Stable fraction approach and attitude-control of a spinning satellite using a gyrotorquer
The problem of joint stabilization and tracking of a spinning satellite system in addition to its regulation are considered. The rational fractional approach is used to obtain coprime equations in a multivariate setting for both coupled and decoupled models. Parametrized compensators are obtained for regulation and stabilization with tracking cases. Simulation results are presented to show the accomplishment of attitude control in different settings with simple control inputs.
Electrical and Computer Engineering | Power and Energy | Signal Processing | Systems and Communications
Use Find in Your Library, contact the author, or interlibrary loan to garner a copy of the item. Publisher policy does not allow archiving the final published version. If a post-print (author's peer-reviewed manuscript) is allowed and available, or publisher policy changes, the item will be deposited.
Stable fraction approach and attitude-control of a spinning satellite using a gyrotorquer.
International Journal of Systems Science, 23