Ang Huang , Xiaodong Wang , Qilun Zhao , Jianglong Yu , Xiwang Dong
{"title":"考虑速度变化的齐射攻击三维实用协同制导律","authors":"Ang Huang , Xiaodong Wang , Qilun Zhao , Jianglong Yu , Xiwang Dong","doi":"10.1016/j.ast.2025.110588","DOIUrl":null,"url":null,"abstract":"<div><div>Three-dimensional practical cooperative guidance problems for aircraft with uncontrollable velocity are investigated. Firstly, the relationship between the guidance states and the lead angle is derived, followed by the development of a fast and accurate prediction algorithm for impact time. Then, the impact time control guidance law is formulated, and the lower bound of the feedback gain that ensures terminal zero overload is analyzed. Furthermore, a distributed expected impact time decision-making and guidance law is extended for salvo attack. Finally, the validity of the proposed analytical results is confirmed through numerical simulations.</div></div>","PeriodicalId":50955,"journal":{"name":"Aerospace Science and Technology","volume":"166 ","pages":"Article 110588"},"PeriodicalIF":5.8000,"publicationDate":"2025-07-08","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Three-dimensional practical cooperative guidance law for salvo attack considering velocity variation\",\"authors\":\"Ang Huang , Xiaodong Wang , Qilun Zhao , Jianglong Yu , Xiwang Dong\",\"doi\":\"10.1016/j.ast.2025.110588\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>Three-dimensional practical cooperative guidance problems for aircraft with uncontrollable velocity are investigated. Firstly, the relationship between the guidance states and the lead angle is derived, followed by the development of a fast and accurate prediction algorithm for impact time. Then, the impact time control guidance law is formulated, and the lower bound of the feedback gain that ensures terminal zero overload is analyzed. Furthermore, a distributed expected impact time decision-making and guidance law is extended for salvo attack. Finally, the validity of the proposed analytical results is confirmed through numerical simulations.</div></div>\",\"PeriodicalId\":50955,\"journal\":{\"name\":\"Aerospace Science and Technology\",\"volume\":\"166 \",\"pages\":\"Article 110588\"},\"PeriodicalIF\":5.8000,\"publicationDate\":\"2025-07-08\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Aerospace Science and Technology\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S1270963825006595\",\"RegionNum\":1,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q1\",\"JCRName\":\"ENGINEERING, AEROSPACE\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Aerospace Science and Technology","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S1270963825006595","RegionNum":1,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
Three-dimensional practical cooperative guidance law for salvo attack considering velocity variation
Three-dimensional practical cooperative guidance problems for aircraft with uncontrollable velocity are investigated. Firstly, the relationship between the guidance states and the lead angle is derived, followed by the development of a fast and accurate prediction algorithm for impact time. Then, the impact time control guidance law is formulated, and the lower bound of the feedback gain that ensures terminal zero overload is analyzed. Furthermore, a distributed expected impact time decision-making and guidance law is extended for salvo attack. Finally, the validity of the proposed analytical results is confirmed through numerical simulations.
期刊介绍:
Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to:
• The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites
• The control of their environment
• The study of various systems they are involved in, as supports or as targets.
Authors are invited to submit papers on new advances in the following topics to aerospace applications:
• Fluid dynamics
• Energetics and propulsion
• Materials and structures
• Flight mechanics
• Navigation, guidance and control
• Acoustics
• Optics
• Electromagnetism and radar
• Signal and image processing
• Information processing
• Data fusion
• Decision aid
• Human behaviour
• Robotics and intelligent systems
• Complex system engineering.
Etc.