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《JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS》 1996-02
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REALIZATION OF ADAPTIVE KALMAN FILTER IN TMS320C30 AND ITS APPLICATION

Chen Yihong; Yan Dong; Zhang Hongyue(Beijing University of Aeronautics and Astronautics,Dept. of Automatic Control)  
Besides the states, the statistics of the system noises must be estimated using adaptiveKalman filtering. so it is very difficult for the real-time data processing to be realized. In thispaper, TMS320C30 chip is used to improve the speed of calculating. The simulation result ofINS/GPS integrated navigation system proves that the real-time data processing of INS/GPSintegrated navigation system can be realized tising TMS320C30 chip.
【Fund】: 高等学校博士学科点科研基金
【CateGory Index】: V249.328
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1 Lan Haibin,Luo Pengfei (National University of Defense Technology, Changsha, 410073);Study of Mapping from IMM Algorithm to Systolic Array[J];火控雷达技术;2000-01
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4 Chen Yihong; Yan Dong; Zhang Hongyue(Beijing University of Aeronautics and Astronautics,Dept. of Automatic Control);REALIZATION OF ADAPTIVE KALMAN FILTER IN TMS320C30 AND ITS APPLICATION[J];北京航空航天大学学报;1996-02
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1 LI De-dong,WANG Zhen-chen,GUO Xiao-xing(Key Lab of Industrial Computer Control Engineering of Hebei Province,Yanshan University,Qinhuangdao Hebei 066004,China);Estimation of SOC of Ni-MH batteries based on fuzzy adaptive Kalman filtering for HEV[J];电源技术;2011-02
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