Vibration suppression of flexible spacecraft during attitude control
Author:
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference13 articles.
1. Millar, A. and Vigneron, F. R., Attitude stability of flexible spacecraft which use dual time constant feedback lag network pseudorate control. AIAA/CASI 6th Communications Satellite Systems Conference, Montreal, Canada, April, 1976.
2. Clark, R. N. and Franklin, G. F., Limit cycle oscillations in pulse modulated systems. Journal of Spacecraft and Rockets, 1969, 6, 799–804.
3. Hablani, H. B., Multiaxis tracking and attitude control of flexible spacecraft with reaction jets. AIAA Journal of Guidance, Control, and Dynamics, 1994, 17, 831–839.
4. Bittner, H., Fischer, H. D. and Surauer, M., Design of Reaction Jet Attitude Control Systems for Flexible Spacecraft. IFAC Automatic Control in Space, Noordwijkerhout, The Netherlands, 1982.
5. Wie, B. and Plescia, C. T., Attitude stabilization of flexible spacecraft during station keeping maneuvers. Journal of Guidance, Control, and Dynamics, 1989, 7, 430–436.
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