A study of aircraft-defense missile cooperative active defense technology

Xiaoping Wang, Lutong Wang, Qin-ying Lin, Minghui Xia, Liangliang Chen
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Abstract

This paper introduced the implementation strategy of three points collinear active defense to realize aircraft active defense. Based on the kinetic characteristic of fighter, defending missile, offensive missile, a induce capture aircraft-defending missile synergy active defense method was put forward, which transform the complex air war confront problem between fighter and defending missile and offensive missile into a simple trajectory problem of fighter. A process performance index during the implementation process of active defense strategy was put forward and the different between process performance index and traditional performance index was analyzed. Because of the QPSO arithmetic is a off-line arithmetic, result in the whole process can't be able to be evaluate. So the method of RHC(receding horizon control) was used to maintain process performance index as the optimization index of every receding optimization window. Which solve the disadvantage of QPSO arithmetic and rise its real-time. Simulation was applied to prove the validity of active defense strategy and synergy method, and the effectiveness and accuracy of this arithmetic.
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防空导弹协同主动防御技术研究
介绍了三点共线主动防御实现飞机主动防御的实施策略。根据战斗机、防御导弹、进攻导弹的运动特性,提出了诱导捕获机防导弹协同主动防御方法,将战斗机与防御导弹、进攻导弹之间复杂的空战对抗问题转化为简单的战斗机弹道问题。提出了主动防御战略实施过程中的过程绩效指标,并分析了过程绩效指标与传统绩效指标的区别。由于QPSO算法是一种离线算法,整个过程的结果无法评估。因此,采用后退水平控制(RHC)方法维持过程性能指标作为每个后退优化窗口的优化指标。解决了量子粒子群算法的缺点,提高了算法的实时性。通过仿真验证了主动防御策略和协同方法的有效性,以及该算法的有效性和准确性。
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