Controlling Attitude Maneuvers of a Flexible Satellite under Low Frequency Vibration by Using Feed-Forward Constant-Amplitude Inputs
Attitude maneuvers of a satellite equipped by using constant-amplitude thrusters are studied. The satellite consists of a rigid main body and two symmetrical flexible solar panels. Under constant-amplitude thrust, large attitude angle oscillations in low frequencies may occur after the maneuver. Thi...
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| Format: | Conference or Workshop Item |
| Published: |
2008
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| Online Access: | http://eprints.utp.edu.my/1504/1/setya-lf2008.pdf http://eprints.utp.edu.my/1504/ |
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| Institution: | Universiti Teknologi Petronas |