Studies on Multi-Constraints Cooperative Guidance Method Based on Distributed MPC for Multi-Missiles

Cooperative terminal guidance with impact angle constraint is a key technology to achieve a saturation attack and improve combat effectiveness. The present study envisaged cooperative terminal guidance with impact angle constraint for multiple missiles. In this pursuit, initially, the three-dimensio...

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Autores principales:	Mingyu Cong, Xianghong Cheng, Zhiquan Zhao, Zhijun Li
Formato:	article
Lenguaje:	EN
Publicado:	MDPI AG 2021
Materias:	cooperative guidance model prediction control multi-missile cooperative control multi-constraint cooperative guidance Technology T Engineering (General). Civil engineering (General) TA1-2040 Biology (General) QH301-705.5 Physics QC1-999 Chemistry QD1-999
Acceso en línea:	https://doaj.org/article/0da46f686e8d42c0bb1e3b3a51416aeb
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id	oai:doaj.org-article:0da46f686e8d42c0bb1e3b3a51416aeb
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spelling	oai:doaj.org-article:0da46f686e8d42c0bb1e3b3a51416aeb2021-11-25T16:39:24ZStudies on Multi-Constraints Cooperative Guidance Method Based on Distributed MPC for Multi-Missiles10.3390/app1122108572076-3417https://doaj.org/article/0da46f686e8d42c0bb1e3b3a51416aeb2021-11-01T00:00:00Zhttps://www.mdpi.com/2076-3417/11/22/10857https://doaj.org/toc/2076-3417Cooperative terminal guidance with impact angle constraint is a key technology to achieve a saturation attack and improve combat effectiveness. The present study envisaged cooperative terminal guidance with impact angle constraint for multiple missiles. In this pursuit, initially, the three-dimensional cooperative terminal guidance law with multiple constraints was studied. The impact time cooperative strategy of virtual leader missile and follower missiles was designed by introducing virtual leader missiles. Subsequently, based on the distributed model prediction control combined with the particle swarm optimization algorithm, a cooperative terminal guidance algorithm was designed for multiple missiles with impact angle constraint that met the guidance accuracy. Finally, the effectiveness of the algorithm was verified using simulation experiments.Mingyu CongXianghong ChengZhiquan ZhaoZhijun LiMDPI AGarticlecooperative guidancemodel prediction controlmulti-missile cooperative controlmulti-constraint cooperative guidanceTechnologyTEngineering (General). Civil engineering (General)TA1-2040Biology (General)QH301-705.5PhysicsQC1-999ChemistryQD1-999ENApplied Sciences, Vol 11, Iss 10857, p 10857 (2021)
institution	DOAJ
collection	DOAJ
language	EN
topic	cooperative guidance model prediction control multi-missile cooperative control multi-constraint cooperative guidance Technology T Engineering (General). Civil engineering (General) TA1-2040 Biology (General) QH301-705.5 Physics QC1-999 Chemistry QD1-999
spellingShingle	cooperative guidance model prediction control multi-missile cooperative control multi-constraint cooperative guidance Technology T Engineering (General). Civil engineering (General) TA1-2040 Biology (General) QH301-705.5 Physics QC1-999 Chemistry QD1-999 Mingyu Cong Xianghong Cheng Zhiquan Zhao Zhijun Li Studies on Multi-Constraints Cooperative Guidance Method Based on Distributed MPC for Multi-Missiles
description	Cooperative terminal guidance with impact angle constraint is a key technology to achieve a saturation attack and improve combat effectiveness. The present study envisaged cooperative terminal guidance with impact angle constraint for multiple missiles. In this pursuit, initially, the three-dimensional cooperative terminal guidance law with multiple constraints was studied. The impact time cooperative strategy of virtual leader missile and follower missiles was designed by introducing virtual leader missiles. Subsequently, based on the distributed model prediction control combined with the particle swarm optimization algorithm, a cooperative terminal guidance algorithm was designed for multiple missiles with impact angle constraint that met the guidance accuracy. Finally, the effectiveness of the algorithm was verified using simulation experiments.
format	article
author	Mingyu Cong Xianghong Cheng Zhiquan Zhao Zhijun Li
author_facet	Mingyu Cong Xianghong Cheng Zhiquan Zhao Zhijun Li
author_sort	Mingyu Cong
title	Studies on Multi-Constraints Cooperative Guidance Method Based on Distributed MPC for Multi-Missiles
title_short	Studies on Multi-Constraints Cooperative Guidance Method Based on Distributed MPC for Multi-Missiles
title_full	Studies on Multi-Constraints Cooperative Guidance Method Based on Distributed MPC for Multi-Missiles
title_fullStr	Studies on Multi-Constraints Cooperative Guidance Method Based on Distributed MPC for Multi-Missiles
title_full_unstemmed	Studies on Multi-Constraints Cooperative Guidance Method Based on Distributed MPC for Multi-Missiles
title_sort	studies on multi-constraints cooperative guidance method based on distributed mpc for multi-missiles
publisher	MDPI AG
publishDate	2021
url	https://doaj.org/article/0da46f686e8d42c0bb1e3b3a51416aeb
work_keys_str_mv	AT mingyucong studiesonmulticonstraintscooperativeguidancemethodbasedondistributedmpcformultimissiles AT xianghongcheng studiesonmulticonstraintscooperativeguidancemethodbasedondistributedmpcformultimissiles AT zhiquanzhao studiesonmulticonstraintscooperativeguidancemethodbasedondistributedmpcformultimissiles AT zhijunli studiesonmulticonstraintscooperativeguidancemethodbasedondistributedmpcformultimissiles
_version_	1718413060031381504

Studies on Multi-Constraints Cooperative Guidance Method Based on Distributed MPC for Multi-Missiles

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