A Time-Varying Control of an Underactuated Rigid Spacecraft

The problem of stabilization was studied for an underactuated rigid spacecraft. First of all, the system dynamic and kinematic equations are given, the kinematic equation is described by the (w, z) parametrization. Some continuous time-varying control laws are then designed based on the characterist...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Yanqin Zheng, Xinsheng Ge
Format: Tagungsbericht
Sprache:eng
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