Characteristic Model-based Discrete-time Sliding Mode Control for Spacecraft with Variable Tilt of Flexible Structures

In this paper, the finite-time attitude tracking control problem for the spacecrafts with variable tilt of flexible appendages in the conditions of exogenous disturbances and inertia uncertainties is addressed. First the characteristic modeling method is applied to the problem of the spacecraft mode...

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Veröffentlicht in:	IEEE/CAA journal of automatica sinica 2016-01, Vol.3 (1), p.42-50
Hauptverfasser:	Chen, Lei, Yan, Yan, Mu, Chaoxu, Sun, Changyin
Format:	Artikel
Sprache:	eng
Schlagworte:	Adaptation models Analytical models Attitude control attitude maneuver characteristic model finite time Mathematical model Sliding mode control Space vehicles Spacecraft Sun
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