WOLFRAM SYSTEM MODELER
RefFlightSignalBusBus for the real signals of the reference flight conditions |
SystemModel["Aircraft.StateSpace.FixedWing.Interfaces.RefFlightSignalBus"]
This expandable connector works as a bus for the real signals of the reference flight conditions.
u0 |
Causality: None Type: Velocity (m/s) Description: Reference velocity u component |
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v0 |
Causality: None Type: Velocity (m/s) Description: Reference velocity v component |
w0 |
Causality: None Type: Velocity (m/s) Description: Reference velocity w component |
p0 |
Causality: None Type: AngularVelocity (rad/s) Description: Reference roll rate |
q0 |
Causality: None Type: AngularVelocity (rad/s) Description: Reference pitch rate |
r0 |
Causality: None Type: AngularVelocity (rad/s) Description: Reference yaw rate |
phi0 |
Causality: None Type: Angle (rad) Description: Reference roll angle |
theta0 |
Causality: None Type: Angle (rad) Description: Reference pitch angle |
psi0 |
Causality: None Type: Angle (rad) Description: Reference yaw angle |
h0 |
Causality: None Type: Height (m) Description: Reference altitude |
Vtot0 |
Causality: None Type: Velocity (m/s) Description: Reference total velocity |
deltaElv0 |
Causality: None Type: Angle (rad) Description: Reference elevator deflection |
deltaThrot0 |
Causality: None Type: DimensionlessRatio Description: Reference throttle setting |
TAvail0 |
Causality: None Type: Force (N) Description: Reference thrust available |
CL0 |
Causality: None Type: Real Description: Reference lift coefficient |
CD0 |
Causality: None Type: Real Description: Reference drag coefficient |
Aircraft.StateSpace.FixedWing Aircraft model using state-space representation |
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Aircraft.StateSpace.FixedWing.Blocks Calculates longitudinal stability and control derivatives |
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Aircraft.StateSpace.FixedWing.Blocks Calculates lateral stability and control derivatives |
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Aircraft.StateSpace.FixedWing.Blocks State space representation of longitudinal motion |
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Aircraft.StateSpace.FixedWing.Blocks State space representation of lateral motion |
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Aircraft.StateSpace.FixedWing.Blocks Calculates the position, orientation and velocities of the aircraft in the world frame |
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Aircraft.StateSpace.FixedWing.Blocks Calculates trimmed conditions for given flight conditions |