Global attitude estimation using single direction measurements

Proceedings of the American Control Conference

Volumn , Issue , 2007, Pages 3659-3664

  Lee, Taeyoung ^a   Leok, Melvin ^b   McClamroch, N Harris ^a   Sanyal, Amit ^c  

^a UNIVERSITY OF MICHIGAN   (United States)

^b PURDUE UNIVERSITY   (United States)

^c University of Hawaii at Manoa   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

(P ,P ,T) MEASUREMENTS; ATTITUDE DYNAMICS; ATTITUDE ESTIMATION; CIRCULAR ORBITS; DIRECTION MEASUREMENT; FEASIBLE SETS; NUMERICAL EXAMPLES; REFERENCE POINT (RP); RIGID BODY (RB); ROTATION MATRICES;

MEASUREMENTS; MODAL ANALYSIS; SPACECRAFT;

ESTIMATION;

EID: 46449091444     PISSN: 07431619     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/ACC.2007.4282363     Document Type: Conference Paper

References (14)

1. G. Wahba, "A least squares estimate of satellite attitude, Problem 65-1," SIAM Review, vol. 7, no. 5, p. 409, 1965.
2. J. L. Farrell, J. C. Stuelpnagel, R. H. Wessner, J. R. Velman, and J. E. Brock, "A least squares estimate of satellite attitude, Solution 65-1," SIAM Review, vol. 8, no. 3, pp. 384-386, 1966.
3. M. D. Shuster and S. D. Oh, "Three-axis attitude determination from vector observations," Journal of Guidance Control and Dynamics, vol. 4, no. 1, pp. 70-77, 1981.
4. A. K. Sanyal, "Optimal attitude estimation and filtering without using local coordinates, Part I: Uncontrolled and deterministic attitude dynamics," in Proceedings of the American Control Conference, 2006, pp. 5734-5739.
5. M. D. Shuster, "Kalman filtering of spacecraft attitude and the QUEST model," Journal of the Astronautical Sciences, vol. 38, no. 3, pp. 377-393, 1990.
6. M. L. Psiaki, "Attitude determination filtering via extended quaternion estimation," AIAA Journal of Guidance, Control and Dynamics, vol. 23, no. 2, pp. 206-214, 2000.
7. T. Lee, A. Sanyal, M. Leok, and N. H. McClamroch, "Deterministic global attitude estimation," in Proceedings of the IEEE Conference on Decision and Control, 2006.
8. ∞ -estimation," IEEE Transactions on Signal Processing, vol. 42, no. 6, pp. 1486-1495, 1994.
9. F. C. Schweppe, "Recursive state estimation: Unknown but bounded errors and system inputs," IEEE Transactions on Automatic Control, vol. 13, no. 1, pp. 22-28, 1968.
10. D. G. Maksarov and J. P. Norton, "State bounding with ellipsoidal set description of the uncertainty," International Journal of Control, vol. 65, no. 5, pp. 847-866, 1996.
11. C. Durieu, E. Walter, and B. Polyak, "Multi-input multi-output ellipsoidal state bounding," Journal of Optimization Theory and Applications, vol. 111, no. 2, pp. 273-303, 2001.
12. T. Lee, M. Leok, and N. H. McClamroch, "Attitude maneuvers of a rigid spacecraft in a circular orbit," in Proceedings of the American Control Conference, 2006, pp. 1742-1747.
13. _, "A Lie group variational integrator for the attitude dynamics of a rigid body with applications to the 3D pendulum," in Proceedings of the IEEE Conference on Control Applications, 2005, pp. 962-967.
14. S. Body, L. E. Ghaoui, E. Feron, and V. Balakrishnan, Linear Matrix Inequalities in System and Control Theory. SIAM, 1994.