679

uiuc_warnings_errors(1, *command_line);

2680

2681

kCZ_a2 = token_value;

2682

break;

2683

}

2684

case kCZ_a3_flag:

2685

{

2686

if (check_float(linetoken3))

2687

token3 >> token_value;

2688

else

2689

uiuc_warnings_errors(1, *command_line);

2690

2691

kCZ_a3 = token_value;

2692

break;

2693

}

2694

case kCZ_adot_flag:

2695

{

2696

if (check_float(linetoken3))

2697

token3 >> token_value;

2698

else

2699

uiuc_warnings_errors(1, *command_line);

2700

2701

kCZ_adot = token_value;

2702

break;

2703

}

2704

case kCZ_q_flag:

2705

{

2706

if (check_float(linetoken3))

2707

token3 >> token_value;

2708

else

2709

uiuc_warnings_errors(1, *command_line);

2710

2711

kCZ_q = token_value;

2712

break;

2713

}

2714

case kCZ_de_flag:

2715

{

2716

if (check_float(linetoken3))

2717

token3 >> token_value;

2718

else

2719

uiuc_warnings_errors(1, *command_line);

2720

2721

kCZ_de = token_value;

2722

break;

2723

}

2724

case kCZ_deb2_flag:

2725

{

2726

if (check_float(linetoken3))

2727

token3 >> token_value;

2728

else

2729

uiuc_warnings_errors(1, *command_line);

2730

2731

kCZ_deb2 = token_value;

2732

break;

2733

}

2734

case kCZ_df_flag:

2735

{

2736

if (check_float(linetoken3))

2737

token3 >> token_value;

2738

else

2739

uiuc_warnings_errors(1, *command_line);

2740

2741

kCZ_df = token_value;

2742

break;

2743

}

2744

case kCZ_adf_flag:

2745

{

2746

if (check_float(linetoken3))

2747

token3 >> token_value;

2748

else

2749

uiuc_warnings_errors(1, *command_line);

2750

2751

kCZ_adf = token_value;

2752

break;

2753

}

2754

case kCmo_flag:

2755

{

2756

if (check_float(linetoken3))

2757

token3 >> token_value;

2758

else

2759

uiuc_warnings_errors(1, *command_line);

2760

2761

kCmo = token_value;

2762

break;

2763

}

2764

case kCm_a_flag:

2765

{

2766

if (check_float(linetoken3))

2767

token3 >> token_value;

2768

else

2769

uiuc_warnings_errors(1, *command_line);

2770

2771

kCm_a = token_value;

2772

break;

2773

}

2774

case kCm_a2_flag:

2775

{

2776

if (check_float(linetoken3))

2777

token3 >> token_value;

2778

else

2779

uiuc_warnings_errors(1, *command_line);

2780

2781

kCm_a2 = token_value;

2782

break;

2783

}

2784

case kCm_adot_flag:

2785

{

2786

if (check_float(linetoken3))

2787

token3 >> token_value;

2788

else

2789

uiuc_warnings_errors(1, *command_line);

2790

2791

kCm_adot = token_value;

2792

break;

2793

}

2794

case kCm_q_flag:

2795

{

2796

if (check_float(linetoken3))

2797

token3 >> token_value;

2798

else

2799

uiuc_warnings_errors(1, *command_line);

2800

2801

kCm_q = token_value;

2802

break;

2803

}

2804

case kCm_de_flag:

2805

{

2806

if (check_float(linetoken3))

2807

token3 >> token_value;

2808

else

2809

uiuc_warnings_errors(1, *command_line);

2810

2811

kCm_de = token_value;

2812

break;

2813

}

2814

case kCm_b2_flag:

2815

{

2816

if (check_float(linetoken3))

2817

token3 >> token_value;

2818

else

2819

uiuc_warnings_errors(1, *command_line);

2820

2821

kCm_b2 = token_value;

2822

break;

2823

}

2824

case kCm_r_flag:

2825

{

2826

if (check_float(linetoken3))

2827

token3 >> token_value;

2828

else

2829

uiuc_warnings_errors(1, *command_line);

2830

2831

kCm_r = token_value;

2832

break;

2833

}

2834

case kCm_df_flag:

2835

{

2836

if (check_float(linetoken3))

2837

token3 >> token_value;

2838

else

2839

uiuc_warnings_errors(1, *command_line);

2840

2841

kCm_df = token_value;

2842

break;

2843

}

2844

case kCYo_flag:

2845

{

2846

if (check_float(linetoken3))

2847

token3 >> token_value;

2848

else

2849

uiuc_warnings_errors(1, *command_line);

2850

2851

kCYo = token_value;

2852

break;

2853

}

2854

case kCY_beta_flag:

2855

{

2856

if (check_float(linetoken3))

2857

token3 >> token_value;

2858

else

2859

uiuc_warnings_errors(1, *command_line);

2860

2861

kCY_beta = token_value;

2862

break;

2863

}

2864

case kCY_p_flag:

2865

{

2866

if (check_float(linetoken3))

2867

token3 >> token_value;

2868

else

2869

uiuc_warnings_errors(1, *command_line);

2870

2871

kCY_p = token_value;

2872

break;

2873

}

2874

case kCY_r_flag:

2875

{

2876

if (check_float(linetoken3))

2877

token3 >> token_value;

2878

else

2879

uiuc_warnings_errors(1, *command_line);

2880

2881

kCY_r = token_value;

2882

break;

2883

}

2884

case kCY_da_flag:

2885

{

2886

if (check_float(linetoken3))

2887

token3 >> token_value;

2888

else

2889

uiuc_warnings_errors(1, *command_line);

2890

2891

kCY_da = token_value;

2892

break;

2893

}

2894

case kCY_dr_flag:

2895

{

2896

if (check_float(linetoken3))

2897

token3 >> token_value;

2898

else

2899

uiuc_warnings_errors(1, *command_line);

2900

2901

kCY_dr = token_value;

2902

break;

2903

}

2904

case kCY_dra_flag:

2905

{

2906

if (check_float(linetoken3))

2907

token3 >> token_value;

2908

else

2909

uiuc_warnings_errors(1, *command_line);

2910

2911

kCY_dra = token_value;

2912

break;

2913

}

2914

case kCY_bdot_flag:

2915

{

2916

if (check_float(linetoken3))

2917

token3 >> token_value;

2918

else

2919

uiuc_warnings_errors(1, *command_line);

2920

2921

kCY_bdot = token_value;

2922

break;

2923

}

2924

case kClo_flag:

2925

{

2926

if (check_float(linetoken3))

2927

token3 >> token_value;

2928

else

2929

uiuc_warnings_errors(1, *command_line);

2930

2931

kClo = token_value;

2932

break;

2933

}

2934

case kCl_beta_flag:

2935

{

2936

if (check_float(linetoken3))

2937

token3 >> token_value;

2938

else

2939

uiuc_warnings_errors(1, *command_line);

2940

2941

kCl_beta = token_value;

2942

break;

2943

}

2944

case kCl_p_flag:

2945

{

2946

if (check_float(linetoken3))

2947

token3 >> token_value;

2948

else

2949

uiuc_warnings_errors(1, *command_line);

2950

2951

kCl_p = token_value;

2952

break;

2953

}

2954

case kCl_r_flag:

2955

{

2956

if (check_float(linetoken3))

2957

token3 >> token_value;

2958

else

2959

uiuc_warnings_errors(1, *command_line);

2960

2961

kCl_r = token_value;

2962

break;

2963

}

2964

case kCl_da_flag:

2965

{

2966

if (check_float(linetoken3))

2967

token3 >> token_value;

2968

else

2969

uiuc_warnings_errors(1, *command_line);

2970

2971

kCl_da = token_value;

2972

break;

2973

}

2974

case kCl_dr_flag:

2975

{

2976

if (check_float(linetoken3))

2977

token3 >> token_value;

2978

else

2979

uiuc_warnings_errors(1, *command_line);

2980

2981

kCl_dr = token_value;

2982

break;

2983

}

2984

case kCl_daa_flag:

2985

{

2986

if (check_float(linetoken3))

2987

token3 >> token_value;

2988

else

2989

uiuc_warnings_errors(1, *command_line);

2990

2991

kCl_daa = token_value;

2992

break;

2993

}

2994

case kCno_flag:

2995

{

2996

if (check_float(linetoken3))

2997

token3 >> token_value;

2998

else

2999

uiuc_warnings_errors(1, *command_line);

3000

3001

kCno = token_value;

3002

break;

3003

}

3004

case kCn_beta_flag:

3005

{

3006

if (check_float(linetoken3))

3007

token3 >> token_value;

3008

else

3009

uiuc_warnings_errors(1, *command_line);

3010

3011

kCn_beta = token_value;

3012

break;

3013

}

3014

case kCn_p_flag:

3015

{

3016

if (check_float(linetoken3))

3017

token3 >> token_value;

3018

else

3019

uiuc_warnings_errors(1, *command_line);

3020

3021

kCn_p = token_value;

3022

break;

3023

}

3024

case kCn_r_flag:

3025

{

3026

if (check_float(linetoken3))

3027

token3 >> token_value;

3028

else

3029

uiuc_warnings_errors(1, *command_line);

3030

3031

kCn_r = token_value;

3032

break;

3033

}

3034

case kCn_da_flag:

3035

{

3036

if (check_float(linetoken3))

3037

token3 >> token_value;

3038

else

3039

uiuc_warnings_errors(1, *command_line);

3040

3041

kCn_da = token_value;

3042

break;

3043

}

3044

case kCn_dr_flag:

3045

{

3046

if (check_float(linetoken3))

3047

token3 >> token_value;

3048

else

3049

uiuc_warnings_errors(1, *command_line);

3050

3051

kCn_dr = token_value;

3052

break;

3053

}

3054

case kCn_q_flag:

3055

{

3056

if (check_float(linetoken3))

3057

token3 >> token_value;

3058

else

3059

uiuc_warnings_errors(1, *command_line);

3060

3061

kCn_q = token_value;

3062

break;

3063

}

3064

case kCn_b3_flag:

3065

{

3066

if (check_float(linetoken3))

3067

token3 >> token_value;

3068

else

3069

uiuc_warnings_errors(1, *command_line);

3070

3071

kCn_b3 = token_value;

3072

break;

3073

}

3074

default:

3075

{

3076

uiuc_warnings_errors(2, *command_line);

3077

break;

3078

}

3079

};

3080

break;

3081

} // end ice map

3082

3083

3084

case fog_flag:

3085

{

3086

switch(fog_map[linetoken2])

3087

{

3088

case fog_segments_flag:

3089

{

3090

if (check_float(linetoken3))

3091

token3 >> token_value_convert1;

3092

else

3093

uiuc_warnings_errors(1, *command_line);

3094

3095

if (token_value_convert1 < 1 || token_value_convert1 > 100)

3096

uiuc_warnings_errors(1, *command_line);

3097

3098

fog_field = true;

3099

fog_point_index = 0;

3100

delete[] fog_time;

3101

delete[] fog_value;

3102

fog_segments = token_value_convert1;

3103

fog_time = new double[fog_segments+1];

3104

fog_time[0] = 0.0;

3105

fog_value = new int[fog_segments+1];

3106

fog_value[0] = 0;

3107

3108

break;

3109

}

3110

case fog_point_flag:

3111

{

3112

if (check_float(linetoken3))

3113

token3 >> token_value;

3114

else

3115

uiuc_warnings_errors(1, *command_line);

3116

3117

if (token_value < 0.1)

3118

uiuc_warnings_errors(1, *command_line);

3119

3120

if (check_float(linetoken4))

3121

token4 >> token_value_convert1;

3122

else

3123

uiuc_warnings_errors(1, *command_line);

3124

3125

if (token_value_convert1 < -1000 || token_value_convert1 > 1000)

3126

uiuc_warnings_errors(1, *command_line);

3127

3128

if (fog_point_index == fog_segments || fog_point_index == -1)

3129

uiuc_warnings_errors(1, *command_line);

3130

3131

fog_point_index++;

3132

fog_time[fog_point_index] = token_value;

3133

fog_value[fog_point_index] = token_value_convert1;

3134

3135

break;

3136

}

3137

default:

3138

{

3139

uiuc_warnings_errors(2, *command_line);

3140

break;

3141

}

3142

};

3143

break;

3144

} // end fog map

3145

3146

3147

3148

3149

3150

3151

case record_flag:

3152

{

3153

static int fout_flag=0;

3154

if (fout_flag==0)

3155

{

3156

fout_flag=-1;

3157

fout.open("uiuc_record.dat");

3158

}

3159

switch(record_map[linetoken2])

3160

{

3161

/************************* Time ************************/

3162

case Simtime_record:

3163

{

3164

recordParts -> storeCommands (*command_line);

3165

break;

3166

}

3167

case dt_record:

3168

{

3169

recordParts -> storeCommands (*command_line);

3170

break;

3171

}

3172

3173

/************************* Mass ************************/

3174

case Weight_record:

3175

{

3176

recordParts -> storeCommands (*command_line);

3177

break;

3178

}

3179

case Mass_record:

3180

{

3181

recordParts -> storeCommands (*command_line);

3182

break;

3183

}

3184

case I_xx_record:

3185

{

3186

recordParts -> storeCommands (*command_line);

3187

break;

3188

}

3189

case I_yy_record:

3190

{

3191

recordParts -> storeCommands (*command_line);

3192

break;

3193

}

3194

case I_zz_record:

3195

{

3196

recordParts -> storeCommands (*command_line);

3197

break;

3198

}

3199

case I_xz_record:

3200

{

3201

recordParts -> storeCommands (*command_line);

3202

break;

3203

}

3204

3205

/*********************** Geometry **********************/

3206

case Dx_pilot_record:

3207

{

3208

recordParts -> storeCommands (*command_line);

3209

break;

3210

}

3211

case Dy_pilot_record:

3212

{

3213

recordParts -> storeCommands (*command_line);

3214

break;

3215

}

3216

case Dz_pilot_record:

3217

{

3218

recordParts -> storeCommands (*command_line);

3219

break;

3220

}

3221

case Dx_cg_record:

3222

{

3223

recordParts -> storeCommands (*command_line);

3224

break;

3225

}

3226

case Dy_cg_record:

3227

{

3228

recordParts -> storeCommands (*command_line);

3229

break;

3230

}

3231

case Dz_cg_record:

3232

{

3233

recordParts -> storeCommands (*command_line);

3234

break;

3235

}

3236

3237

/********************** Positions **********************/

3238

case Lat_geocentric_record:

3239

{

3240

recordParts -> storeCommands (*command_line);

3241

break;

3242

}

3243

case Lon_geocentric_record:

3244

{

3245

recordParts -> storeCommands (*command_line);

3246

break;

3247

}

3248

case Radius_to_vehicle_record:

3249

{

3250

recordParts -> storeCommands (*command_line);

3251

break;

3252

}

3253

case Latitude_record:

3254

{

3255

recordParts -> storeCommands (*command_line);

3256

break;

3257

}

3258

case Longitude_record:

3259

{

3260

recordParts -> storeCommands (*command_line);

3261

break;

3262

}

3263

case Altitude_record:

3264

{

3265

recordParts -> storeCommands (*command_line);

3266

break;

3267

}

3268

case Phi_record:

3269

{

3270

recordParts -> storeCommands (*command_line);

3271

break;

3272

}

3273

case Theta_record:

3274

{

3275

recordParts -> storeCommands (*command_line);

3276

break;

3277

}

3278

case Psi_record:

3279

{

3280

recordParts -> storeCommands (*command_line);

3281

break;

3282

}

3283

3284

/******************** Accelerations ********************/

3285

case V_dot_north_record:

3286

{

3287

recordParts -> storeCommands (*command_line);

3288

break;

3289

}

3290

case V_dot_east_record:

3291

{

3292

recordParts -> storeCommands (*command_line);

3293

break;

3294

}

3295

case V_dot_down_record:

3296

{

3297

recordParts -> storeCommands (*command_line);

3298

break;

3299

}

3300

case U_dot_body_record:

3301

{

3302

recordParts -> storeCommands (*command_line);

3303

break;

3304

}

3305

case V_dot_body_record:

3306

{

3307

recordParts -> storeCommands (*command_line);

3308

break;

3309

}

3310

case W_dot_body_record:

3311

{

3312

recordParts -> storeCommands (*command_line);

3313

break;

3314

}

3315

case A_X_pilot_record:

3316

{

3317

recordParts -> storeCommands (*command_line);

3318

break;

3319

}

3320

case A_Y_pilot_record:

3321

{

3322

recordParts -> storeCommands (*command_line);

3323

break;

3324

}

3325

case A_Z_pilot_record:

3326

{

3327

recordParts -> storeCommands (*command_line);

3328

break;

3329

}

3330

case A_X_cg_record:

3331

{

3332

recordParts -> storeCommands (*command_line);

3333

break;

3334

}

3335

case A_Y_cg_record:

3336

{

3337

recordParts -> storeCommands (*command_line);

3338

break;

3339

}

3340

case A_Z_cg_record:

3341

{

3342

recordParts -> storeCommands (*command_line);

3343

break;

3344

}

3345

case N_X_pilot_record:

3346

{

3347

recordParts -> storeCommands (*command_line);

3348

break;

3349

}

3350

case N_Y_pilot_record:

3351

{

3352

recordParts -> storeCommands (*command_line);

3353

break;

3354

}

3355

case N_Z_pilot_record:

3356

{

3357

recordParts -> storeCommands (*command_line);

3358

break;

3359

}

3360

case N_X_cg_record:

3361

{

3362

recordParts -> storeCommands (*command_line);

3363

break;

3364

}

3365

case N_Y_cg_record:

3366

{

3367

recordParts -> storeCommands (*command_line);

3368

break;

3369

}

3370

case N_Z_cg_record:

3371

{

3372

recordParts -> storeCommands (*command_line);

3373

break;

3374

}

3375

case P_dot_body_record:

3376

{

3377

recordParts -> storeCommands (*command_line);

3378

break;

3379

}

3380

case Q_dot_body_record:

3381

{

3382

recordParts -> storeCommands (*command_line);

3383

break;

3384

}

3385

case R_dot_body_record:

3386

{

3387

recordParts -> storeCommands (*command_line);

3388

break;

3389

}

3390

3391

/********************** Velocities *********************/

3392

case V_north_record:

3393

{

3394

recordParts -> storeCommands (*command_line);

3395

break;

3396

}

3397

case V_east_record:

3398

{

3399

recordParts -> storeCommands (*command_line);

3400

break;

3401

}

3402

case V_down_record:

3403

{

3404

recordParts -> storeCommands (*command_line);

3405

break;

3406

}

3407

case V_north_rel_ground_record:

3408

{

3409

recordParts -> storeCommands (*command_line);

3410

break;

3411

}

3412

case V_east_rel_ground_record:

3413

{

3414

recordParts -> storeCommands (*command_line);

3415

break;

3416

}

3417

case V_down_rel_ground_record:

3418

{

3419

recordParts -> storeCommands (*command_line);

3420

break;

3421

}

3422

case V_north_airmass_record:

3423

{

3424

recordParts -> storeCommands (*command_line);

3425

break;

3426

}

3427

case V_east_airmass_record:

3428

{

3429

recordParts -> storeCommands (*command_line);

3430

break;

3431

}

3432

case V_down_airmass_record:

3433

{

3434

recordParts -> storeCommands (*command_line);

3435

break;

3436

}

3437

case V_north_rel_airmass_record:

3438

{

3439

recordParts -> storeCommands (*command_line);

3440

break;

3441

}

3442

case V_east_rel_airmass_record:

3443

{

3444

recordParts -> storeCommands (*command_line);

3445

break;

3446

}

3447

case V_down_rel_airmass_record:

3448

{

3449

recordParts -> storeCommands (*command_line);

3450

break;

3451

}

3452

case U_gust_record:

3453

{

3454

recordParts -> storeCommands (*command_line);

3455

break;

3456

}

3457

case V_gust_record:

3458

{

3459

recordParts -> storeCommands (*command_line);

3460

break;

3461

}

3462

case W_gust_record:

3463

{

3464

recordParts -> storeCommands (*command_line);

3465

break;

3466

}

3467

case U_body_record:

3468

{

3469

recordParts -> storeCommands (*command_line);

3470

break;

3471

}

3472

case V_body_record:

3473

{

3474

recordParts -> storeCommands (*command_line);

3475

break;

3476

}

3477

case W_body_record:

3478

{

3479

recordParts -> storeCommands (*command_line);

3480

break;

3481

}

3482

case V_rel_wind_record:

3483

{

3484

recordParts -> storeCommands (*command_line);

3485

break;

3486

}

3487

case V_true_kts_record:

3488

{

3489

recordParts -> storeCommands (*command_line);

3490

break;

3491

}

3492

case V_rel_ground_record:

3493

{

3494

recordParts -> storeCommands (*command_line);

3495

break;

3496

}

3497

case V_inertial_record:

3498

{

3499

recordParts -> storeCommands (*command_line);

3500

break;

3501

}

3502

case V_ground_speed_record:

3503

{

3504

recordParts -> storeCommands (*command_line);

3505

break;

3506

}

3507

case V_equiv_record:

3508

{

3509

recordParts -> storeCommands (*command_line);

3510

break;

3511

}

3512

case V_equiv_kts_record:

3513

{

3514

recordParts -> storeCommands (*command_line);

3515

break;

3516

}

3517

case V_calibrated_record:

3518

{

3519

recordParts -> storeCommands (*command_line);

3520

break;

3521

}

3522

case V_calibrated_kts_record:

3523

{

3524

recordParts -> storeCommands (*command_line);

3525

break;

3526

}

3527

case P_local_record:

3528

{

3529

recordParts -> storeCommands (*command_line);

3530

break;

3531

}

3532

case Q_local_record:

3533

{

3534

recordParts -> storeCommands (*command_line);

3535

break;

3536

}

3537

case R_local_record:

3538

{

3539

recordParts -> storeCommands (*command_line);

3540

break;

3541

}

3542

case P_body_record:

3543

{

3544

recordParts -> storeCommands (*command_line);

3545

break;

3546

}

3547

case Q_body_record:

3548

{

3549

recordParts -> storeCommands (*command_line);

3550

break;

3551

}

3552

case R_body_record:

3553

{

3554

recordParts -> storeCommands (*command_line);

3555

break;

3556

}

3557

case P_total_record:

3558

{

3559

recordParts -> storeCommands (*command_line);

3560

break;

3561

}

3562

case Q_total_record:

3563

{

3564

recordParts -> storeCommands (*command_line);

3565

break;

3566

}

3567

case R_total_record:

3568

{

3569

recordParts -> storeCommands (*command_line);

3570

break;

3571

}

3572

case Phi_dot_record:

3573

{

3574

recordParts -> storeCommands (*command_line);

3575

break;

3576

}

3577

case Theta_dot_record:

3578

{

3579

recordParts -> storeCommands (*command_line);

3580

break;

3581

}

3582

case Psi_dot_record:

3583

{

3584

recordParts -> storeCommands (*command_line);

3585

break;

3586

}

3587

case Latitude_dot_record:

3588

{

3589

recordParts -> storeCommands (*command_line);

3590

break;

3591

}

3592

case Longitude_dot_record:

3593

{

3594

recordParts -> storeCommands (*command_line);

3595

break;

3596

}

3597

case Radius_dot_record:

3598

{

3599

recordParts -> storeCommands (*command_line);

3600

break;

3601

}

3602

3603

/************************ Angles ***********************/

3604

case Alpha_record:

3605

{

3606

recordParts -> storeCommands (*command_line);

3607

break;

3608

}

3609

case Alpha_deg_record:

3610

{

3611

recordParts -> storeCommands (*command_line);

3612

break;

3613

}

3614

case Alpha_dot_record:

3615

{

3616

recordParts -> storeCommands (*command_line);

3617

break;

3618

}

3619

case Alpha_dot_deg_record:

3620

{

3621

recordParts -> storeCommands (*command_line);

3622

break;

3623

}

3624

case Beta_record:

3625

{

3626

recordParts -> storeCommands (*command_line);

3627

break;

3628

}

3629

case Beta_deg_record:

3630

{

3631

recordParts -> storeCommands (*command_line);

3632

break;

3633

}

3634

case Beta_dot_record:

3635

{

3636

recordParts -> storeCommands (*command_line);

3637

break;

3638

}

3639

case Beta_dot_deg_record:

3640

{

3641

recordParts -> storeCommands (*command_line);

3642

break;

3643

}

3644

case Gamma_vert_record:

3645

{

3646

recordParts -> storeCommands (*command_line);

3647

break;

3648

}

3649

case Gamma_vert_deg_record:

3650

{

3651

recordParts -> storeCommands (*command_line);

3652

break;

3653

}

3654

case Gamma_horiz_record:

3655

{

3656

recordParts -> storeCommands (*command_line);

3657

break;

3658

}

3659

case Gamma_horiz_deg_record:

3660

{

3661

recordParts -> storeCommands (*command_line);

3662

break;

3663

}

3664

3665

/**************** Atmospheric Properties ***************/

3666

case Density_record:

3667

{

3668

recordParts -> storeCommands (*command_line);

3669

break;

3670

}

3671

case V_sound_record:

3672

{

3673

recordParts -> storeCommands (*command_line);

3674

break;

3675

}

3676

case Mach_number_record:

3677

{

3678

recordParts -> storeCommands (*command_line);

3679

break;

3680

}

3681

case Static_pressure_record:

3682

{

3683

recordParts -> storeCommands (*command_line);

3684

break;

3685

}

3686

case Total_pressure_record:

3687

{

3688

recordParts -> storeCommands (*command_line);

3689

break;

3690

}

3691

case Impact_pressure_record:

3692

{

3693

recordParts -> storeCommands (*command_line);

3694

break;

3695

}

3696

case Dynamic_pressure_record:

3697

{

3698

recordParts -> storeCommands (*command_line);

3699

break;

3700

}

3701

case Static_temperature_record:

3702

{

3703

recordParts -> storeCommands (*command_line);

3704

break;

3705

}

3706

case Total_temperature_record:

3707

{

3708

recordParts -> storeCommands (*command_line);

3709

break;

3710

}

3711

3712

/******************** Earth Properties *****************/

3713

case Gravity_record:

3714

{

3715

recordParts -> storeCommands (*command_line);

3716

break;

3717

}

3718

case Sea_level_radius_record:

3719

{

3720

recordParts -> storeCommands (*command_line);

3721

break;

3722

}

3723

case Earth_position_angle_record:

3724

{

3725

recordParts -> storeCommands (*command_line);

3726

break;

3727

}

3728

case Runway_altitude_record:

3729

{

3730

recordParts -> storeCommands (*command_line);

3731

break;

3732

}

3733

case Runway_latitude_record:

3734

{

3735

recordParts -> storeCommands (*command_line);

3736

break;

3737

}

3738

case Runway_longitude_record:

3739

{

3740

recordParts -> storeCommands (*command_line);

3741

break;

3742

}

3743

case Runway_heading_record:

3744

{

3745

recordParts -> storeCommands (*command_line);

3746

break;

3747

}

3748

case Radius_to_rwy_record:

3749

{

3750

recordParts -> storeCommands (*command_line);

3751

break;

3752

}

3753

case D_pilot_north_of_rwy_record:

3754

{

3755

recordParts -> storeCommands (*command_line);

3756

break;

3757

}

3758

case D_pilot_east_of_rwy_record:

3759

{

3760

recordParts -> storeCommands (*command_line);

3761

break;

3762

}

3763

case D_pilot_above_rwy_record:

3764

{

3765

recordParts -> storeCommands (*command_line);

3766

break;

3767

}

3768

case X_pilot_rwy_record:

3769

{

3770

recordParts -> storeCommands (*command_line);

3771

break;

3772

}

3773

case Y_pilot_rwy_record:

3774

{

3775

recordParts -> storeCommands (*command_line);

3776

break;

3777

}

3778

case H_pilot_rwy_record:

3779

{

3780

recordParts -> storeCommands (*command_line);

3781

break;

3782

}

3783

case D_cg_north_of_rwy_record:

3784

{

3785

recordParts -> storeCommands (*command_line);

3786

break;

3787

}

3788

case D_cg_east_of_rwy_record:

3789

{

3790

recordParts -> storeCommands (*command_line);

3791

break;

3792

}

3793

case D_cg_above_rwy_record:

3794

{

3795

recordParts -> storeCommands (*command_line);

3796

break;

3797

}

3798

case X_cg_rwy_record:

3799

{

3800

recordParts -> storeCommands (*command_line);

3801

break;

3802

}

3803

case Y_cg_rwy_record:

3804

{

3805

recordParts -> storeCommands (*command_line);

3806

break;

3807

}

3808

case H_cg_rwy_record:

3809

{

3810

recordParts -> storeCommands (*command_line);

3811

break;

3812

}

3813

3814

/********************* Engine Inputs *******************/

3815

case Throttle_pct_record:

3816

{

3817

recordParts -> storeCommands (*command_line);

3818

break;

3819

}

3820

case Throttle_3_record:

3821

{

3822

recordParts -> storeCommands (*command_line);

3823

break;

3824

}

3825

3826

/******************** Control Inputs *******************/

3827

case Long_control_record:

3828

{

3829

recordParts -> storeCommands (*command_line);

3830

break;

3831

}

3832

case Long_trim_record:

3833

{

3834

recordParts -> storeCommands (*command_line);

3835

break;

3836

}

3837

case Long_trim_deg_record:

3838

{

3839

recordParts -> storeCommands (*command_line);

3840

break;

3841

}

3842

case elevator_record:

3843

{

3844

recordParts -> storeCommands (*command_line);

3845

break;

3846

}

3847

case elevator_deg_record:

3848

{

3849

recordParts -> storeCommands (*command_line);

3850

break;

3851

}

3852

case Lat_control_record:

3853

{

3854

recordParts -> storeCommands (*command_line);

3855

break;

3856

}

3857

case aileron_record:

3858

{

3859

recordParts -> storeCommands (*command_line);

3860

break;

3861

}

3862

case aileron_deg_record:

3863

{

3864

recordParts -> storeCommands (*command_line);

3865

break;

3866

}

3867

case Rudder_pedal_record:

3868

{

3869

recordParts -> storeCommands (*command_line);

3870

break;

3871

}

3872

case rudder_record:

3873

{

3874

recordParts -> storeCommands (*command_line);

3875

break;

3876

}

3877

case rudder_deg_record:

3878

{

3879

recordParts -> storeCommands (*command_line);

3880

break;

3881

}

3882

case Flap_handle_record:

3883

{

3884

recordParts -> storeCommands (*command_line);

3885

break;

3886

}

3887

case flap_record:

3888

{

3889

recordParts -> storeCommands (*command_line);

3890

break;

3891

}

3892

case flap_deg_record:

3893

{

3894

recordParts -> storeCommands (*command_line);

3895

break;

3896

}

3897

3898

/****************** Aero Coefficients ******************/

3899

case CD_record:

3900

{

3901

recordParts -> storeCommands (*command_line);

3902

break;

3903

}

3904

case CDfaI_record:

3905

{

3906

recordParts -> storeCommands (*command_line);

3907

break;

3908

}

3909

case CDfadeI_record:

3910

{

3911

recordParts -> storeCommands (*command_line);

3912

break;

3913

}

3914

case CDfdfI_record:

3915

{

3916

recordParts -> storeCommands (*command_line);

3917

break;

3918

}

3919

case CDfadfI_record:

3920

{

3921

recordParts -> storeCommands (*command_line);

3922

break;

3923

}

3924

case CX_record:

3925

{

3926

recordParts -> storeCommands (*command_line);

3927

break;

3928

}

3929

case CL_record:

3930

{

3931

recordParts -> storeCommands (*command_line);

3932

break;

3933

}

3934

case CLfaI_record:

3935

{

3936

recordParts -> storeCommands (*command_line);

3937

break;

3938

}

3939

case CLfadeI_record:

3940

{

3941

recordParts -> storeCommands (*command_line);

3942

break;

3943

}

3944

case CLfdfI_record:

3945

{

3946

recordParts -> storeCommands (*command_line);

3947

break;

3948

}

3949

case CLfadfI_record:

3950

{

3951

recordParts -> storeCommands (*command_line);

3952

break;

3953

}

3954

case CZ_record:

3955

{

3956

recordParts -> storeCommands (*command_line);

3957

break;

3958

}

3959

case Cm_record:

3960

{

3961

recordParts -> storeCommands (*command_line);

3962

break;

3963

}

3964

case CmfaI_record:

3965

{

3966

recordParts -> storeCommands (*command_line);

3967

break;

3968

}

3969

case CmfadeI_record:

3970

{

3971

recordParts -> storeCommands (*command_line);

3972

break;

3973

}

3974

case CmfdfI_record:

3975

{

3976

recordParts -> storeCommands (*command_line);

3977

break;

3978

}

3979

case CmfadfI_record:

3980

{

3981

recordParts -> storeCommands (*command_line);

3982

break;

3983

}

3984

case CY_record:

3985

{

3986

recordParts -> storeCommands (*command_line);

3987

break;

3988

}

3989

case CYfadaI_record:

3990

{

3991

recordParts -> storeCommands (*command_line);

3992

break;

3993

}

3994

case CYfbetadrI_record:

3995

{

3996

recordParts -> storeCommands (*command_line);

3997

break;

3998

}

3999

case Cl_record:

4000

{

4001

recordParts -> storeCommands (*command_line);

4002

break;

4003

}

4004

case ClfadaI_record:

4005

{

4006

recordParts -> storeCommands (*command_line);

4007

break;

4008

}

4009

case ClfbetadrI_record:

4010

{

4011

recordParts -> storeCommands (*command_line);

4012

break;

4013

}

4014

case Cn_record:

4015

{

4016

recordParts -> storeCommands (*command_line);

4017

break;

4018

}

4019

case CnfadaI_record:

4020

{

4021

recordParts -> storeCommands (*command_line);

4022

break;

4023

}

4024

case CnfbetadrI_record:

4025

{

4026

recordParts -> storeCommands (*command_line);

4027

break;

4028

}

4029

4030

/******************** Ice Detection ********************/

4031

case CLclean_wing_record:

4032

{

4033

recordParts -> storeCommands (*command_line);

4034

break;

4035

}

4036

case CLiced_wing_record:

4037

{

4038

recordParts -> storeCommands (*command_line);

4039

break;

4040

}

4041

case CLclean_tail_record:

4042

{

4043

recordParts -> storeCommands (*command_line);

4044

break;

4045

}

4046

case CLiced_tail_record:

4047

{

4048

recordParts -> storeCommands (*command_line);

4049

break;

4050

}

4051

case Lift_clean_wing_record:

4052

{

4053

recordParts -> storeCommands (*command_line);

4054

break;

4055

}

4056

case Lift_iced_wing_record:

4057

{

4058

recordParts -> storeCommands (*command_line);

4059

break;

4060

}

4061

case Lift_clean_tail_record:

4062

{

4063

recordParts -> storeCommands (*command_line);

4064

break;

4065

}

4066

case Lift_iced_tail_record:

4067

{

4068

recordParts -> storeCommands (*command_line);

4069

break;

4070

}

4071

case Gamma_clean_wing_record:

4072

{

4073

recordParts -> storeCommands (*command_line);

4074

break;

4075

}

4076

case Gamma_iced_wing_record:

4077

{

4078

recordParts -> storeCommands (*command_line);

4079

break;

4080

}

4081

case Gamma_clean_tail_record:

4082

{

4083

recordParts -> storeCommands (*command_line);

4084

break;

4085

}

4086

case Gamma_iced_tail_record:

4087

{

4088

recordParts -> storeCommands (*command_line);

4089

break;

4090

}

4091

case w_clean_wing_record:

4092

{

4093

recordParts -> storeCommands (*command_line);

4094

break;

4095

}

4096

case w_iced_wing_record:

4097

{

4098

recordParts -> storeCommands (*command_line);

4099

break;

4100

}

4101

case w_clean_tail_record:

4102

{

4103

recordParts -> storeCommands (*command_line);

4104

break;

4105

}

4106

case w_iced_tail_record:

4107

{

4108

recordParts -> storeCommands (*command_line);

4109

break;

4110

}

4111

case V_total_clean_wing_record:

4112

{

4113

recordParts -> storeCommands (*command_line);

4114

break;

4115

}

4116

case V_total_iced_wing_record:

4117

{

4118

recordParts -> storeCommands (*command_line);

4119

break;

4120

}

4121

case V_total_clean_tail_record:

4122

{

4123

recordParts -> storeCommands (*command_line);

4124

break;

4125

}

4126

case V_total_iced_tail_record:

4127

{

4128

recordParts -> storeCommands (*command_line);

4129

break;

4130

}

4131

case beta_flow_clean_wing_record:

4132

{

4133

recordParts -> storeCommands (*command_line);

4134

break;

4135

}

4136

case beta_flow_clean_wing_deg_record:

4137

{

4138

recordParts -> storeCommands (*command_line);

4139

break;

4140

}

4141

case beta_flow_iced_wing_record:

4142

{

4143

recordParts -> storeCommands (*command_line);

4144

break;

4145

}

4146

case beta_flow_iced_wing_deg_record:

4147

{

4148

recordParts -> storeCommands (*command_line);

4149

break;

4150

}

4151

case beta_flow_clean_tail_record:

4152

{

4153

recordParts -> storeCommands (*command_line);

4154

break;

4155

}

4156

case beta_flow_clean_tail_deg_record:

4157

{

4158

recordParts -> storeCommands (*command_line);

4159

break;

4160

}

4161

case beta_flow_iced_tail_record:

4162

{

4163

recordParts -> storeCommands (*command_line);

4164

break;

4165

}

4166

case beta_flow_iced_tail_deg_record:

4167

{

4168

recordParts -> storeCommands (*command_line);

4169

break;

4170

}

4171

case Dbeta_flow_wing_record:

4172

{

4173

recordParts -> storeCommands (*command_line);

4174

break;

4175

}

4176

case Dbeta_flow_wing_deg_record:

4177

{

4178

recordParts -> storeCommands (*command_line);

4179

break;

4180

}

4181

case Dbeta_flow_tail_record:

4182

{

4183

recordParts -> storeCommands (*command_line);

4184

break;

4185

}

4186

case Dbeta_flow_tail_deg_record:

4187

{

4188

recordParts -> storeCommands (*command_line);

4189

break;

4190

}

4191

case pct_beta_flow_wing_record:

4192

{

4193

recordParts -> storeCommands (*command_line);

4194

break;

4195

}

4196

case pct_beta_flow_tail_record:

4197

{

4198

recordParts -> storeCommands (*command_line);

4199

break;

4200

}

4201

4202

/************************ Forces ***********************/

4203

case F_X_wind_record:

4204

{

4205

recordParts -> storeCommands (*command_line);

4206

break;

4207

}

4208

case F_Y_wind_record:

4209

{

4210

recordParts -> storeCommands (*command_line);

4211

break;

4212

}

4213

case F_Z_wind_record:

4214

{

4215

recordParts -> storeCommands (*command_line);

4216

break;

4217

}

4218

case F_X_aero_record:

4219

{

4220

recordParts -> storeCommands (*command_line);

4221

break;

4222

}

4223

case F_Y_aero_record:

4224

{

4225

recordParts -> storeCommands (*command_line);

4226

break;

4227

}

4228

case F_Z_aero_record:

4229

{

4230

recordParts -> storeCommands (*command_line);

4231

break;

4232

}

4233

case F_X_engine_record:

4234

{

4235

recordParts -> storeCommands (*command_line);

4236

break;

4237

}

4238

case F_Y_engine_record:

4239

{

4240

recordParts -> storeCommands (*command_line);

4241

break;

4242

}

4243

case F_Z_engine_record:

4244

{

4245

recordParts -> storeCommands (*command_line);

4246

break;

4247

}

4248

case F_X_gear_record:

4249

{

4250

recordParts -> storeCommands (*command_line);

4251

break;

4252

}

4253

case F_Y_gear_record:

4254

{

4255

recordParts -> storeCommands (*command_line);

4256

break;

4257

}

4258

case F_Z_gear_record:

4259

{

4260

recordParts -> storeCommands (*command_line);

4261

break;

4262

}

4263

case F_X_record:

4264

{

4265

recordParts -> storeCommands (*command_line);

4266

break;

4267

}

4268

case F_Y_record:

4269

{

4270

recordParts -> storeCommands (*command_line);

4271

break;

4272

}

4273

case F_Z_record:

4274

{

4275

recordParts -> storeCommands (*command_line);

4276

break;

4277

}

4278

case F_north_record:

4279

{

4280

recordParts -> storeCommands (*command_line);

4281

break;

4282

}

4283

case F_east_record:

4284

{

4285

recordParts -> storeCommands (*command_line);

4286

break;

4287

}

4288

case F_down_record:

4289

{

4290

recordParts -> storeCommands (*command_line);

4291

break;

4292

}

4293

4294

/*********************** Moments ***********************/

4295

case M_l_aero_record:

4296

{

4297

recordParts -> storeCommands (*command_line);

4298

break;

4299

}

4300

case M_m_aero_record:

4301

{

4302

recordParts -> storeCommands (*command_line);

4303

break;

4304

}

4305

case M_n_aero_record:

4306

{

4307

recordParts -> storeCommands (*command_line);

4308

break;

4309

}

4310

case M_l_engine_record:

4311

{

4312

recordParts -> storeCommands (*command_line);

4313

break;

4314

}

4315

case M_m_engine_record:

4316

{

4317

recordParts -> storeCommands (*command_line);

4318

break;

4319

}

4320

case M_n_engine_record:

4321

{

4322

recordParts -> storeCommands (*command_line);

4323

break;

4324

}

4325

case M_l_gear_record:

4326

{

4327

recordParts -> storeCommands (*command_line);

4328

break;

4329

}

4330

case M_m_gear_record:

4331

{

4332

recordParts -> storeCommands (*command_line);

4333

break;

4334

}

4335

case M_n_gear_record:

4336

{

4337

recordParts -> storeCommands (*command_line);

4338

break;

4339

}

4340

case M_l_rp_record:

4341

{

4342

recordParts -> storeCommands (*command_line);

4343

break;

4344

}

4345

case M_m_rp_record:

4346

{

4347

recordParts -> storeCommands (*command_line);

4348

break;

4349

}

4350

case M_n_rp_record:

4351

{

4352

recordParts -> storeCommands (*command_line);

4353

break;

4354

}

4355

default:

4356

{

4357

uiuc_warnings_errors(2, *command_line);

4358

break;

4359

}

4360

};

4361

break;

4362

} // end record map

4363

4364

4365

case misc_flag:

4366

{

4367

switch(misc_map[linetoken2])

4368

{

4369

case simpleHingeMomentCoef_flag:

4370

{

4371

if (check_float(linetoken3))

4372

token3 >> token_value;

4373

else

4374

uiuc_warnings_errors(1, *command_line);

4375

4376

simpleHingeMomentCoef = token_value;

4377

break;

4378

}

4379

case dfTimefdf_flag:

4380

{

4381

dfTimefdf = linetoken3;

4382

/* call 1D File Reader with file name (dfTimefdf);

4383

function returns array of dfs (dfArray) and

4384

corresponding time values (TimeArray) and max

4385

number of terms in arrays (ndf) */

4386

uiuc_1DdataFileReader(dfTimefdf,

4387

dfTimefdf_dfArray,

4388

dfTimefdf_TimeArray,

4389

dfTimefdf_ndf);

4390

break;

4391

}

4392

default:

4393

{

4394

uiuc_warnings_errors(2, *command_line);

4395

break;

4396

}

4397

};

4398

break;

4399

} // end misc map

4400

4401

4402

default:

4403

{

4404

if (linetoken1=="*")

4405

return;

4406

uiuc_warnings_errors(2, *command_line);

4407

break;

4408

}

4409

};

4410

} // end keyword map

4411

4412

delete airplane;

4413

}

4414

4415

// end menu.cpp

Older »