WOLFRAM SYSTEM MODELER
CircularOrbitSpace shuttle in a circular orbit under Kepler dynamics |
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SystemModel["DocumentationExamples.Control.CircularOrbit"]
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.
omega |
Value: 0.0011 Type: Real Description: Angular velocity in default circular orbit |
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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 |
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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 |
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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 |