(μ-Mu)-Iteration Technique: Application to attitude control of satellite with large flexible appendages

This paper addresses the problem of increasing robustness, with respect to real parameter variations, for a satellite with large flexible appendages. A first control law is designed using, for example, a classical frequency-domain method. Subsequently, robustness is improved iteratively, using the (...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Chiappa, C., Bodineau, G., Boulade, S., Beugnon, C.
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	Artificial satellites Centralized control Damping Flexible structures Mars Radar antennas Robust control Space vehicles Uncertainty Vehicle dynamics
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