Shape Change Maneuvers for Attitude Control of Underactuated Satellites
An asymptotically stable set point control law is introduced for attitude control of the underactuated spacecraft of a satellite system through its appendage shape changes. It is proposed that rotational maneuvers of the spacecraft are possible while simultaneously achieving a desired shape if the t...
|Authors:||Hashem Ashrafiuon, R.S. Irwin|
|Conference Location:||Portland, OR|
|Conference Dates:||Jun. 8-10, 2005|
|Proceedings Title:||Proceedings of the 2005 American Control Conference|
Evanston, IL :
American Automatic Control Council,