Stability Analysis for Constrained Principal Axis Slew Maneuvers

This paper addresses the problem of reorientating a rigid spacecraft from arbitrary initial conditions to prescribed final conditions with zero angular velocity. The control law analyzed is based on quaternion feedback and leaves the user to choose two gains as functions of position, angular rate, a...

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Veröffentlicht in:	The Journal of the astronautical sciences 1999-07, Vol.47 (3-4), p.239-258
Hauptverfasser:	Seywald, Hans, Lim, Kyong B, Kumar, Renjith R, Anthony, Tobin C
Format:	Artikel
Sprache:	eng
Schlagworte:	Angular position Angular velocity Asymptotic stability Constraint theory Constraints Control stability Control theory Feedback control Initial conditions Maneuvers Quaternions Slew rate Stability analysis System stability
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