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Article Navigation> JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY> 2009> 18(3): 304-308
YANG Chun-lei, TANG Sheng-jing, SHI Jiao. Proportional Navigation Guidance Law with Variable Coefficient Gravity Compensation[J]. JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY, 2009, 18(3): 304-308.
Citation: YANG Chun-lei, TANG Sheng-jing, SHI Jiao. Proportional Navigation Guidance Law with Variable Coefficient Gravity Compensation[J].JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY, 2009, 18(3): 304-308.
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Proportional Navigation Guidance Law with Variable Coefficient Gravity Compensation

  • School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China

  • Received Date:2008-06-16
    Abstract
  • Based upon a discussion on the merits and limitations of proportional navigation (PN) guidance law in which constant gravity compensation is included as a part, a counterpart having varying compensations, which changes with pitching angle and line-of-sight angle, is substituted. Flight trajectory simulation over a submissile model is conducted, resulting in increased impact angle, shorter miss distance, smaller maximum normal overload and narrower terminal angle of attack.
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    • References (5)
  • [1]
    Lin Bo, Meng Xiuyun, Liu Zaozhen. Design of the robust guidance law with terminal angle constraint[J]. Systems Engineering and Electronics, 2005, 27(11): 1943-1945. (in Chinese)
    [2]
    Lin Defu, Qi Zaikang, Xia Qunli. Design and identification on parameters of proportional navigation guidance law with gravity over compensation[J]. Journal of System Simulation, 2006, 18(10): 2753-2756. (in Chinese)
    [3]
    Jiang Ming, Song Weidong, Wang Zechuan. Analysis of proportional navigation with compensation over gravity used in laser terminal homing projectile . Journal of Ordnance Engineering College, 2007, 19(1): 47-50. (in Chinese)
    [4]
    Yang Guiqing, Xia Qunli, Zuo Titi. Study of terminal angle of attack control method for penetrating-type guided bombs with proportional navigation guidance law[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2005, 25(4): 141-143. (in Chinese)
    [5]
    Qian Xingfang, Lin Ruixiong, Zhao Yanan. Flight dynamics[M]. Beijing: Beijing Institute of Technology Press, 2000. (in Chinese) (Edited by
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