Three-axis attitude determination from vector observations

Journal of Guidance, Control, and Dynamics

Volumn 4, Issue 1, 1981, Pages 70-77

  Shuster, M D ^a   Oh, S D ^a  

^a Computer Sciences Corporation ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

SPACECRAFT;

EID: 0019384696     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.19717     Document Type: Article

References (8)

1. Lerner, G.M., “Three-Axis Attitude Determination,” Spacecraft Attitude Determination and Control, edited by J.R. Wertz, D. Reidel Publishing Co., Dordrecht, The Netherlands, 1978, p. 420-428.
2. D. Niebur, et al., “HCMM Attitude Analysis and Support Plan,” NASA X-581-78-4, March 1978, p. 4-149.
3. Wahba, G., “A Least Squares Estimate of Satellite Attitude, Problem 65.1,” SIAM Review, July 1966, pp. 385-386.
4. Keat, J., “Analysis of Least-Squares Attitude Determination Routine, DOAOP,” Computer Sciences Corp., Report CSC/TM-77/6034, Feb. 1977.
5. Shuster, M.D., “Approximate Algorithms for Fast Optimal Attitude Computation,” Proceedings, AIAA Guidance and Control Conference, Palo Alto, Calif., Aug. 7-9, 1978.
6. Markiey, F.L., “Parameterization of the Attitude,” Spacecraft Attitude Determination and Control, edited by J.R. Wertz, D.Reidel Publishing Co., Dordrecht, The Netherlands, 1978, pp. 410-420.
7. Hildebrand, F.B., Advanced Calculus for Applications, Prentice-Hall, Inc., Englewood Cliffs, N.J., 1962.
8. Hoffman, K. and Kunze, R., Linear Algebra, Prentice-Hall, Inc., Englewood Cliffs, N.J., 1961.