WOLFRAM SYSTEM MODELER
AutopilotGliderAutopilot for gliders |
SystemModel["Aircraft.ControlSystems.Autopilots.AutopilotGlider"]
This autopilot model extends the AutopilotBase model and is adjusted to work with gliders.
nEng |
Value: 1 Type: Integer Description: Number of engines to control |
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elvControl |
Value: true Type: Boolean Description: true, if elevator is controlled |
throtControl |
Value: false Type: Boolean Description: true, if throttle is controlled |
ailControl |
Value: true Type: Boolean Description: true, if ailerons are controlled |
rdrControl |
Value: true Type: Boolean Description: true, if rudder is controlled |
maxPhi |
Value: 0.349065850398866 Type: Angle (rad) Description: Maximum roll angle |
maxTheta |
Value: 0.349065850398866 Type: Angle (rad) Description: Maximum pitch angle |
altPIDk |
Value: 0.025 Type: Real Description: Altitude PID Gain |
altPIDTi |
Value: 4.5 Type: Time (s) Description: Altitude PID Integrator Block |
altPIDTd |
Value: 0.9 Type: Time (s) Description: Altitude PID Derivative Block |
thetaPIDk |
Value: 1.5 Type: Real Description: Theta PID Gain |
thetaPIDTi |
Value: 1.4 Type: Time (s) Description: Theta PID Integrator Block |
thetaPIDTd |
Value: 0.27 Type: Time (s) Description: Theta PID Derivative Block |
vtotPIDk |
Value: 0.17 Type: Real Description: Velocity PID Gain |
vtotPIDTi |
Value: 50 Type: Time (s) Description: Velocity PID Integrator Block |
vtotPIDTd |
Value: 0.5 Type: Time (s) Description: Velocity PID Derivative Block |
trackPIDk |
Value: 0.75 Type: Real Description: Track PID Gain |
trackPIDTi |
Value: 6000 Type: Time (s) Description: Track PID Integrator Block |
trackPIDTd |
Value: 0.4 Type: Time (s) Description: Track PID Derivative Block |
phiPIDk |
Value: 1.35 Type: Real Description: Phi PID Gain |
phiPIDTi |
Value: 20 Type: Time (s) Description: Phi PID Integrator Block |
phiPIDTd |
Value: 0.95 Type: Time (s) Description: Phi PID Derivative Block |
betaPIDk |
Value: 0.12 Type: Real Description: Beta PID Gain |
betaPIDTi |
Value: 0.5 Type: Time (s) Description: Beta PID Integrator Block |
betaPIDTd |
Value: 0.9 Type: Time (s) Description: Beta PID Derivative Block |
deltaElvCmd |
Type: RealOutput Description: Elevator deflection command |
|
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deltaThrotCmd |
Type: RealOutput[nEng] Description: Throttle position command |
|
altCmd |
Type: RealInput Description: Altitude command |
|
vTotCmd |
Type: RealInput Description: Total velocity command |
|
deltaRdrCmd |
Type: RealOutput Description: Rudder deflection command |
|
deltaAilCmd |
Type: RealOutput Description: Aileron deflection command |
|
trackCmd |
Type: RealInput Description: Track command |
|
flightDataIn |
Type: FlightDataIn Description: Flight data input |
altPID |
Type: LimPID Description: PID controller from altitude command to pitch angle (theta) command |
|
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vtotPID |
Type: LimPID Description: PID controller from total velocity command to throttle position command |
|
trackPID |
Type: LimPID Description: PID controller from track angle command to roll angle (phi) command |
|
betaPID |
Type: LimPID Description: PID controller from sideslip angle command to rudder deflection command |
|
phiPID |
Type: LimPID Description: PID controller from roll angle (phi) command to aileron deflection command |
|
thetaPID |
Type: LimPID Description: PID controller from pitch angle (theta) command to elevator deflection command |
|
constBeta |
Type: Constant Description: Constant 0 signal to Beta PID setpoint input |
|
deltaElvSignChange |
Type: Gain Description: Sign change for elevator deflection command |
Aircraft.Examples Example of towing a glider up to cruise altitude by an electric aircraft |