Variable structure controller design for spacecraft nutation damping

Variable structure controller design for spacecraft nutation damping

Variable structure systems theory is used to design an automatic controller for active nutation damping in momentum biased stabilized spacecraft. Robust feedback stabilization of roll and yaw angular dynamics is achieved with prescribed qualitative characteristics which are totally independent of th...

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Veröffentlicht in:IEEE transactions on automatic control 1987-05, Vol.32 (5), p.435-438
Hauptverfasser: Sira-Ramirez, H., Dwyer, T.
Format: Artikel
Sprache:eng
Schlagworte:
Applied sciences
Automatic control
Computer science
control theory
systems
Control system synthesis
Control systems
Control theory. Systems
controllers
Convergence
Damping
Exact sciences and technology
Motion control
Regulators
Space vehicles
spacecraft
Spacecraft Design, Testing And Performance
stability
Variable structure systems
Weight control
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Beschreibung
Zusammenfassung:Variable structure systems theory is used to design an automatic controller for active nutation damping in momentum biased stabilized spacecraft. Robust feedback stabilization of roll and yaw angular dynamics is achieved with prescribed qualitative characteristics which are totally independent of the spacecraft defining parameters.
ISSN:0018-9286
1558-2523
DOI:10.1109/TAC.1987.1104627