New singularity escape/avoidance steering logic for control moment Gyro systems

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2003, Pages

  Wie, Bong ^a  

^a AZ 85281   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

GYROSCOPES;

CONTROL MOMENT GYROS; DESATURATION; DOUBLE-GIMBAL; PSEUDO-INVERSES; PYRAMID ARRAYS;

COMPUTER CIRCUITS;

EID: 85087597243     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-5659     Document Type: Conference Paper

References (24)

1. Crenshaw, J., "2-SPEED, A Single-Gimbal Control Moment Gyro Attitude Control System," Paper No. 73- 895, presented at AIAA Guidance and Control Conference, Key Biscayne, FL, August 20-22, 1973.
2. Margulies, G. and Aubrun, J. N., "Geometric Theory of Single-Gimbal Control Moment Gyro Systems," Journal of the Astronautical Sciences, Vol. 26, No. 2, 1978, pp. 159-191.
3. Cornick, D. E., "Singularity Avoidance Control Laws for Single Gimbal Control Moment Gyros," Paper No. 79-1698, Proceedings of the AIAA Guidance and Control Conference, Boulder, CO, August 1979, pp. 20-33.
4. Kennel, H. F., "Steering Law for Parallel Mounted Double-Gimballed Control Moment Gyros: Revision A," NASA TM-82390, January 1981.
5. Bedrossian, N. S., Paradiso, J., Bergmann, E. V., and Rowell, D., "Redundant Single-Gimbal Control Moment Gyroscope Singularity Analysis," Journal of Guidance, Control, and Dynamics, Vol. 13, No. 6, 1990, pp. 1096-1101.
6. Bedrossian, N. S., Paradiso, J., Bergmann, E. V., and Rowell, D., "Steering Law Design for Redundant Single-Gimbal Control Moment Gyroscopes," Journal of Guidance, Control, and Dynamics, Vol. 13, No. 6, 1990, pp. 1083-1089 (also, N. S. Bedrossian's M.S. thesis at MIT, August 1987).
7. Vadali, S. R., Oh, H., and Walker, S., "Preferred Gimbal Angles for Single Gimbal Control Moment Gyroscopes," Journal of Guidance, Control, and Dynamics, Vol. 13, No. 6, 1990, pp. 1090-1095.
8. Paradiso, J. A., "Global Steering of Single Gimballed Control Moment Gyroscopes Using a Direct Search," Journal of Guidance, Control, and Dynamics, Vol. 15, No. 5, 1992, pp. 1236-1244.
9. Schaub, H. and Junkins, J. L., "Singularity Avoidance Using Null Motion and Variable-Speed Control Moment Gyros," Journal of Guidance, Control, and Dynamics, Vol. 23, No. 1, 2000, pp. 11-16.
10. Ford, K. A. and Hall, C. D., "Singular Direction Avoidance Steering for Control Moment Gyros," Journal of Guidance, Control, and Dynamics, Vol. 23, No. 4, 2000, pp. 648-656.
11. Heiberg, C. J., Bailey, D., and Wie, B., "Precision Spacecraft Pointing Using Single-Gimbal Control Moment Gyros with Disturbance," Journal of Guidance, Control, and Dynamics, Vol. 23, No. 1, 2000, pp. 77-85.
12. Wie, B., Space Vehicle Dynamics and Control, AIAA Education Series, AIAA, Washington, DC, 1998, Chapter 7.
13. Wie, B., Heiberg, C., and Bailey, D., "Singularity Robust Steering Logic for Redundant Single-Gimbal Control Moment Gyros," Journal of Guidance, Control, and Dynamics, Vol. 24, No. 5, 2001, pp. 865-872.
14. Wie, B., Bailey, D., and Heiberg, C., "Robust Singularity Avoidance in Satellite Attitude Control," U.S. Patent 6,039,290, March 21, 2000.
15. Bailey, D., Heiberg, C., and Wie, B., "Continuous Attitude Control That Avoids CMG Array Singularities," U.S. Patent 6,131,056, October 10, 2000.
16. Wie, B., Heiberg, C., and Bailey, D., "Rapid Multi- Target Acquisition and Pointing Control of Agile Spacecraft," Journal of Guidance, Control, and Dynamics, Vol. 25, No. 1, 2002, pp. 96-104.
17. Dominguez, J. and Wie, B., "Computation and Visualization of Control Moment Gyroscope Singularities," Paper No. 2002-4570, AIAA Guidance, Navigation, and Control Conference, Monterey, CA, August 5-8, 2002.
18. Roser, X., Sghedoni, M., "Control Moment Gyroscopes (CMGs) and their Application in Future Scientific Missions," Proceedings of 3rd ESA International Conference on Spacecraft Guidance, Navigation, and Control Systems, ESTEC, Noordwijk, The Netherlands, Nov. 26-29, 1996, pp. 523-528.
19. Busseuil, J., Llibre, M., and Roser, X., "High Precision Mini-CMG's and their Spacecraft Applications," presented at AAS Guidance and Control-Advances in the Astronautical Sciences, Breckenridge, CO., February 1998.
20. Salenc, C. and Roger, X., "AOCS for Agile Scientific Spacecraft with mini-CMGs," Proceedings of 4th ESA International Conference on Spacecraft Guidance, Navigation, and Control Systems, ESTEC, Noordwijk, The Netherlands, Oct. 18-21, 1999, pp. 379-384.
21. Defendini, A, Lagadec, K., Guay, P., and Griseri, G., "Low Cost CMG-based AOCS Designs," Proceedings of 4th ESA International Conference on Spacecraft Guidance, Navigation, and Control Systems, ESTEC, Noordwijk, The Netherlands, Oct. 18-21, 1999, pp. 393-398.
22. Lappas, V. J., Steyn, W. H., and Underwood, C. I., "Attitude Control for Small Satellites Using Control Moment Gyros," presented at 52nd International Astronautical Federation Congress, Toulouse, France, Oct. 1-5, 2001.
23. Wie, B., "Singularity Analysis and Visualization of Single-Gimbal Control Moment Gyro Systems," Paper No. 2003-5658, AIAA Guidance, Navigation, and Control Conference, Austin, TX, August 11-14, 2003.
24. Wie, B., "Singularity Escape/Avoidance Steering Logic for Control Moment Gyros," Patent pending, Invention Disclosure #M2-092, Arizona State University, June 13, 2002.