Controlling Attitude Maneuvers of a Flexible Satellite under
Low Frequency Vibration by Using Feed-Forward Constant-Amplitude Inputs

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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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Bibliographic Details
Main Author:	Parman, Setyamartana
Format:	Conference or Workshop Item
Language:	English
Published:	2008
Subjects:	TL Motor vehicles. Aeronautics. Astronautics
Online Access:	http://scholars.utp.edu.my/id/eprint/1504/ http://scholars.utp.edu.my/id/eprint/1504/1/setya-lf2008.pdf

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