Volume 34 Issue 8
Aug.  2008
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Gong Xiaolin, Fang Jiancheng, Guo Leiet al. Modeling and simulation of rapid transfer alignment for SINS[J]. Journal of Beijing University of Aeronautics and Astronautics, 2008, 34(8): 865-868. (in Chinese)
Citation: Gong Xiaolin, Fang Jiancheng, Guo Leiet al. Modeling and simulation of rapid transfer alignment for SINS[J]. Journal of Beijing University of Aeronautics and Astronautics, 2008, 34(8): 865-868. (in Chinese)

Modeling and simulation of rapid transfer alignment for SINS

  • Received Date: 30 Jul 2007
  • Publish Date: 31 Aug 2008
  • Aiming at the problem of rapid and accurate transfer alignment for the space weapon strapdown inertial navigation system (SINS), the error model of weapon SINS was established and the errors of inertial elements were considered. The attitude matching was selected, and the measurement equation of the attitude error between space weapon SINS and satellite was deduced based on the principle of attitude transfer alignment. Based on these, the filter model of space weapon SINS was established and a rapid Kalman filter was designed for the space weapon-s transfer alignment. The results of simulation show that this model is efficient on filter-s convergence and precision. The alignment accuracy is similar to the one attitude measurement system of satellite have, and furthermore, the constant errors of gyros on space weapon can be calibrated.

     

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  • [1] 王司,邓正隆.基于H与Kalman联合滤波的二次快速传递对准方法研究[J].宇航学报, 2006, 27(6): 1266-1270 Wang Si, Deng Zhenglong. Study on an approach to two time rapid transfer alignments based on H filtering associated with kalman filtering[J]. Journal of Astronautics, 2006, 27(6): 1266-1270(in Chinese) [2] 于小红.空间平台在空间对抗中的应用[J].装备指挥技术学院学报, 2003, 14(4): 35-38 Yu Xiaohong. Application research of space platform in space confrontation[J]. Journal of the Academy of Equipment Command & Technology, 2003, 14(4): 35-38(in Chinese) [3] Christopher C R, Timothy F E. A transfer alignment algorithm study based on actual flight test data from a tactical air-to-ground weapon launch //IEEE Position Location and Navigation Symposium. USA,NJ:IEEE,1994:431-438 [4] 徐福祥.卫星工程概论[M].北京:中国宇航出版社, 2003: 79-112 Xu Fuxiang. Satellite engineering[M]. Beijing: Astronautics Press, 2003: 79-112(in Chinese) [5] Zhou Naixin, Wang Si, Deng Zhenglong. Comparison of three transfer alignment methods in marine missile SINS //Proceed of the 25th Chinese Control Conference. USA,NJ:IEEE, 2006:27-31 [6] 房建成,周锐,祝世平.捷联惯导系统动基座对准的可观测性分析[J].北京航空航天大学学报, 1999, 25(6):714-719 Fang Jiancheng, Zhou Rui, Zhu Shiping. Observability analysis ofstrapdown inertial navigation system on moving base[J]. Journal of Beijing University of Aeronautics and Astronautics, 1999, 25(6):714-719(in Chinese) [7] David T, Chris R, David J, et al. Rapid and robust transfer alignment //Proceedings of the First IEEE Regional Conference on Aerospace Control Systems. USA,NJ:IEEE, 1993:758-762 [8] Shortelle K J, Graham W R, Raboum C. F-16 flight tests of a rapid transfer alignment procedure //IEEE Position Location and Navigation Symposium. USA,NJ:IEEE, 1998:379-386 [9] 郭创,张宗麟,郭明威.精确制导炸弹传递对准技术研究[J].光电与控制, 2007, 14(1):102-105 Guo Chuang, Zhang Zonglin, Guo Mingwei. On transfer alignment technology for precision guided bombs[J]. Electronics Optics & Control, 2007, 14(1):102-105(in Chinese) [10] Ross C C, Elbert T F. A transfer alignment algorithm study based on actual flight test data from a tactical air-to-ground weapon launch //IEEE Position Location and Navigation Symposium. USA,NJ:IEEE, 1994: 431-438
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