Attitude control using higher order sliding mode

This paper proposes a chattering-free global finite-time convergent robust control method for the attitude control of a rigid spacecraft. The control method is formulated using higher order sliding mode control in integral sliding mode. The sliding mode order is higher than the system relative degre...

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Veröffentlicht in:	Aerospace science and technology 2016-07, Vol.54, p.108-113
Hauptverfasser:	Tiwari, Pyare Mohan, Janardhanan, S., un Nabi, Mashuq
Format:	Artikel
Sprache:	eng
Schlagworte:	Attitude control Controllers Derivatives Disturbances Finite-time convergence Higher order sliding mode Inertia Integral sliding mode Sliding mode Sliding mode control Uncertainty Vibration
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