Attitude Estimation Using Parallel Quaternion Particle Filter Based on New Quaternion Distribution
Author:
Affiliation:
1. Department of Test Engineering, College of Automation Engineering, Nanjing University of Aeronautics and Astronautics
Publisher
Japan Society for Aeronautical and Space Sciences
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://www.jstage.jst.go.jp/article/tjsass/64/5/64_T-19-13/_pdf
Reference20 articles.
1. 1) Titterton, D. H. and Weston, J. L.: Strapdown Inertial Navigation Technology, Peter Pregrinus Ltd., 1997.
2. 2) Lefferts, E., Markley, F., and Shuster, M.: Kalman Filtering for Spacecraft Attitude Estimation, J. Guid. Control Dynam., 5, 5 (1982), pp. 417–429.
3. 3) Bar-Itzhack, I. Y. and Oshman, Y.: Attitude Determination from Vector Observations: Quaternion Estimation, IEEE Trans. Aerosp. Electron. Syst., AES-21, 1 (1985), pp. 128–136.
4. 4) Markley, F.: Attitude Error Representations for Kalman Filtering, J. Guid. Control Dynam., 26, 2 (2003), pp. 311–317.
5. 5) Crassidis, J. L. and Markley, F. L.: Unscented Filtering for Spacecraft Attitude Estimation, J. Guid. Control Dynam., 26, 4 (2003), pp. 536–542.
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