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Volume 41 Issue 5
May  2015
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Journal of Beijing University of Aeronautics and Astronautics  > 2015  >  41(5): 857-863.
YAN Liang, ZHAO Jiguang, LI Yuanet al. Guidance law with angular constraints for head-pursuit or head-on engagement[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(5): 857-863. doi: 10.13700/j.bh.1001-5965.2014.0369(in Chinese)
Citation: YAN Liang, ZHAO Jiguang, LI Yuanet al. Guidance law with angular constraints for head-pursuit or head-on engagement[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(5): 857-863. doi: 10.13700/j.bh.1001-5965.2014.0369(in Chinese)
shu

Guidance law with angular constraints for head-pursuit or head-on engagement

doi: 10.13700/j.bh.1001-5965.2014.0369
  • 1.

    Department of Postgraduate, Equipment Academy, Beijing 101416, China

  • 2. Beijing Institute of Tracking and Telecommunications Technology, Beijing 100094, China

  • 3. Department of Scientific Research, Equipment Academy, Beijing 101416, China

  • Received Date: 19 Jun 2014
  • Rev Recd Date: 20 Jul 2014
  • Publish Date: 20 May 2015
    Abstract
  • For head-on or head-pursuit engagement, angle control proportional navigation (ACPN) and angle control retro-proportional navigation (ACRPN) closed-form trajectory shaping guidance law with impact angular constraints were proposed, which were based on proportional navigation (PN) or retro-proportional navigation (RPN) guidance law. ACPN with positive navigation ratio intercepted targets in head-on engagement, whose advantages were using less control efforts and final acceleration. ACRPN with negative navigation ratio intercepted targets in head-pursuit engagement. ACRPN's control efforts, miss distance and impact angle error were much less than that of guidance law in head-on engagement. Simulations demonstrate these claims mentioned above. Besides, the capture regions of ACPN and ACRPN for interception of high-speed targets are analyzed, which indicates that ACPN's capture region is larger than that of bias PN. Moreover, ACPN should be used to intercept targets in head-on engagement when the gimbal angle is less than sum of initial line-of-sight angle and 90°, and ACRPN should be used in head-pursuit engagement for the gimbal angle is equal to or greater than sum of initial line-of-sight angle and 90°.

     

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    • References(15)
  • [1]
    Adler F P. Missile guidance by three-dimensional proportional navigation[J].Journal of Applied Physics,1956,27(5):500-507.
    [2]
    Kim B S,Lee J G,Han H S.Biased PNG law for impact with angular constraint[J].IEEE Transactions on Aerospace and Electronic Systems,1998,34(1):277-288.
    [3]
    Zarchan P. Tactical and strategic missile guidance[M].3rd ed.Reston:AIAA,2002:15.
    [4]
    Ratnoo A,Ghose D.Impact angle constrained guidance against nonstationary nonmaneuvering targets[J].Journal of Guidance,Control,and Dynamics,2010,33(1):269-275.
    [5]
    Erer K S,Merttopcuoglu O.Indirect impact-angle-control against stationary targets using biased pure proportional navigation[J].Journal of Guidance,Control,and Dynamics,2012,35(2):700-703.
    [6]
    Jeon I,Lee J,Tahk M.Impact-time-control guidance law for anti-ship missiles[J].IEEE Transactions on Control Systems Technology,2006,14(2):260-266.
    [7]
    Prasanna H M,Ghose D.Retro-proportional-navigation:a new guidance law for interception of high-speed targets[J].Journal of Guidance,Control,and Dynamics,2012,35(2):377-386.
    [8]
    Shima T. Intercept-angle guidance[J].Journal of Guidance,Control,and Dynamics,2011,34(2):484-492.
    [9]
    闫梁,李辕,赵继广,等.基于变节点虚拟域动态逆的轨迹实时优化[J].航空学报,2013,34(12):2794-2803. Yan L,Li Y,Zhao J G,et al.Trajectory real-time optimization based on variable node inverse dynamics in the virtual domain[J].Acta Aeronautica et Astronautica Sinica,2013,34(12):2794-2803(in Chinese).
    [10]
    Mott D L. Proportional navigation[J].American Journal of Physics,1980,48(6):486-487.
    [11]
    Ben-Asher J Z,Farber N,Levinson S.New proportional navigation law for ground-to-air systems[J].Journal of Guidance,Control,and Dynamics,2003,26(5):822-825.
    [12]
    Zarchan P. Proportional navigation and weaving targets[J].Journal of Guidance,Control,and Dynamics,1995,18(5):969-974.
    [13]
    闫梁,赵继广,沈怀荣,等.带末端约束碰撞角的三维联合偏置比例制导律设计[J].航空学报,2014,35(7):1999-2010. Yan L,Zhao J G,Shen H R,et al.Three-dimensional united biased proportional navigation guidance law for interception of targets with angular constraints[J].Acta Aeronautica et Astronautica Sinica,2014,35(7):1999-2010(in Chinese).
    [14]
    Dhar A,Ghose D.Capture region for a realistic TPN guidance law[J].IEEE Transactions on Aerospace and Electronic Systems,1993,29(3):995-1003.
    [15]
    Yuan P J,Chern J S.Analytic study of biased proportional navigation[J].Journal of Guidance,Control,and Dynamics,1992,15(1): 185-190.
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