Constraint in Attitude Estimation Part II: Unconstrained Estimation

Author:

Shuster Malcolm D.

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Aerospace Engineering

Reference40 articles.

1. SHUSTER, M. D. “Constraint in Attitude Estimation, Part I: Constrained Estimation,” The Journal of the Astronautical Sciences, Vol. 51, No. 1, pp. 51–74.

2. SHUSTER, M. D. “The Quaternion in the Kaiman Filter,” presented as paper No. AAS 93–62, Proceedings, AAS/AIAA Astrodynamics Specialists Conference, Victoria, British Columbia, Canada, August 1993; printed as “The Quaternion in the Kaiman Filter,” Advances in the Astronautical Sciences, Vol. 85, pp. 25–37, 1993.

3. BAR-ITZHACK, I. Y. and OSHMAN, J. “Attitude Determination from Vector Observations: Quaternion Observation,” IEEE Transactions on Automatic Control, Vol. AES-21, No. 1, January 1985, pp. 128–136.

4. BAR-ITZHACK, I. Y. and REINER, J. “Recursive Attitude Determination from Vector Observations: DCM Identification,” Journal of Guidance, Control and Dynamics, Vol. 7, No. 1, January–February 1984, pp. 51–56.

5. BAR-ITZHACK, I. Y., MARKLEY, F. L., and DEUTSCHMANN, J. “Quaternion Normalization in Additive EKF for Spacecraft Attitude Determination,” presented at the Flight Mechanics/Estimation Theory Symposium, NASA Goddard Space Flight Center, May 1991.

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