setupControlStates

Class: Aero.FixedWing.State
Namespace: Aero

Set up control states for Aero.FixedWing.State object

Since R2021a

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Syntax

state = setupControlStates(aircraft, state)

Description

state = setupControlStates(aircraft, state) sets up initial control states for the Aero.FixedWing object.

Input Arguments

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Aero.FixedWing object, specified as a scalar.

Data Types: double

Aero.FixedWing.State object, specified as a scalar.

Output Arguments

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Modified Aero.FixedWing.State object, returned as a scalar.

Data Types: double

Examples

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Open Live Script

This example shows how to initialize the control and command states on a cruise state.

[C182, CruiseState] = astC182();
CruiseState = setupControlStates(CruiseState,C182)
CruiseState = 
  State with properties:

                    Alpha: 0
                     Beta: 0
                 AlphaDot: 0
                  BetaDot: 0
                     Mass: 82.2981
                  Inertia: [3×3 table]
          CenterOfGravity: [1.2936 0 0]
         CenterOfPressure: [1.2250 0 0]
              AltitudeMSL: 5000
             GroundHeight: 0
                       XN: 0
                       XE: 0
                       XD: -5000
                        U: 220.1000
                        V: 0
                        W: 0
                      Phi: 0
                    Theta: -0.0073
                      Psi: 0
                        P: 0
                        Q: 0
                        R: 0
                   Weight: 2.6488e+03
              AltitudeAGL: 5000
                 Airspeed: 220.1000
              GroundSpeed: 220.1000
               MachNumber: 0.2006
             BodyVelocity: [220.1000 0 0]
           GroundVelocity: [220.1000 0 0]
                       Ur: 220.1000
                       Vr: 0
                       Wr: 0
          FlightPathAngle: 0
              CourseAngle: 0
     InertialToBodyMatrix: [3×3 double]
     BodyToInertialMatrix: [3×3 double]
         BodyToWindMatrix: [3×3 double]
         WindToBodyMatrix: [3×3 double]
    BodyToStabilityMatrix: [3×3 double]
    StabilityToBodyMatrix: [3×3 double]
          DynamicPressure: 49.6090
              Environment: [1×1 Aero.Aircraft.Environment]
            ControlStates: [1×4 Aero.Aircraft.ControlState]
         OutOfRangeAction: "Limit"
         DiagnosticAction: "Warning"
               Properties: [1×1 Aero.Aircraft.Properties]
               UnitSystem: "English (ft/s)"
        TemperatureSystem: "Fahrenheit"
              AngleSystem: "Radians"

Version History

Introduced in R2021a

See Also

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