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 |
|---|---|
| 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 |
|
|
Aircraft.StateSpace.FixedWing.Blocks Calculates longitudinal stability and control derivatives |
|
|
Aircraft.StateSpace.FixedWing.Blocks Calculates lateral stability and control derivatives |
|
|
Aircraft.StateSpace.FixedWing.Blocks State space representation of longitudinal motion |
|
|
Aircraft.StateSpace.FixedWing.Blocks State space representation of lateral motion |
|
|
Aircraft.StateSpace.FixedWing.Blocks Calculates the position, orientation and velocities of the aircraft in the world frame |
|
|
Aircraft.StateSpace.FixedWing.Blocks Calculates trimmed conditions for given flight conditions |