WOLFRAM SYSTEM MODELER
VectoredThrustAircraftSimplified model of a rockect with vectored thrust |
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Diagram
Wolfram Language
In[1]:=
SystemModel["DocumentationExamples.Control.VectoredThrustAircraft"]
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Information
Wolfram Language Documentation Examples
This library contains models used in the documentation of system modeling functionality in Wolfram Language. These examples and this library can be explored in the Wolfram Language documentation.
Parameters (3)
| uniformSizeScale |
Value: 1 Type: Real Description: Factor by which dimensions of rocket are rescaled |
|---|---|
| r |
Value: 34 * uniformSizeScale Type: Distance (m) Description: Distance from point of application of tangential thrust to center of mass |
| d |
Value: 1 Type: TranslationalDampingConstant (N·s/m) Description: Linear air resistance constant |
Connectors (5)
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fv |
Type: RealInput Description: Vertical thrust in addition to weight compensation, resolved in the rocket frame |
|---|---|---|
|
ft |
Type: RealInput Description: Tangential thrust acting at distance r from the center of mass, resolved in the rocket frame |
|
fwind |
Type: RealInput Description: Wind force acting on the center of mass of the rocket in the direction of the y-axis, resolved in the laboratory frame |
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angles |
Type: RealOutput[3] Description: Euler angles from fixed to rocket frame |
|
z |
Type: RealOutput Description: Position of center of mass |
Components (11)
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world |
Type: World |
|---|---|---|
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fixedTranslation1 |
Type: FixedTranslation |
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force1 |
Type: WorldForce |
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force2 |
Type: WorldForce |
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linearAirResistance |
Type: LinearAirResistance |
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add |
Type: Add |
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const |
Type: Constant |
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rocket |
Type: Rocket |
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fixedTranslation2 |
Type: FixedTranslation |
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fixedShape1 |
Type: FixedShape |
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windForce |
Type: WorldForce |