• Infrared and Laser Engineering
  • Vol. 46, Issue 5, 504004 (2017)
Zang Luyao1、*, Hou Miao2, Wang Hui1, Wang Guangshuai3, and Lin Defu1
Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
  • 3[in Chinese]
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    DOI: 10.3788/irla201746.0504004 Cite this Article
    Zang Luyao, Hou Miao, Wang Hui, Wang Guangshuai, Lin Defu. A switched-gain proportional navigation applicable for infrared guidance munitions[J]. Infrared and Laser Engineering, 2017, 46(5): 504004 Copy Citation Text show less
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    [11] Paul Z. Tactical and Strategic Missile Guidance[M]. 6th ed. Lexington: Progress in Astronautics and Aeronautics, 2012: 569-601.

    [12] Wang Hui, Lin Defu, Wang Jiang, et al. Analysis and application study on the extended trajectory shaping guidance law[J]. Acta Armamentarii, 2013, 34(7): 801-809. (in Chinese)

    [13] Wang Hui, Lin Defu, Cui Xiaoxi. Extended trajectory shaping guidance laws[J]. Transactions of Beijing Institute of Technology, 2014, 34(6): 597-602. (in Chinese)

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    [2] Wang Hongtao, Shi Deping, Liu Hengjun. Three-dimensional guidance law for missile of adjustable thrust with heat flux limit[J]. Infrared and Laser Engineering, 2018, 47(3): 304004

    Zang Luyao, Hou Miao, Wang Hui, Wang Guangshuai, Lin Defu. A switched-gain proportional navigation applicable for infrared guidance munitions[J]. Infrared and Laser Engineering, 2017, 46(5): 504004
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