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landing/code/.gitkeep

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landing/code/code/JSBout172B.csv

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+Time,P (deg/s),Q (deg/s),R (deg/s),P dot (deg/s^2),Q dot (deg/s^2),R dot (deg/s^2),P_{inertial} (deg/s),Q_{inertial} (deg/s),R_{inertial} (deg/s),q bar (psf),Reynolds Number,V_{Total} (ft/s),V_{Inertial} (ft/s),UBody,VBody,WBody,UdotBody,VdotBody,WdotBody,UdotBody_i,VdotBody_i,WdotBody_i,BodyAccel_X,BodyAccel_Y,BodyAccel_Z,Aero V_{X Body} (ft/s),Aero V_{Y Body} (ft/s),Aero V_{Z Body} (ft/s),V_{X_{inertial}} (ft/s),V_{Y_{inertial}} (ft/s),V_{Z_{inertial}} (ft/s),V_{X_{ecef}} (ft/s),V_{Y_{ecef}} (ft/s),V_{Z_{ecef}} (ft/s),V_{North} (ft/s),V_{East} (ft/s),V_{Down} (ft/s),I_{xx},I_{xy},I_{xz},I_{yx},I_{yy},I_{yz},I_{zx},I_{zy},I_{zz},Mass,Weight,X_{cg},Y_{cg},Z_{cg},Altitude ASL (ft),Altitude AGL (ft),Phi (deg),Theta (deg),Psi (deg),Q(1)_{LOCAL},Q(2)_{LOCAL},Q(3)_{LOCAL},Q(4)_{LOCAL},Q(1)_{ECEF},Q(2)_{ECEF},Q(3)_{ECEF},Q(4)_{ECEF},Q(1)_{ECI},Q(2)_{ECI},Q(3)_{ECI},Q(4)_{ECI},Alpha (deg),Beta (deg),Latitude (deg),Latitude Geodetic (deg),Longitude (deg),X_{ECI} (ft),Y_{ECI} (ft),Z_{ECI} (ft),X_{ECEF} (ft),Y_{ECEF} (ft),Z_{ECEF} (ft),Earth Position Angle (deg),Distance AGL (ft),Terrain Elevation (ft),navigation/actual-heading-rad,propulsion/tank[0]/contents-volume-gal,propulsion/tank[1]/contents-volume-gal,systems/mixture-cmd-norm,guidance/wp-heading-rad,guidance/wp-distance,guidance/wp-heading-deg,guidance/selected_target_heading,guidance/angle-to-heading-rad,ap/roll-control-autopilot-on,ap/roll-autopilot-windup-trigger,ap/limited-roll-angle-rad,ap/roll-attitude-selector,ap/limited-roll-angle-error,ap/roll-rate-pid-control,ap/total-limited-roll-rate,ap/roll-rate-saturation,ap/limited-roll-rate-error,ap/roll-command-pid-control,ap/roll-cmd-smoother,ap/roll-cmd-norm-output,ap/roll-command-selector-steering,fcs/attitude/sensor/phi-rad,fcs/wing-leveler-ap-on-off,fcs/roll-ap-error-pid,fcs/roll-ap-autoswitch,fcs/heading-true-degrees,fcs/heading-error,fcs/heading-error-bias-switch,fcs/heading-corrected,fcs/heading-command,fcs/heading-roll-error-lag,fcs/heading-roll-error,fcs/heading-roll-error-switch,fcs/heading-pi-controller,fcs/roll-command-selector,fcs/altitude-error,fcs/alt-error-lag,fcs/hdot-command,fcs/hdot-error,fcs/ap-alt-hold-switch,fcs/windup-trigger,fcs/altitude-hold-pid,fcs/elevator,fcs/pitch-trim-sum,fcs/elevator-control,fcs/elevator-actuator,fcs/roll-trim-sum,fcs/left-aileron-control,fcs/left-aileron-actuator,fcs/right-aileron-control,fcs/right-aileron-actuator,fcs/delta-aileron-pos,fcs/effective-aileron-pos,fcs/yaw-trim-sum,fcs/rudder-control,fcs/flaps-control,fcs/flap-position-normalizer,IO320 Power Available (engine 0 in ft-lbs/sec),IO320 HP (engine 0),IO320 equivalent ratio (engine 0),IO320 MAP (engine 0 in inHg),Fixed-Pitch 75-inch Two-Blade Propeller Torque (engine 0),Fixed-Pitch 75-inch Two-Blade Propeller PFactor Pitch (engine 0),Fixed-Pitch 75-inch Two-Blade Propeller PFactor Yaw (engine 0),Fixed-Pitch 75-inch Two-Blade Propeller Thrust (engine 0 in lbs),Fixed-Pitch 75-inch Two-Blade Propeller RPM (engine 0),Fuel Tank 0,Fuel Tank 1,/fdm/jsbsim/position/vrp-gc-latitude_deg,/fdm/jsbsim/position/vrp-longitude_deg,/fdm/jsbsim/position/vrp-radius-ft,velocities/pi-deg_sec
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