Earticle

초록

영어

For the inadequacies of the classical proportional navigation law, the mathematical model of increment proportional navigation law is established in this paper. According to the mathematical model comes to attacking targets uniform linear motion trajectory simulation. The trajectory simulation of classical proportional navigation law and incremental proportional navigation law about attacking high maneuvering target are compared. Simulation results show that incremental proportional navigation law can reduce the meet time, and stabilize the missile desired normal overload beating phenomenon in the end of the curve, also it can hit the high maneuvering target in the design requirements, and its performance is superior to classical proportional navigation law.

목차

Abstract
 1. Introduction
 2. Derivation of Relative Motion Equations
 3. Analysis of Ballistics’ Characters
  3.1 Influence of ω to Meeting Time t
  3.2 Influence of ω to Required Normal Overload ny
 4. Analysis and Simulation of Increment Proportional Guidance Law
  4.1 Simulation of Initial Condition
  4.2 Simulation and analysis of meeting time
  4.3 Simulation and Analysis of Required Normal Overload
 5. Simulation and Design of Attacking Big Maneuvering Target
  5.1 Maneuvering Targets
  5.2 Analysis of Comparison with Simulation
 6. Conclusions
 References

키워드

저자

• Yao Jun [ Shenyang Ligong University, Shenyang 110159, China ]
• Wei Zhou Fei [ Shenyang Ligong University, Shenyang 110159, China ]
• Wang Xin [ Shenyang Ligong University, Shenyang 110159, China ]

참고문헌

발행기관

간행물

표지보기 관심저널 등록

• 간행물명

  International Journal of Signal Processing, Image Processing and Pattern Recognition

• 간기

  격월간

• pISSN

  2005-4254

• 수록기간

  2008~2016

• 십진분류

  KDC 505 DDC 605