Adaptive asymptotic tracking of spacecraft attitude motion with inertia matrix identification

1997 Guidance, Navigation, and Control Conference

Volumn , Issue , 1997, Pages 311-321

  Ahmed, Jasim ^a   Coppola, Vincent T ^a   Bernstein, Dennis S ^a  

^a UNIVERSITY OF MICHIGAN   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; DYNAMICS; SPACECRAFT;

ADAPTIVE FEEDBACK CONTROL; ASYMPTOTIC TRACKING; CONING MOTION; DESIRED TRAJECTORIES; INERTIA MATRIX; ORDERING DYNAMICS; PRINCIPAL AXIS; SPACECRAFT ATTITUDE MOTION;

TRACKING (POSITION);

EID: 84959142540     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (13)

1. Junkins, J. L., and Turner, J. D., “Optimal Continuous Torque Attitude Maneuvers”, J. Guidance Contr., Vol. 3, no. 3, May-June 1980, pp 210-217.
2. Skaar, S. B., and Kraige, L. G., “Large Angle Spacecraft Attitude Maneuvers Using an Optimal Reaction Wheel Power Criterion”, The Journal of Astronautical Sciences, Vol. 32, no. 1, Jan.-Mar. 1984, pp. 47-61.
3. Wie, B., Weiss, H., and Arapostathis, A., “Quaternion Feedback Regulator for Spacecraft Eigenaxis Rotations”, J. Guidance Contr., Vol. 8, no. 3, 1989, pp. 360-365.
4. Joshi, S. M., Kelkar, A. G., and Wen, J. T.-Y., “Robust Attitude Stabilization of Spacecraft Using Nonlinear Quaternion Feedback”, IEEE Trans. Aulom. Contr., Vol. 40, Oct. 1995, pp. 1800-1803.
5. Singh, S. N., “Nonlinear Adaptive Attitude Control of Spacecraft”, IEEE Trans. Aerospace Elect. Sys., Vol. AES-23, No. 3, May 1987.
6. Sheen, J. J., and Bishop, R. H., “Adaptive Nonlinear Control of Spacecraft”, Proc. Amer. Contr. Conf., Baltimore, MD, June 1994, pp. 2867-2871.
7. Slotine, J. J. E., and Li, W., Applied Nonlinear Control, Prentice-Hall, NJ, 1989.
8. Astrom, K. J. and Wittenmark, B., Adaptive Control, Addison-Wesley, Reading, MA, 2nd edition, 1995.
9. Bloch, A. M., and Marsden, J. E., “Stabilization of Rigid Body Dynamics by the Energy-Casimir Method”, Systems & Control Letters, 14, 1990, pp. 341-346.
10. Aeyels, D., “On Stablization by Means of the Energy-Casimir Method”, Systems & Control Letters, 18, 1992, pp. 325-328.
11. Hughes, P. C., Spacecraft Attitude Dynamics, John Wiley & Sons, 1986.
12. Narendra, K. S., and Annaswamy, A. M., Stable Adaptive Systems, Prentice Hall, 1989.
13. Greenwood, D. T., Principles of Dynamics, Prentice-Hall, 1988.