WOLFRAM SYSTEM MODELER

RefFlightSignalBus

Bus for the real signals of the reference flight conditions

Wolfram Language

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

Information

This expandable connector works as a bus for the real signals of the reference flight conditions.

Connector Variables (16)

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

Used in Components (7)

DefaultAircraft

Aircraft.StateSpace.FixedWing

Aircraft model using state-space representation

LongitudinalDerivatives

Aircraft.StateSpace.FixedWing.Blocks

Calculates longitudinal stability and control derivatives

LateralDerivatives

Aircraft.StateSpace.FixedWing.Blocks

Calculates lateral stability and control derivatives

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

TrimCalculator

Aircraft.StateSpace.FixedWing.Blocks

Calculates trimmed conditions for given flight conditions