WOLFRAM SYSTEM MODELER
CircularOrbitSpace shuttle in a circular orbit under Kepler dynamics |
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Diagram
Wolfram Language
In[1]:=
SystemModel["DocumentationExamples.Control.CircularOrbit"]
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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 (8)
| omega |
Value: 0.0011 Type: Real Description: Angular velocity in default circular orbit |
|---|---|
| G |
Value: Modelica.Constants.G Type: Real (m³/(kg·s²)) Description: Gravitational constant |
| M |
Value: 1000 Type: Mass (kg) Description: Mass of object at the center of trajectory |
| m |
Value: 1 Type: Mass (kg) Description: Mass of orbiting object |
| phi0 |
Value: 0 Type: Angle (rad) Description: Initial polar angle |
| bodyVolume |
Value: 55.52171636674795 * uniformSizeScale ^ 3 Type: Volume (m³) Description: Volume of the body |
| uniformDensity |
Value: 7700 Type: Density (kg/m³) Description: Uniform density of the body. If it is not provided, it defaults to 7.7 g.cm-3 |
| uniformSizeScale |
Value: 0.01 Type: Real Description: Factor by which dimensions of rocket are rescaled |
Connectors (4)
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fphi |
Type: RealInput Description: Dimensionless external tangential force |
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fr |
Type: RealInput Description: Dimensionless external radial force |
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dphi |
Type: RealOutput Description: Dimensionless deviation in the radial direction from circular orbit |
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dr |
Type: RealOutput Description: Dimensionless deviation in the tangential direction from circular orbit |
Components (5)
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keplerDynamics |
Type: KeplerDynamics |
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world |
Type: World |
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translation |
Type: Translation |
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shape |
Type: FixedShape |
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rotation |
Type: Rotation |