Optimal linear attitude estimator

Advances in the Astronautical Sciences

Volumn 105 I, Issue , 2000, Pages 465-477

  Mortari, Daniele ^a   Markley, F Landis ^b   Junkins, John L ^c  

^a SAPIENZA UNIVERSITY OF ROME   (Italy)

^b NASA GODDARD SPACE FLIGHT CENTER   (United States)

^c TEXAS A AND M UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0040566752     PISSN: 00653438     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Article

References (18)

1. Junkins, J.L., and Kim, Y. "Introduction to Dynamics and Control of Flexible Structures," AIAA, Education Series, J.S. Przemieniecki / Series Editor-in-chief, 1978.
2. Shuster, M.D. "A Survey of Attitude Representations," Journal of Guidance and Control, Vol. 41, No. 4, 1993, pp. 439-517.
3. Rodrigues, O. "Des Lois géométriques qui regissent les déplacements d'un système solide dans l'espace," ⋯ Jour. de Math. (5) 380-480. Royal Society Catalogue of Scientific Papers, 1800-1863, Vol. 5, 1871, pp. 250-251.
4. Rodrigues, O. "Des Lois géométriques qui regissent les déplacements d'un système solide dans l'espace," ⋯ Jour. de Math. (5) 380-480. Royal Society Catalogue of Scientific Papers, 1800-1863, Vol. 5, 1871, pp. 250-251.
5. Markley, F.L., and Mortari, D. "How to Estimate Attitude from Vector Observations," Paper 99-427 of the AAS/AIAA Astrodynamics Specialist Conference, Girdwood, AK, August 15-19, 1999.
6. Mortari, D., Angelucci, M., and Markley, F.L. "Singularity, and Attitude Estimation," Paper AAS 00-130 of the 10th Annual AIAA/AAS Space Flight Mechanics Meeting, Clearwaters, FL, Jan. 23-26, 2000.
7. Wahba, G. "A Least Squares Estimate of Satellite Attitude," Problem 65-1, SIAM Review, July 1965, pp. 385-386.
8. Shuster, M.D. "Maximum Likelihood Estimate of Spacecraft Attitude," Journal of the Astronautical Sciences, Vol. 37, No. 1, 1989, pp. 79-88.
9. Shuster, M.D., and Oh, S.D. "Three-Axis Attitude Determination from Vector Observations," Journal of Guidance and Control, Vol. 4, No. 1, 1981, pp. 70-77.
10. Markley, F.L., and Mortari, D. "New Developments in Quaternion Estimation from Vector Observations," Richard H. Battin Astrodynamics Symposium Conference, Texas A&M University, College Station, TX, March 20-21, 2000.
11. Keat, J. "Analysis of Least Squares Attitude Determination Routine DOAOP," CSC/TM-77/6034, Computer Sciences Corporation, Lanham-Seabrock, Maryland, February 1977.
12. Lerner, G.M. "Three-Axis Attitude Determination," Spacecraft Attitude Determination and Control, J. R. Wertz (editor), D. Reidel, Dordrecht, Holland, 1978.
13. Mortari, D. "ESOQ-2 Single-Point Algorithm for Fast Optimal Spacecraft Attitude Determination," Advances in the Astronautical Sciences, Vol. 95, Pt. II, pp. 817-826. Paper 97-167 of the 7th Annual AIAA/AAS Space Flight Mechanics Meeting, Huntsville, AL, Feb. 10-12, 1997.
14. Mortari, D. "Second Estimator of the Optimal Quaternion," Journal of Guidance, Control, and Dynamics, publication in progress.
15. MATLAB Reference Guide. The MATH WORKS Inc. Oct. 1992.
16. Markley, F.L. "Attitude Determination using Vector Observations and the Singular Value Decomposition," Journal of the Astronautical Sciences, Vol. 36, No. 3, 1988, pp. 245-258.
17. Mortari, D. "Euler-q Algorithm for Attitude Determination from Vector Observations," Journal of Guidance, Control, and Dynamics, Vol. 21, No. 3, 1998, pp. 328-334.
18. Mortari, D. "ESOQ: A Closed-Form Solution to the Wahba Problem," Journal of the Astronautical Sciences, Vol. 45, No. 2, 1997, pp. 195-204.