{"title":"基于自由意志任意时间共识的领导-追随者网络合作齐射制导","authors":"R. S. Pal, S. R. Kumar, Dwaipayan Mukherjee","doi":"10.23919/ACC55779.2023.10156111","DOIUrl":null,"url":null,"abstract":"In this paper, a cooperative salvo guidance strategy using free-will arbitrary time consensus over a leader-follower communication network is proposed. Guidance commands are derived considering nonlinear engagement kinematics and a system lag to account for the effect of interceptor autopilot, so as to capture realistic scenarios. The guidance schemes utilize the time-to-go estimates of all interceptors to achieve simultaneous target interception. The agreement among time-to-go of all interceptors is achieved within a fixed time, to which the interceptors’ time-to-go converge within a settling time that is bounded above. This time-to-go, as well as the aforesaid bound on settling time, can be pre-specified arbitrarily independent of the initial conditions or the design parameters, which allows the interceptors to converge on a stationary target simultaneously at a predetermined impact time. Numerical simulations are presented to demonstrate the efficacy of the proposed guidance strategy.","PeriodicalId":397401,"journal":{"name":"2023 American Control Conference (ACC)","volume":"24 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2023-05-31","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Free Will Arbitrary Time Consensus-Based Cooperative Salvo Guidance over Leader-Follower Network\",\"authors\":\"R. S. Pal, S. R. Kumar, Dwaipayan Mukherjee\",\"doi\":\"10.23919/ACC55779.2023.10156111\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"In this paper, a cooperative salvo guidance strategy using free-will arbitrary time consensus over a leader-follower communication network is proposed. Guidance commands are derived considering nonlinear engagement kinematics and a system lag to account for the effect of interceptor autopilot, so as to capture realistic scenarios. The guidance schemes utilize the time-to-go estimates of all interceptors to achieve simultaneous target interception. The agreement among time-to-go of all interceptors is achieved within a fixed time, to which the interceptors’ time-to-go converge within a settling time that is bounded above. This time-to-go, as well as the aforesaid bound on settling time, can be pre-specified arbitrarily independent of the initial conditions or the design parameters, which allows the interceptors to converge on a stationary target simultaneously at a predetermined impact time. Numerical simulations are presented to demonstrate the efficacy of the proposed guidance strategy.\",\"PeriodicalId\":397401,\"journal\":{\"name\":\"2023 American Control Conference (ACC)\",\"volume\":\"24 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2023-05-31\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2023 American Control Conference (ACC)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.23919/ACC55779.2023.10156111\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2023 American Control Conference (ACC)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.23919/ACC55779.2023.10156111","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Free Will Arbitrary Time Consensus-Based Cooperative Salvo Guidance over Leader-Follower Network
In this paper, a cooperative salvo guidance strategy using free-will arbitrary time consensus over a leader-follower communication network is proposed. Guidance commands are derived considering nonlinear engagement kinematics and a system lag to account for the effect of interceptor autopilot, so as to capture realistic scenarios. The guidance schemes utilize the time-to-go estimates of all interceptors to achieve simultaneous target interception. The agreement among time-to-go of all interceptors is achieved within a fixed time, to which the interceptors’ time-to-go converge within a settling time that is bounded above. This time-to-go, as well as the aforesaid bound on settling time, can be pre-specified arbitrarily independent of the initial conditions or the design parameters, which allows the interceptors to converge on a stationary target simultaneously at a predetermined impact time. Numerical simulations are presented to demonstrate the efficacy of the proposed guidance strategy.