WOLFRAM SYSTEM MODELER

MotionSignalBus

Bus for the real signals of the linear and angular velocity perturbations resolved in the body frame

Wolfram Language

In[1]:=
SystemModel["Aircraft.StateSpace.FixedWing.Interfaces.MotionSignalBus"]
Out[1]:=

Information

This expandable connector works as a bus for the real signals of the linear and angular velocity perturbations from reference flight condition values resolved in the body frame.

Connector Variables (6)

Du

Causality: None

Type: Velocity (m/s)

Description: Velocity u-component perturbation

Dv

Causality: None

Type: Velocity (m/s)

Description: Velocity v-component perturbation

Dw

Causality: None

Type: Velocity (m/s)

Description: Velocity w-component perturbation

Dp

Causality: None

Type: AngularVelocity (rad/s)

Description: Roll rate perturbation

Dq

Causality: None

Type: AngularVelocity (rad/s)

Description: Pitch rate perturbation

Dr

Causality: None

Type: AngularVelocity (rad/s)

Description: Yaw rate perturbation

Used in Components (4)

DefaultAircraft

Aircraft.StateSpace.FixedWing

Aircraft model using state-space representation

LongitudinalMotion

Aircraft.StateSpace.FixedWing.Blocks

State space representation of longitudinal motion

LateralMotion

Aircraft.StateSpace.FixedWing.Blocks

State space representation of lateral motion

PositionAndOrientation

Aircraft.StateSpace.FixedWing.Blocks

Calculates the position, orientation and velocities of the aircraft in the world frame