Detumbling and partial attitude stabilization of a rigid spacecraft under actuator failure

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2000, Pages

  Tsiotras, Panagiotis ^a   Schleicher, Alexander ^a  

^a Georgia Institute of Technology   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; CONTROL THEORY; DYNAMICAL SYSTEMS; STABILIZATION;

ACTUATOR FAILURES; ATTITUDE STABILIZATION; CONTROL OBJECTIVES; CONTROL STRATEGIES; NON SYMMETRIES; RIGID SPACECRAFT; SINGLE ACTUATORS; THEORETICAL DEVELOPMENT;

SPACECRAFT;

EID: 85087593528     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-4044     Document Type: Conference Paper

References (26)

1. Mortensen, R. E., "A Globally Stable Linear Attitude Regulator," International Journal of Control, Vol. 8, No. 3, 1968, pp. 297-302.
2. Bach, R. and Paielli, R., "Linearization of attitude-control error dynamics," IEEE Transactions on Automatic Control, Vol. 38, No. 10, 1993, pp. 1521-1525.
3. Wie, B., Weiss, H., and Arapostathis, A., "Quaternion feedback regulator for spacecraft eigenaxis rotation," Journal of Guidance, Control, and Dynamics, Vol. 12, 1989, pp. 375-380.
4. Wen, J. T. and Kreutz-Delgado, K., "The attitude control problem," IEEE Transactions on Automatic Control, Vol. 36, No. 10, 1991, pp. 1148-1162.
5. Crouch, P. E., "Spacecraft attitude control and stabilization: Applications of geometric control theory to rigid body models," IEEE Transactions on Automatic Control, Vol. 29, No. 4, 1984, pp. 321-331.
6. Byrnes, C. I., Isidori, A., Monaco, S., and Sabatino, S., "Analysis and simulation of a controlled rigid spacecraft: stability and instability near attractors," Proceedings of the American Control Conference, 1988, pp. 81-85, Austin, TX.
7. Byrnes, C. I. and Isidori, A., "On the attitude stabilization of a rigid spacecraft," Automatica, Vol. 27, No. 1, 1991, pp. 87-95.
8. Krishnan, H., Reyhanoglu, M., and McClamroch, H., "Attitude stabilization of a rigid spacecraft using two control torques: A nonlinear control approach based on the spacecraft attitude dynamics," Automatica, Vol. 30, No. 6, 1994, pp. 1023-1027.
9. Tsiotras, P., Corless, M., and Longuski, M., "A novel approach to the attitude control of an axisyrnmetric spacecraft," Automatica, Vol. 31, No. 8, 1995, pp. 1099-1112.
10. Tsiotras, P. and Luo, J., "Stabilization and Tracking of Underactuated Axisymmetric Spacecraft with Bounded Control," Proc. 4th IFAC Nonlinear Control Systems Design Symposium, July 1-3, 1998, pp. 800-806, Twente, The Netherlands.
11. Tsiotras, P., "Feasible Trajectory Generation for Underactuated Spacecraft Using Differential Flatness," AAS Astrodynamics Specialists Conference, Girdwood, AL, Aug. 16-18 1999, AAS Paper 99-323.
12. Morin, P. and Samson, C., "Time-Varying Exponential Stabilization of a Rigid Spacecraft with Two Control Torques," IEEE Transactions on Automatic Control, Vol. 42, No. 4, 1997, pp. 528-534.
13. Coron, J. M. and Keraï, E. L., "Explicit Feedback Stabilizing the Attitude of a Rigid Spacecraft with Two Control Torques," Automatica, Vol. 36, No. 5, 1996, pp. 669-677.
14. Morin, P., Samson, C., Pomet, J., and Jiang, Z.-P., "Time-Varying Feedback Stabilization of the Attitude of a Rigid Spacecraft with Two Controls," Systems and Control Letters, Vol. 25, 1995, pp. 375-385.
15. Brockett, R. W., "Asymptotic Stability and Feedback Stabilization," Differential Geometric Control Theory, edited by R. W. Brockett, R. S. Millman, and H. J. Sussman, Birkhauser, 1983, pp. 181-208.
16. M'Closkey, R. T. and Murray, R. M., "Nonholonomic Systems and Exponential Convergence: Some Analysis Tools," Proc., 32nd Conference on Decision and Control, 1993, pp. 943-948, San Antonio, TX.
17. Tsiotras, P. and Doumtchenko, V, "Control of Spacecraft Subject to Actuator Failures: State-of-the-Art and Open Problems," Proceedings of the R.H. Battin Astrodynamics Symposium, College Station, TX, March 20-21, 2000, AAS Paper 00-264.
18. Tsiotras, P. and Luo, J., "Reduced-Effort Control Laws for Underactuated Rigid Spacecraft," Journal of Guidance, Control, and Dynamics, Vol. 20, No. 6, 1997, pp. 1089-1095.
19. Tsiotras, P. and Longuski, J. M., "A new parameterization of the attitude kinematics," Journal of the Astronautical Sciences, Vol. 43, No. 3, 1995, pp. 243-262.
20. Rosier, L., "Homogeneous Lyapunov functions for Homogeneous vector fields," Systems and Control Letters, Vol. 19, No. 6, 1992, pp. 467-473.
21. Bacciotti, A., Local Stabilizability of Nonlinear Control Systems, World Scientific, Singapore, 1992.
22. Tsiotras, P. and Luo, J., "A Low-Authority Control Law for Underactuated Rigid Spacecraft," 35th Aerospace Sciences Meeting, Reno, NV, Jan. 6-10, 1997, pp. 57-66, AIAA Paper 97-0113.
23. Tsiotras, P. and Longuski, J. M., "Comments on a New Parameterization of the Attitude Kinematics," AIAA/AAS Astrodynamics Specialists Conference, San Diego, CA, July 29-31 1996, Paper AAS 96-3627.
24. Coron, J. M. and Praly, L., "Adding an integrator for the stabilization problem," Systems and Control Letters, Vol. 17, 1991, pp. 89-104.
25. Praly, L., d'Andrea Novel, B., and Coron, J. M., "Lyapunov Design of Stabilizing Controllers for Cascaded Systems," IEEE Transactions on Automatic Control, Vol. 36, No. 10, 1991, pp. 1177-1118.
26. Kolmanovsky, I. and McClamroch, H., "Application of integrator backstepping to nonholonomic control problems," Proc. of the IFAC Symposium Nonlinear Control Systems Design, 1995, pp. 753-758, Tahoe City, CA.