Periodic-disturbance accommodating control of the Space Station for asymptotic momentum management

Author:

WARREN WAYNE1,WIE BONG1,GELLER DAVID2

Affiliation:

1. Texas, University, Austin

2. NASA, Johnson Space Center, Houston, TX

Publisher

American Institute of Aeronautics and Astronautics

Reference18 articles.

1. INFLUENCE OF CONSTANT DISTURBING TORQUES ON THE MOTION OF GRAVITY-GRADIENT STABILIZED SATELLITES

2. Wie, B., Byun, K.W., Warren, W., Geller, D., Long, D., and Sunkel, J. "A New Approach to Attitude/Momentum Controlof the SpaceStation," AIAA Paper No.88-4132 (to appear in the Journal of Guidance, Control, and Dyamics).

3. Quaternion feedback for spacecraft large angle maneuvers

4. Wie, B., Weiss, H., and Arapostathis, A. "Quaternion Feedback Regulator forSpacecraft Eigenaxis Rotations," AIAA Paper No.88-4117 (toappear in the Journalof Guidance, Control, and Dynamics).

5. Kane, T.R., Likins, P.W., and Levinson, D.A., Spacecraft Dynamics, McGraw-Hill, 1983,pp.12-16,23-25, 58-62.

Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Application of LQR Algorithm with Pole Placement in TEA Control for Space Station;Chinese Journal of Space Science;2017

2. Adaptive attitude stability and control for Space Station/Orbiter berthing operations;Guidance, Navigation and Control Conference;1992-08-10

3. Continuous momentum management of earth-oriented spacecraft;Guidance, Navigation and Control Conference;1990-08-17

4. An innovative approach to the momentum management control for Space Station Freedom;Guidance, Navigation and Control Conference;1990-08-17

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