Stabilization of high-order constant systems by multilevel control is proposed in the framework of the decomposition-aggregation method for stability analysis of large-scale systems. An 11-order linear model of a spinning flexible spacecraft is stabilized by the method using both the passive and the active stabilization devices. The method can take advantage of the special structural features of the model to provide the best estimate of the stability region for an important parameter which couples the wobble and the spin motion of the spacecraft.
Stabilization of large-scale systems - A spinning flexible spacecraft
International Federation of Automatic Control, Triennial World Congress ; 1975 ; oston, US
1975-01-01
Miscellaneous
No indication
English
Attitude Stabilization of Large Flexible Spacecraft
AIAA | 1981
|Attitude stabilization of large flexible spacecraft
AIAA | 1978
|Distributed Control of Spinning Flexible Spacecraft
AIAA | 1979
|Digital Control of Spinning Flexible Spacecraft
AIAA | 1978
|