A comparison of the pseudo-linear and extended kalman filters for spacecraft attitude estimation

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference

Volumn 5, Issue , 2004, Pages 3007-3017

  Leung, W S W ^a   Damaren, C J ^a  

^a UNIVERSITY OF TORONTO   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; ERROR ANALYSIS; ESTIMATION; FLIGHT DYNAMICS; GEOMAGNETISM; MATRIX ALGEBRA; RICCATI EQUATIONS; SENSORS; SPACECRAFT; TORQUE; VECTORS; VELOCITY MEASUREMENT;

ANGULAR VELOCITY; EULER PARAMETERS; EXTENDED KALMAN FILTER (EKF); SPACECRAFT ATTITUDE ESTIMATION;

KALMAN FILTERING;

EID: 19944387960     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

1. Shuster, M. D., Lefferts, E. J., & Markley, F. L., "Kalman filtering for Spacecraft Attitude Estimation," J. Guidance, Control, and Dynamics, vol. 5, no. 5, pp. 417-429, 1982.
2. Jazwinski, A. H., Stochastic Processes and Filtering Theory, Academic Press, London, 1970.
3. Cloutier, J. R., "State-Dependent Riccati Equation Techniques: An Overview," Proc. American Control Conference, pp. 932-936, Albuquerque, NM, June 1997.
4. Harman, R. R. & Bar-Itzhack, "Psuedo-linear and State-Dependent Riccati Equation Filters for Angular Rate Estimation," J. Guidance, Control, and Dynamics, vol. 22, no. 5, ppp. 723-725, 1999.
5. Choukroun, D., Bar-Itzhack, I. Y., & Harman, R. R., "State-Dependent Pseudo-Linear Filters for Spacecraft Attitude and Rate Estimation," Proc. AIAA Guidance, Navigation, and Control Conference, Monterey, CA, USA, August 2002.
6. Wertz, J. R., Spacecraft Attitude Determination and Control, D. Reidel Publishing Co., Dordrecht, Holland, 1985.