Analysis of Retainer Induced Disturbances of Reaction Wheel

Author:

TANIWAKI Shigemune1,KUDO Masahito2,SATO Makoto3,OHKAMI Yoshiaki4

Affiliation:

1. Graduate School of Science and Engineering, Ehime University

2. Mitsubishi Space Software Co., LTD.

3. Japan Aerospace Exploration Agency Tsukuba Space Center

4. Keio University

Publisher

Japan Society of Mechanical Engineers

Reference12 articles.

1. (1) Pedreiro, N., Next Generation Space Telescope Pointing Stability, Proceedings of AIAA Guidance, Navigation, and Control Conference, A00-37184 (2000-8).

2. (2) Bialke, B., High Fidelity Mathematical Modeling of Reaction Wheel Performance, Advances in the Astronautical Sciences, AAS 98-063 (1998).

3. (3) Masterson, R. A., Miller, D. W., and Grogan, R. L., Development and Validation of Reaction Wheel Disturbance Model, Empirical Model, Journal of Sound and Vibration, Vol. 3, No. 249 (2002), pp. 575-598.

4. (4) Boesiger, E. A., and Warner, M. H., Spin Bearing Retainer Design Optimization, Proceedings of the 25th Aerospace Mechanisms Symposium, (1991-5), pp. 161-178.

5. An Analytical and Experimental Investigation of Ball Bearing Retainer Instabilities

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