拦截高超声速目标的异类导弹协同制导律
收稿日期: 2015-04-23
修回日期: 2015-08-19
网络出版日期: 2015-08-29
基金资助
国家自然科学基金(91116002,91216304,61333011,61121003)
Cooperative guidance law for heterogeneous missiles intercepting hypersonic weapon
Received date: 2015-04-23
Revised date: 2015-08-19
Online published: 2015-08-29
Supported by
National Natural Science Foundation of China(91116002, 91216304, 61333011, 61121003)
对于多导弹协同拦截高超声速目标的问题,设计了一种具有领弹-从弹拓扑结构的异类导弹协同制导律:配备有高性能导引头的领弹采用改进比例导引法拦截目标;未配备导引头的从弹利用通信手段,采用二阶一致性跟踪算法,对领弹进行跟踪。两类导弹同时命中目标,形成"多对一"的拦截态势。异构型的制导策略可以降低对导引设备的需求,具备较理想的作战效费比。领弹与从弹的弹道均源于改进比例导引法,具有较理想的弹道特性。给出了协同制导律在固定拓扑与切换拓扑下成立的充分条件。算例仿真验证了所提出的制导律能够实现对高超声速目标的协同拦截,具有良好的可行性。
赵启伦 , 陈建 , 董希旺 , 李清东 , 任章 . 拦截高超声速目标的异类导弹协同制导律[J]. 航空学报, 2016 , 37(3) : 936 -948 . DOI: 10.7527/S1000-6893.2015.0235
To solve the cooperative interception problem of hypersonic weapons for multi-missiles, a cooperative guidance law based on leader-follower communication topologies for heterogeneous missiles is investigated. The leader missile is equipped with high-performance seeker to intercept the target under the modified proportional navigation guidance law. The follower missiles, not equipped with seekers, track the leader missile under the second-order consensus protocols by means of communication. Hitting the target at the same time, the two types of missiles form a several-for-one intercepting situation. The heterogeneous guidance strategy can reduce the needs for seekers, and has an ideal operational efficiency.The trajectories of the leader missile and follower missiles, which have better ballistic characteristics, derive from the modified proportional navigation guidance law. The sufficient conditions for the cooperative guidance law under the fixed topology and switched topology are presented. Numerical simulations demonstrate that the guidance law proposed could accomplish the cooperative interception of hypersonic target, and has a good feasibility.
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