The Modified Cubature Kalman Filter for Relative Navigation of Space Target Tracking

Abstract At present, the trend of improving the mobility of fast acquisition, long-term tracking and high-precision control has been formed in China. The continuous observation ability of non-cooperative targets and good imaging performance in motion are important trends in the development of optica...

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Published inJournal of physics. Conference series Vol. 2437; no. 1; pp. 12108 - 12115
Main Authors Zhang, Ai, Zhang, Chao, Zhao, Xin, Jiu, Yuanwei, Li, Jing, Huang, Gang, Liang, Fengchao
Format Journal Article
LanguageEnglish
Published Bristol IOP Publishing 01.01.2023
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Abstract Abstract At present, the trend of improving the mobility of fast acquisition, long-term tracking and high-precision control has been formed in China. The continuous observation ability of non-cooperative targets and good imaging performance in motion are important trends in the development of optical remote sensing technology. Aiming at the high-precision observation and real-time tracking requirements of high orbit space satellites, this paper studies the high-precision relative navigation of space non cooperative targets. In order to solve the problem that the estimation accuracy of Cubature Kalman filter (CKF) decreases when the system visibility is low, a modified Cubature Kalman filter (MCKF) based on the visibility is proposed. This algorithm defines a system visibility characterization method based on the error gain matrix of the filtering process, and proposes the visibility scaling parameter based on this method, The filter gain covariance matrix is adjusted online, so that the algorithm can adjust the weight of state prediction and system observation online according to the observability of the current time. Numerical simulation shows that compared with CKF, the estimation accuracy of MCKF is improved by about 4 times, and MCKF stabilizes faster and has higher accuracy.
AbstractList At present, the trend of improving the mobility of fast acquisition, long-term tracking and high-precision control has been formed in China. The continuous observation ability of non-cooperative targets and good imaging performance in motion are important trends in the development of optical remote sensing technology. Aiming at the high-precision observation and real-time tracking requirements of high orbit space satellites, this paper studies the high-precision relative navigation of space non cooperative targets. In order to solve the problem that the estimation accuracy of Cubature Kalman filter (CKF) decreases when the system visibility is low, a modified Cubature Kalman filter (MCKF) based on the visibility is proposed. This algorithm defines a system visibility characterization method based on the error gain matrix of the filtering process, and proposes the visibility scaling parameter based on this method, The filter gain covariance matrix is adjusted online, so that the algorithm can adjust the weight of state prediction and system observation online according to the observability of the current time. Numerical simulation shows that compared with CKF, the estimation accuracy of MCKF is improved by about 4 times, and MCKF stabilizes faster and has higher accuracy.
Abstract At present, the trend of improving the mobility of fast acquisition, long-term tracking and high-precision control has been formed in China. The continuous observation ability of non-cooperative targets and good imaging performance in motion are important trends in the development of optical remote sensing technology. Aiming at the high-precision observation and real-time tracking requirements of high orbit space satellites, this paper studies the high-precision relative navigation of space non cooperative targets. In order to solve the problem that the estimation accuracy of Cubature Kalman filter (CKF) decreases when the system visibility is low, a modified Cubature Kalman filter (MCKF) based on the visibility is proposed. This algorithm defines a system visibility characterization method based on the error gain matrix of the filtering process, and proposes the visibility scaling parameter based on this method, The filter gain covariance matrix is adjusted online, so that the algorithm can adjust the weight of state prediction and system observation online according to the observability of the current time. Numerical simulation shows that compared with CKF, the estimation accuracy of MCKF is improved by about 4 times, and MCKF stabilizes faster and has higher accuracy.
Author Liang, Fengchao
Zhang, Ai
Jiu, Yuanwei
Zhang, Chao
Zhao, Xin
Li, Jing
Huang, Gang
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Cites_doi 10.2514/1.45006
10.1109/TAC.2009.2019800
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Snippet Abstract At present, the trend of improving the mobility of fast acquisition, long-term tracking and high-precision control has been formed in China. The...
At present, the trend of improving the mobility of fast acquisition, long-term tracking and high-precision control has been formed in China. The continuous...
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StartPage 12108
SubjectTerms Accuracy
Algorithms
Covariance matrix
Cubature Kalman filter
Kalman filters
Navigation
Non-cooperative targets
Physics
relative navigation
Remote observing
Remote sensing
Satellite tracking
space situational awareness
Tracking
Tracking control
Visibility
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Title The Modified Cubature Kalman Filter for Relative Navigation of Space Target Tracking
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