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VEGA satellite launcher control units

AMET > Case History > Aerospace > VEGA satellite launcher control units

Main Target

Testing and validation of the VEGA satellite launcher control units.

Objective

  • Full system dynamic simulation
  • Validated Vs experimental tests
  • Numerical simulation
  • MIL-1553-STD interface

Deliverable

Complete system

Other case history

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Development of a model for the assessment of attitude disturbances of two spacecraft

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Ultrasonic measurement rig

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VEGA satellite launcher control units

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Previous Case HistoryRobotic assistive strategy
Next Case HistoryControl for a demonstrator of a pressurized rover
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