A Variable Structure Control (VSC) approach is presented for multi-axial spacecraft reorientation maneuvers. A nonlinear sliding surface is proposed which results in an asymptotically stable, ideal linear sliding motion of Cayley-Rodriques attitude parameters. By imposing a desired equivalent dynamics on the attitude parameters, the approach is devoid of optimal control considerations. The single axis case provides a design scheme for the multiple axes design problem. Illustrative examples are presented.
Variable structure control of spacecraft reorientation maneuvers
01.01.1986
Aufsatz (Konferenz)
Keine Angabe
Englisch
Spacecraft reorientation maneuvers via linearizing variable structure control
Tema Archiv | 1987
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