Electronics Optics & Control, Volume. 22, Issue 9, 15(2015)

An IMM Algorithm for Tracking Near-Space Hypersonic

LI Jun-jie1...2, WANG Guo-hong1, ZHANG Xiang-yu1 and WU Wei1 |Show fewer author(s)
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  • 2[in Chinese]
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    References(7)

    [1] [1] DI X G, YANG Y F. Ascending trajectory optimization of near-space airship based on genetic algorithm [ C ] //IEEE 8th Conference on Industrial Electronics and Applications (ICIEA), 2013:918-922.

    [2] [2] DOU L Q, ZONG Q, JI Y H. Robust dynamic inversion control for near space vehicle [ C ]//IEEE Proceedings of 3rd International Symposium on Systems and Control in Aeronautics and Astronautics, 2010:744-749.

    [3] [3] SHEN Q K, JIANG B, COCQUEMPOT V. Fuzzy logic system-based adaptive fault-tolerant control for near-space vehicle attitude dynamics with actuator faults [ J ]. IEEE Transactions on Fuzzy Systems, 2013, 21 (2) :289-300.

    [4] [4] BUSCH M, BLACKMAN S. Evaluation of IMM filtering for an air defence system application [ C ]//Proceedings of the SPIE Conference on Signal and Data Processing of Small Targets, 1995 :435-447.

    [5] [5] BLACKMAN S S, DEMPSTER R J, ROSZKOWSKI S H. IMM/MHT application to radar and IR multitarget tracking [ C ]//Proceedings of the SPIE Conference on Signal and Data Processing of Small Targets, 1997 :429-439.

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    [11] [11] BOLLINO K P. High-fidelity real-time trajectory optimization for reusable launch vehicles[ D]. Monterey: Naval Postgraduate School, 2006.

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    LI Jun-jie, WANG Guo-hong, ZHANG Xiang-yu, WU Wei. An IMM Algorithm for Tracking Near-Space Hypersonic[J]. Electronics Optics & Control, 2015, 22(9): 15

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    Paper Information

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    Received: Oct. 24, 2014

    Accepted: --

    Published Online: Jan. 28, 2021

    The Author Email:

    DOI:10.3969/j. issn. 1671 -637x. 2015.09.004

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