Kalman Filtering for Relative Spacecraft Attitude and Position Estimation: A Revisit

Abstract

No AccessEngineering NoteKalman Filtering for Relative Spacecraft Attitude and Position Estimation: A RevisitLijun Zhang, Huabo Yang, Shifeng Zhang, Hong Cai and Shan QianLijun ZhangDepartment of Astronautics Science and Engineering, National University of Defense Technology, 410073 Changsha, People’s Republic of China*Ph.D. Student, College of Aerospace Science and Engineering, Department of Astronautics Science and Engineering; , .Search for more papers by this author, Huabo YangDepartment of Astronautics Science and Engineering, National University of Defense Technology, 410073 Changsha, People’s Republic of China†Lecturer, College of Aerospace Science and Engineering, Department of Astronautics Science and Engineering; .Search for more papers by this author, Shifeng ZhangDepartment of Astronautics Science and Engineering, National University of Defense Technology, 410073 Changsha, People’s Republic of China‡Professor, College of Aerospace Science and Engineering, Department of Astronautics Science and Engineering; .Search for more papers by this author, Hong CaiDepartment of Astronautics Science and Engineering, National University of Defense Technology, 410073 Changsha, People’s Republic of China§Professor, College of Aerospace Science and Engineering, Department of Astronautics Science and Engineering; .Search for more papers by this author and Shan QianState Key Laboratory of Astronautic Dynamics, China Xi’an Satellite Control Center, 710043 Xi’an, People’s Republic of China¶Aerospace Engineer; .Search for more papers by this authorPublished Online:11 Sep 2014https://doi.org/10.2514/1.G000204SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations About References [1] Kim S. G., Crassidis J. L., Cheng Y., Fosbury A. M. and Junkins J. L., “Kalman Filtering for Relative Spacecraft Attitude and Position Estimation,” Journal of Guidance, Control, and Dynamics, Vol. 30, No. 1, Jan.–Feb. 2007, pp. 133–143. doi:https://doi.org/10.2514/1.22377 JGCDDT 0162-3192 LinkGoogle Scholar[2] Zipfel P. H., Modeling and Simulation of Aerospace Vehicle Dynamics, 2nd ed., AIAA, Reston, VA, 2007, pp. 368–373. LinkGoogle Scholar[3] Shuster M. D., “A Survey of Attitude Representations,” Journal of the Astronautical Sciences, Vol. 41, No. 4, 1993, pp. 439–517. JALSA6 0021-9142 Google Scholar[4] Mayo R. A., “Relative Quaternion State Transition Relation,” Journal of Guidance, Control, and Dynamics, Vol. 2, No. 1, 1979, pp. 44–48. doi:https://doi.org/10.2514/3.55830 JGCDDT 0162-3192 LinkGoogle Scholar[5] Shuster M. D., “Kalman Filtering of Spacecraft Attitude and the QUEST Model,” Journal of the Astronautical Sciences, Vol. 38, No. 3, July–Sept. 1990, pp. 377–393. JALSA6 0021-9142 Google Scholar[6] Farrenkopf R. L., “Analytic Steady-State Accuracy Solutions for Two Common Spacecraft Attitude Estimators,” Journal of Guidance and Control, Vol. 1, No. 4, 1978, pp. 282–284. doi:https://doi.org/10.2514/3.55779 JGCODS 0162-3192 LinkGoogle Scholar[7] Crassidis J. L., “Sigma-Point Kalman Filtering for Integrated GPS and Inertial Navigation,” AIAA Guidance, Navigation, and Control Conference, AIAA, Reston, VA, 2005, pp. 1981–2004. doi:https://doi.org/10.2514/6.2005-6052 Google Scholar[8] Maybeck P. S., Stochastic Models, Estimation, and Control, Vol. 2, Navtech Book and Software Store, Arlington, VA, 1994, pp. 39–59. Google Scholar Previous article Next article