A novel quaternion Kalman filter

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2002, Pages

  Choukroun, D ^a   Bar Itzhack, I Y ^a   Oshman, Y ^a  

^a TECHNION ISRAEL INSTITUTE OF TECHNOLOGY   (Israel)

Author keywords

[No Author keywords available]

Indexed keywords

ERROR COMPENSATION; INTELLIGENT SYSTEMS; MONTE CARLO METHODS;

ADAPTIVE VERSIONS; CONVERGENCE PROPERTIES; ESTIMATION ERRORS; LINEAR KALMAN FILTERS; MEASUREMENT EQUATIONS; PSEUDO MEASUREMENTS; QUATERNION KINEMATICS; VECTOR MEASUREMENTS;

KALMAN FILTERS;

EID: 85088755470     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-4460     Document Type: Conference Paper

References (16)

1. Wertz, J.R. (ed.), Spacecraft Attitude Determi nation and Control, D. Reidel, Dordrecht, The Netherlands, 1984.
2. Shuster, M.D.,"A Survey of Attitude Representations," Journal of the Astronautical Sciences, Vol. 41, No. 4, 1993, pp. 439-517.
3. Markley, F.L.,"Spacecraft Attitude Determination Methods," 40th Israel Annual Conference on Aerospace Sciences, Tel Aviv, Israel, February 23- 24, 2000.
4. Wahba, G.,"A Least Squares Estimate of Space craft Attitude," SIAM Review, Vol. 7, No. 3, 1965, p. 409.
5. Keat, J,"Analysis of Least Squares Attitude De termination Routine DOAOP," Computer Sciences Corp., CSC/TM-77/6034, Silver Spring, MD, Feb. 1977.
6. 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.
7. Shuster, M.D.,"A Simple Kalman Filter and Smoother for Spacecraft Attitude," Journal of the Astronautical Sciences, Vol. 37, No. 1, January- March 1989, pp. 89-106.
8. Bar-Itzhack, I.Y.,"REQUEST: a Recursive QUEST Algorithm for Sequential Attitude Deter mination" Journal of Guidance, Control, and Dynamics, Vol. 19, No. 5, Sept.-Oct. 1996, pp. 1034-1038.
9. Psiaki, M.L.,"Attitude Determination Filtering via Extended Quaternion Estimation," Journal of Guidance, Control, and Dynamics, Vol. 23, No. 2, 2000, pp.206-214.
10. Markley, F.L.,"Attitude Determination Using Vector Observations: Theory," Journal of the Astronautical Sciences, Vol. 37, No. 1, January-March 1989, pp. 41-58.
11. Shuster, M.D.,"Maximum Likelihood Estimation of Spacecraft Attitude," Journal of the Astronautical Sciences, Vol. 37, No. 1, January-March 1989, pp. 79-88.
12. Lefferts, E.J., Markley, F.L., and Shuster, M.D., "Kalman Filtering for Spacecraft Attitude Estimation," Journal of Guidance, Control, and Dynamics, Vol. 5, Sept.-Oct. 1982, pp. 417-429.
13. Bar-Itzhack, I.Y., and Oshman, J., "Attitude De termination from Vector Observations: Quaternion Estimation," IEEE Transactions on Aerospace and Electronic Systems, Vol-AES-21, Jan. 1985, pp. 128-136.
14. Bar-Itzhack, I.Y., Deutschmann, J., and Markley, F.L., "Quaternion Normalization in Additive EKF for Spacecraft Attitude Determination," AIAA Pa per 91-2706, Guidance, Navigation, and Control Conference, New Orleans, LA, August 1991.
15. Mendel, J.M., Lessons in Estimation Theory for Signal Processing, Communications, and Control, Prentice Hall PTR, 1988.
16. Jazwinski, A.H., Stochastic Processes and Filtering Theory, New York: Academic, 1970.