A bias proportional navigation guidance law based on terminal impact angle constraint

Feng Gao*, Sheng Jing Tang, Jiao Shi, Jie Guo

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

34 Citations (Scopus)

Abstract

In order to increase the impact angle of upper armor attack trajectory and increase the damage effect of anti-tank missile, the missile-target relative motion model of terminal guidance phase was derived. A new guidance law called bias proportional navigation guidance law based on terminal impact angle constraint was proposed, the influence of impact angle constraint on normal overload was studied and a control scheme of blind area was designed to decrease the normal overload at hit point. At last, the new guidance law was compared with conventional proportional navigation guidance law and two other improved proportional navigation guidance law based on trajectory simulation. Results of the simulation show that the new guidance law has better effect on control impact angle and high impact accuracy.

Original languageEnglish
Pages (from-to)277-282
Number of pages6
JournalBeijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology
Volume34
Issue number3
Publication statusPublished - Mar 2014

Keywords

  • Anti-tank missile
  • Bias proportion guidance law
  • Blind area
  • Impact angle constraint
  • Normal overload

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