Volume 41 Issue 5
May  2015
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LI Yuan, ZHAO Jiguang, YAN Liang, et al. United-proportional-navigation law for interception of high-speed maneuvering targets[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(5): 825-834. doi: 10.13700/j.bh.1001-5965.2014.0335(in Chinese)
Citation: LI Yuan, ZHAO Jiguang, YAN Liang, et al. United-proportional-navigation law for interception of high-speed maneuvering targets[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(5): 825-834. doi: 10.13700/j.bh.1001-5965.2014.0335(in Chinese)

United-proportional-navigation law for interception of high-speed maneuvering targets

doi: 10.13700/j.bh.1001-5965.2014.0335
  • Received Date: 09 Jun 2014
  • Rev Recd Date: 02 Jul 2014
  • Publish Date: 20 May 2015
  • Aimed to high-speed maneuvering targets, three dimensional united proportional navigation (UPN) law was proposed. The guidance law combines the advantages of head-on and head-pursuit engagement through time-varying navigation ratio. The three-dimensional UPN law consisted of two planar laws can execute head-on with head-on, head-pursuit with head-pursuit and head-on with head-pursuit mixed models, which enlarge the capture region of interceptor tremendously. At planar engagement geometry, the analytic expression of line of sight (LOS) angular rate was deduced according to the target acceleration, and the time-variant navigation ratio was designed. While the planar UPN guidance law was extended into a three dimensional condition, the mistake of interceptor path angle and velocity at pitch plane in prior algorithm was modified and the target evading model was given. The simulation results show that, for high speed maneuvering targets, UPN has less miss distance than proportional navigation (PN) and retro proportional navigation (RPN), less control effort than augmented proportional navigation (APN) and larger capture region than the others.

     

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