WOLFRAM SYSTEM MODELER
SatelliteMassModels the mass of the satellite |
SystemModel["EducationExamples.AerospaceEngineering.Satellite.Components.SatelliteMass"]
frame_a |
Type: Frame_a Description: Coordinate system fixed to the component with one cut-force and cut-torque (filled rectangular icon) |
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satellite |
Type: Body Description: Rigid body with mass, inertia tensor and one frame connector (12 potential states) |
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EducationExamples.AerospaceEngineering.Satellite Model scenario of the launch and flight of a satellite. |