WOLFRAM SYSTEM MODELER
VectoredThrustAircraftSimplified model of a rockect with vectored thrust |
SystemModel["DocumentationExamples.Control.VectoredThrustAircraft"]
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.
uniformSizeScale |
Value: 1 Type: Real Description: Factor by which dimensions of rocket are rescaled |
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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 |
fv |
Type: RealInput Description: Vertical thrust in addition to weight compensation, resolved in the rocket frame |
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ft |
Type: RealInput Description: Tangential thrust acting at distance r from the center of mass, resolved in the rocket frame |
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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 |
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z |
Type: RealOutput Description: Position of center of mass |
world |
Type: World Description: World coordinate system + gravity field + default animation definition |
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fixedTranslation1 |
Type: FixedTranslation Description: Fixed translation of frame_b with respect to frame_a |
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force1 |
Type: WorldForce Description: External force acting at frame_b, defined by 3 input signals and resolved in frame world, frame_b or frame_resolve |
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force2 |
Type: WorldForce Description: External force acting at frame_b, defined by 3 input signals and resolved in frame world, frame_b or frame_resolve |
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linearAirResistance |
Type: LinearAirResistance Description: Linear air resistance |
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add |
Type: Add Description: Output the sum of the two inputs |
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const |
Type: Constant Description: Generate constant signal of type Real |
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rocket |
Type: Rocket Description: Body and shape for rocket |
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fixedTranslation2 |
Type: FixedTranslation Description: Fixed translation of frame_b with respect to frame_a |
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fixedShape1 |
Type: FixedShape Description: Visualizing an elementary shape with dynamically varying shape attributes (has one frame connector) |
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windForce |
Type: WorldForce Description: External force acting at frame_b, defined by 3 input signals and resolved in frame world, frame_b or frame_resolve |