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
1986-01-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Spacecraft reorientation maneuvers via linearizing variable structure control
Tema Archiv | 1987
|Variable Speed Control Moment Gyroscopes for Reorientation Maneuvers of Rigid Spacecraft
Online Contents | 2004
|Variable Speed Control Moment Gyroscopes for Reorientation Maneuvers of Rigid Spacecraft
Springer Verlag | 2004
|Variable Speed Control Moment Gyroscopes for Reorientation Maneuvers of Rigid Spacecraft
Online Contents | 2004
|