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Controlled airship simulation with autopilot and feedback control.
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Form:
p = AirshipControlSim( latLon, h0, v0, psi0, theta0, trajDes );
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Inputs
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latLon (1,2) Initial latitude & longitude [deg]
- Or, you may supply the string name of a U.S. city.
- Type "help LatLon" for more information.
h0 (1) Initial altitude [km]
v0 (1) Initial velocity [m/s]
psi0 (1) Initial heading angle [deg]
theta0 (1) Initial flight-path angle [deg]
trajDes (.) Data structure containing desired trajectory.
Has the following fields:
.vel (1,N) Time-history of desired velocity [m/s]
.psi (1,N) Time-history of desired heading angle [deg]
.theta (1,N) Time-history of desired flight-path angle [deg]
.dT (1) Time-step used in desired trajectory [sec]
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Outputs
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p (.) Structure with time-histories of recorded simulation data
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