子母导弹反无人机集群制导策略

doi:10.12305/j.issn.1001-506X.2023.10.29

摘要/Abstract

摘要：

针对中远程反无人机(unmanned aerial vehicle, UAV)集群的制导问题, 提出了一种子母导弹拦截UAV集群的作战构想与制导策略。首先, 综合考虑UAV目标的位置分布与威胁程度, 提出了集群威胁“重心”的选取方法, 将集群目标转化为空间中的一个点目标; 然后, 分析了子拦截弹对UAV目标的零控拦截条件与捕获区, 得到子拦截弹对目标的可拦截性约束条件, 另外结合母舱探测视场角约束、母舱探测距离约束、母舱制导约束, 提出了子拦截弹“释放点”的选取方法, 为母舱制导提供了目标点; 最后, 对集群威胁“重心”与子拦截弹“释放点”的计算模型进行了仿真, 证明了所提制导策略的有效性。所提出的制导策略, 为解决子母导弹拦截UAV集群的制导问题提供了参考。

关键词: 子母导弹, 反无人机集群, 制导策略, 捕获区

Abstract:

Aiming at the problem of anti unmanned aerial vehicle (UAV) cluster in the medium-and-long range, a combat concept and guidance strategy of mother-son missile intercepting UAV cluster is proposed. Firstly, comprehensively considering the location distribution and threat degree of UAV targets, a selection method of cluster threat "center of gravity" is proposed to transform the cluster target into a point target in the space. Secondly, the zero control interception conditions and capture region of the son interceptor to the UAV target are deduced, the interceptability constraints of the son interceptor to the target are obtained. In addition, combined with the constraints of the field of view of the mother cabin, the detection distance of the mother cabin and the guidance of the mother cabin, the selection method of the "release point" of the son interceptor is proposed, which provides the target point for the guidance of the mother cabin. Finally, the calculation models of cluster threat "center of gravity" and son interceptor "release point" are simulated, which proves the effectiveness of the designed guidance strategy and provides the reference to the UAV interception guidance for mother-son missile.

Key words: mother-son missile, anti unmanned aerial vehicle (UAV) cluster, guidance strategy, capture region

中图分类号:

TJ756

罗瑞宁, 黄树彩, 赵岩, 张振. 子母导弹反无人机集群制导策略[J]. 系统工程与电子技术, 2023, 45(10): 3249-3258.

Ruining LUO, Shucai HUANG, Yan ZHAO, Zhen ZHANG. Guidance strategy of mother-son missile against unmanned aerial vehicle cluster[J]. Systems Engineering and Electronics, 2023, 45(10): 3249-3258.

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参考文献 31

1	CHEN W , LIU J J , GUO H Z , et al. Toward robust and intelligent drone swarm: challenges and future directions[J]. IEEE Network, 2020, 34 (4): 278- 283. doi: 10.1109/MNET.001.1900521
2	HAN Y , WANG Z H , LU X M , et al. Application of AHP to road selection[J]. International Journal of GEO-Information, 2020, 9 (2): 86- 106. doi: 10.3390/ijgi9020086
3	HURST J . Robotic swarms in offensive maneuver[J]. Jont Force Quarterly, 2017, 87, 105- 111.
4	刘雷, 刘大为, 王晓光, 等. 无人机集群与反无人机集群发展现状分析[J]. 航空学报, 2022, 43 (S1): 4- 20.
	LIU L , LIU D W , WANG X G , et al. Analysis of the development status of UAV clusters and anti-UAV clusters[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43 (S1): 4- 20.
5	闫家鼎, 谢海斌, 庄东晔. 无人机集群对要地防空的威胁及反制对策研究[J]. 飞航导弹, 2021, 439 (7): 56- 61.
	YAN J D , XIE H B , ZHUANG D Y . Research on threat and countermeasures of UAV cluster to air defense in important places[J]. Aerodynamic Missile Journal, 2021, 439 (7): 56- 61.
6	孙昭, 何广军, 李广剑. 美军反无人机技术研究[J]. 飞航导弹, 2021, 443 (11): 12- 18.
	SUN Z , HE G J , LI G J . Research on american anti UAV technology[J]. Aerodynamic Missile Journal, 2021, 443 (11): 12- 18.
7	杨扬, 武蔚琦, 刘晓昕, 等. 反无人机系统研究发展分析[C]//中国航天电子技术研究院科学技术委员会2020年学术年会, 2020: 77-84.
	YANG Y, WU W Q, LIU X X, et al. Research and development analysis of anti UAV system[C]//Proc. of the Academic Annual Meeting of Science and Technology Committee of China Academy of Aerospace Electronic Technology, 2020: 77-84.
8	高显忠, 王克亮, 彭新, 等. 无人机粉碎机——硬杀伤式反无人机蜂群关键技术解析[J]. 国防科技, 2020, 41 (2): 33- 38.
	GAO X Z , WANG K L , PENG X , et al. Drone-smasher: the key technology analysis on the manner of hard kill to counter UAV swarm[J]. National Defense Technology, 2020, 41 (2): 33- 38.
9	李晶晶, 罗晨旭, 黄维. "捕蜂"——低空近程反无人机蜂群体系构想[J]. 现代防御技术, 2020, 48 (4): 16- 22. doi: 10.3969/j.issn.1009-086x.2020.04.03
	LI J J , LUO C X , HUANG W . "Bee catching": system conception of air short range anti-UAV bee colony[J]. Modern Defence Technology, 2020, 48 (4): 16- 22. doi: 10.3969/j.issn.1009-086x.2020.04.03
10	蒋镕圻, 白若楷, 彭月平. 低慢小无人机目标探测技术综述[J]. 飞航导弹, 2020, 429 (9): 100- 105.
	JIANG R Q , BAI R K , PENG Y P . Overview of target detection technology of low slow small UAV[J]. Aerodynamic Missile Journal, 2020, 429 (9): 100- 105.
11	DENG L, WU J, SHI J X, et al. Research on intelligent decision technology for multi-UAVs prevention and control[C]//Proc. of the Chinese Automation Congress, 2020: 5362-5367.
12	WANG X , TAN G Z , DAI Y S , et al. An optimal guidance strategy for moving-target interception by a multirotor unmanned aerial vehicle swarm[J]. IEEE Access, 2020, 8, 121650- 121664. doi: 10.1109/ACCESS.2020.3006479
13	刘立章, 张骞, 赵梓涵. 无人机蜂群拦截系统作战构想与关键技术[J]. 指挥控制与仿真, 2021, 43 (1): 48- 54.
	LIU L Z , ZHANG Q , ZHAO Z H . Operational conception and key technologies of unmanned aerial vehicle swarm interception system[J]. Command Control and Simulation, 2021, 43 (1): 48- 54.
14	李林汉. 针对集群目标的多飞行器协同拦截问题研究[D]. 成都: 电子科技大学, 2021.
	LI L H. Study on multi-aircraft cooperative interception for cluster targets[D]. Chengdu: University of Electronic Science and Technology of China, 2021.
15	OH J H , HA I J . Capturability of the 3-dimensional pure PNG law[J]. IEEE Trans.on Aerospace Electronic Systems, 1999, 35 (2): 491- 503.
16	GHOSH S , GHOSE D , RAHA S . Composite guidance for impact angle control against higher speed targets[J]. Journal of Guidance, Control and Dynamics, 2015, 39 (1): 98- 117.
17	廖选平, 黎克波, 刘远贺, 等. 纯比例导引律解析解与三维碰撞角约束制导[J]. 哈尔滨工业大学学报, 2021, 53 (12): 42- 50.
	LIAO X P , LI K B , LIU Y H , et al. Analytical solution of pure proportional navigation guidance law and three-dimensional guidance with impact angle constraint[J]. Journal of Harbin Institute of Technology, 2021, 53 (12): 42- 50.
18	GHOSE D . True proportional navigation with maneuvering target[J]. IEEE Trans.on Aerospace Electronic Systems, 1994, 30 (1): 229- 237.
19	KEBO L I , LIANG Y G , WENSHAN S U , et al. Performance of 3D TPN against true-arbitrarily maneuvering target for exoatmospheric interception[J]. Science China Technological Sciences, 2018, 61 (8): 1161- 1174.
20	CHAKRAVARTHY A , GHOSE D . Capturability of realistic generalized true proportional navigation[J]. IEEE Trans.on Aerospace Electronic Systems, 1996, 32 (1): 407- 418.
21	YANG C D , YANG C C . Analytical solution of 3D realistic true proportional navigation[J]. IFAC Proceedings Volumes, 1996, 29 (4): 7504- 7509.
22	FENG T. The capture region of a general 3D TPN guidance law for missile and target with limited maneuverability[C]//Proc. of the American Control Conference, 2001.
23	TYAN F . Capture region of a gipn guidance law for missile and target with bounded maneuverability[J]. IEEE Trans.on Ae-rospace Electronic Systems, 2011, 47 (1): 201- 213.
24	YANG C D , YANG C C . A unified approach to proportional navigation[J]. IEEE Trans.on Aerospace Electronic Systems, 1997, 33 (2): 557- 567.
25	张锦林, 李炯, 雷虎民, 等. 有限过载的三维现实真比例导引的捕获区域[J]. 系统工程与电子技术, 2022, 44 (3): 986- 997.
	ZHANG J L , LI J , LEI H M , et al. Capture region of 3D realistic true proportional navigation with finite overload[J]. Systems Engineering and Electronics, 2022, 44 (3): 986- 997.
26	LI K B , SU W S , CHEN L . Performance analysis of realistic true proportional navigation against maneuvering targets using Lyapunov-like approach[J]. Aerospace Science and Technology, 2017, 69, 333- 341.
27	KEBO L I , CHEN L , BAI X Z . Differential geometric modeling of guidance problem for interceptors[J]. Science China, 2011, 54 (9): 2283- 2295.
28	LI K B , ZHANG T T , CHEN L . Ideal proportional navigation for exoatmospheric interception[J]. Chinese Journal of Aeronautics, 2013, 26 (4): 976- 985.
29	周觐, 雷虎民, 侯峰, 等. 拦截高速目标的比例与反比例导引捕获区分析[J]. 宇航学报, 2018, 39 (9): 1003- 1012.
	ZHOU J , LEI H M , HOU F , et al. Capture region analysis of proportional navigation and retro-proportional navigation guidance for hypersonic target interception[J]. Journal of Astronautics, 2018, 39 (9): 1003- 1012.
30	周觐, 雷虎民. 真比例导引反高速目标拦截能力分析[J]. 系统工程与电子技术, 2018, 40 (10): 2296- 2304.
	ZHOU J , LEI H M . Interception capability analysis of the true proportional navigation guidance law against hypersonic targets[J]. Systems Engineering and Electronics, 2018, 40 (10): 2296- 2304.
31	李浩, 薛俊杰, 王晗中. 美军ISR无人机系统现状及其发展趋势[J]. 飞航导弹, 2020, (1): 76- 82.
	LI H , XUE J J , WANG H Z . Current situation and development trend of American ISR UAV system[J]. Aerodynamic Missile Journal, 2020, (1): 76- 82.

目标序号	惯性坐标系下位置			威胁度
目标序号	X/m	Y/m	Z/m	威胁度
1	3 400	79 900	8 100	0.5
2	3 600	79 700	7 900	2
3	3 800	79 900	8 100	1
4	3 300	80 100	8 000	1
5	3 500	80 100	8 000	2
6	3 700	80 100	7 900	1
7	3 900	80 200	8 200	1
8	3 400	80 500	8 000	0.5
9	3 600	80 300	8 200	1.5
10	3 800	80 600	7 800	2

目标序号	拦截时间/s	脱靶量/m
1	4.384	0.286
2	4.090	0.279
3	4.393	0.327
4	4.679	0.696
5	4.659	0.157
6	4.666	0.315
7	4.845	0.260
8	5.237	0.223
9	4.955	0.318
10	5.399	0.075

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