高超武器与常规导弹协同攻击策略可行域研究

doi:10.7527/S1000-6893.2015.0048

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高超武器与常规导弹协同攻击策略可行域研究

赵启伦¹, 陈建¹, 李清东¹, 任章¹, 李亮²

1. 北京航空航天大学飞行器控制一体化技术国防科技重点实验室, 北京 100191;
2. 上海机电工程研究所, 上海 201109

收稿日期:2014-08-26 修回日期:2015-02-20 出版日期:2015-07-15 发布日期:2015-03-01
通讯作者: 赵启伦男, 博士研究生。主要研究方向: 多飞行器协同制导与控制。 Tel: 010-82314573 E-mail: zhaoqilun@126.com E-mail:zhaoqilun@126.com
作者简介:陈建男, 博士。主要研究方向: 飞行器导航、制导与控制。 E-mail: chenjian@buaa.edu.cn;李清东男, 博士, 讲师。主要研究方向: 飞行器导航、制导与控制, 故障检测与诊断, 容错控制, 人工智能。 E-mail: muziqingdong@126.com;任章男, 博士, 教授, 博士生导师, 长江学者。主要研究方向: 飞行器导航, 制导与控制, 精确制导技术, 控制系统故障检测与诊断,系统仿真与仿真系统集成。 E-mail: renzhang@buaa.edu.cn;李亮女, 硕士, 工程师。主要研究方向: 飞行器导航、制导与控制。 E-mail: ice_li1983@163.com
基金资助:
国家自然科学基金 (91116002, 91216304, 61333011, 61121003)

Feasible region of hypersonic and ballistic missiles' cooperative attack strategy

ZHAO Qilun¹, CHEN Jian¹, LI Qingdong¹, REN Zhang¹, LI Liang²

1. Science and Technology on Aircraft Control Laboratory, Beihang University, Beijing 100191, China;
2. Shanghai Electro-Mechanical Engineering Institute, Shanghai 201109, China

Received:2014-08-26 Revised:2015-02-20 Online:2015-07-15 Published:2015-03-01
Supported by:
National Natural Science Foundation of China (91116002, 91216304, 61333011, 61121003)

摘要/Abstract

摘要：

对于高超声速武器与常规导弹协同攻击问题,提出一种同时满足法向过载约束、遭遇时间约束与终端角度约束的协同攻击策略。为提高突防能力,实现战术隐身效果,具有常规气动外型的导弹从目标正面进攻;高超声速导弹利用自身高速和大范围持续高机动能力,绕到雷达视场盲区,从目标两侧进攻;两类导弹的同时命中将对目标形成多对一的打击态势。考虑到实际工程中两类导弹机动能力的限制,推导出了保证协同攻击策略可行的充分条件,得到了协同攻击策略可行域的解析解,并分析了可用过载、飞行速度与攻击阵位对可行域的影响。仿真结果表明,协同攻击策略可以满足给定的多个约束条件,具有良好的可行性。

关键词: 高超声速飞行器, 协同制导, 过载约束, 遭遇时间约束, 终端角度约束, 可行性分析

Abstract:

For solving the cooperative attack problem of hypersonic and ballistic missiles, a cooperative attack strategy with multiple constraints of the overload, impact time and impact angle is investigated. To enhance penetration capability and achieve the effect of tactical stealth, missiles with conventional aerodynamic shape attack the target in the front. In the mean time, hypersonic missiles, taking use of its super high speed and the continuous high mobility in a large scale, go to the dead zone of radar's view field and attack the target from two other sides. Hitting the target at the same time, the two kinds of missiles form a several-for-one attacking situation. Taking into account the maneuver ability limit of two kinds of missiles, a sufficient condition of guaranteeing the cooperative attack strategy feasible is investigated, the analytic solutions of the feasible regions of cooperative attack are obtained, and the feasible regions are analyzed under different overload constraints, velocites and attacking situations. Numerical simulations demonstrate that the cooperative attack strategy could satisfy the given multiple constraints and has a well feasibility.

Key words: hypersonic vehicles, cooperative guidance, overload constraint, impact time constraint, impact angle constraint, feasibility analysis

中图分类号:

赵启伦, 陈建, 李清东, 任章, 李亮. 高超武器与常规导弹协同攻击策略可行域研究[J]. 航空学报, 2015, 36(7): 2291-2300.

ZHAO Qilun, CHEN Jian, LI Qingdong, REN Zhang, LI Liang. Feasible region of hypersonic and ballistic missiles' cooperative attack strategy[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(7): 2291-2300.

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E-mail：hkxb@buaa.edu.cn

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主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

高超武器与常规导弹协同攻击策略可行域研究

Feasible region of hypersonic and ballistic missiles' cooperative attack strategy

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