Control of Spacecraft Subject to Actuator Failures: State-of-the-Art and Open Problems-Reference-Cited by-同舟云学术

Control of Spacecraft Subject to Actuator Failures: State-of-the-Art and Open Problems

Published:2000-06 Issue:2-3 Volume:48 Page:337-358
ISSN:0021-9142
Container-title:The Journal of the Astronautical Sciences
language:en
Short-container-title:J of Astronaut Sci

Author:

Tsiotras Panagiotis,Doumtchenko Viktoria

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://link.springer.com/content/pdf/10.1007/BF03546283.pdf

Reference72 articles.

1. WIE, E., WEISS, H., and ARAPOSTATHIS, A. “Quaternion Feedback Regulator for Spacecraft Eigenaxis Rotation,” Journal of Guidance, Control, and Dynamics, Vol. 12, 1989, pp. 375–380.

2. WIE B. and BARBA, P. M. “Quaternion Feedback for Spacecraft Large Angle Maneuvers,” Journal of Guidance, Control, and Dynamics, Vol. 8, No. 3, 1985, pp. 360–365.

3. VADALI, S. R. “Variable-Structure Control of Spacecraft Large-Angle Maneuvers,” Journal of Guidance, Control, and Dynamics, Vol. 9, No. 2, 1989, pp. 235–239.

4. DWYER, T. A. W. and SENA R. P. “Control of Spacecraft Slewing Maneuvers,” in Proc. of the 21st Conference on Decision and Control, 1982, Orlando, FL. pp. 1142–1144.

5. SHEEN, J. J. and BISHOP, R. H. “Spacecraft Nonlinear Control,” Paper AAS 92–172, presented at the AIAA/AAS Astrodynamics Conference, Hilton Head, SC, Aug. 10–12, 1992.

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