Attitude Control of Flexible System by Shaping Constant-Amplitude Input
Attitude manoeuvres of satellites in space are generally performed by using thrusters. Thrusts resulted usually can not be variable, they are constant in amplitudes. When a satellite has flexibility in its structural members or in its member’s joints, under constant-amplitude thrust, large struct...
| Main Authors: | , , |
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| Format: | Conference or Workshop Item |
| Language: | English |
| Published: |
2008
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| Subjects: | |
| Online Access: | http://scholars.utp.edu.my/id/eprint/1506/ http://scholars.utp.edu.my/id/eprint/1506/1/PETRONAS07_-_Full.pdf |