This run is for testing the C172 altitude hold autopilot and cruise performance
simulation/run_id
simulation/sim-time-sec ge 0.0
simulation/run_id
0.0
-36.0
36.0
simulation/sim-time-sec ge 0.01
simulation/sim-time-sec gt 1.0
velocities/u-aero-fps
velocities/v-aero-fps
velocities/w-aero-fps
attitude/psi-rad
attitude/theta-rad
attitude/phi-rad
position/h-agl-ft
accelerations/pdot-rad_sec2
accelerations/qdot-rad_sec2
accelerations/rdot-rad_sec2
propulsion/engine/thrust-lbs
propulsion/engine/propeller-rpm
velocities/p-rad_sec
velocities/q-rad_sec
velocities/r-rad_sec
fcs/elevator-cmd-norm
fcs/aileron-cmd-norm
fcs/rudder-cmd-norm
fcs/elevator-pos-norm
fcs/right-aileron-pos-norm
fcs/rudder-pos-norm
fcs/throttle-pos-norm[0]
fcs/mixture-pos-norm[0]
inertia/weight-lbs
velocities/vc-kts
velocities/ve-kts
velocities/vtrue-kts
atmosphere/T-R
propulsion/engine/fuel-flow-rate-gph
propulsion/engine/power-hp
simulation/sim-time-sec ge 5
simulation/sim-time-sec ge 10
simulation/sim-time-sec >= 30.0
simulation/terminate != 1
simulation/run_id
simulation/run_id ge 3
simulation/terminate