EULER-2 and EULER-n algorithms for attitude determination from vector observations

Space Technology

Volumn 16, Issue 5-6, 1996, Pages 317-321

  Mortari, Daniele ^a  

^a SAPIENZA UNIVERSITY OF ROME   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0006189599     PISSN: 08929270     EISSN: None     Source Type: Journal    
DOI: 10.1016/s0892-9270(96)00019-x     Document Type: Article

References (6)

1. Wahba, G., A least squares estimate of spacecraft attitude. Problem 65-1, SIAM Review, 1965, 7(3), 409.
2. Shuster, M. D. and Oh, S. D. Three-axis attitude determination from vector observations. Journal of Guidance and Control, 1981, 4, 70-77.
3. Mortari, D., Energy approach algorithm for attitude determination from vector observations. Advances in Astronautical Sciences, 1995, 89, 773-784. (Paper AAS-95-207 presented at the AAS/AIAA Conference, Albuquerque, NM, February 13-16, 1995).
4. Mortari, D., Energy approach algorithm for attitude determination from vector observations. Advances in Astronautical Sciences, 1995, 89, 773-784. (Paper AAS-95-207 presented at the AAS/AIAA Conference, Albuquerque, NM, February 13-16, 1995).
5. Markley, F. L., Attitude determination using vector observations and the singular value decomposition. Journal of the Astronautical Sciences, 1988, 36(3), 70-77.
6. Wertz, J. R. (ed.), Spacecraft Attitude Determination and Control. Kluwer, Dordrecht, 1978, pp. 427-428.