{"title":"基于混合控制的空对空作战机动决策","authors":"Fenghua He, Yu Yao","doi":"10.1109/AERO.2010.5446733","DOIUrl":null,"url":null,"abstract":"In this paper, a maneuver decision-making strategy in air combat is investigated via a hybrid control theory. A Hybrid Input/Output Automaton (HIOA) model is established to describe a maneuver decision-making system for a flight vehicle in air combat.An evaluation index function is proposed considering angle, space range and acceleration of two aircraft. The two-point boundary value problem is converted into two single optimization ones, and a saddle point solution is obtained for an optimal problem. A hybrid decision-making algorithm is formulated. Simulation results show the effectiveness of the proposed method.","PeriodicalId":378029,"journal":{"name":"2010 IEEE Aerospace Conference","volume":"35 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2010-03-06","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"4","resultStr":"{\"title\":\"Maneuver decision-making on air-to-air combat via hybrid control\",\"authors\":\"Fenghua He, Yu Yao\",\"doi\":\"10.1109/AERO.2010.5446733\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"In this paper, a maneuver decision-making strategy in air combat is investigated via a hybrid control theory. A Hybrid Input/Output Automaton (HIOA) model is established to describe a maneuver decision-making system for a flight vehicle in air combat.An evaluation index function is proposed considering angle, space range and acceleration of two aircraft. The two-point boundary value problem is converted into two single optimization ones, and a saddle point solution is obtained for an optimal problem. A hybrid decision-making algorithm is formulated. Simulation results show the effectiveness of the proposed method.\",\"PeriodicalId\":378029,\"journal\":{\"name\":\"2010 IEEE Aerospace Conference\",\"volume\":\"35 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2010-03-06\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"4\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2010 IEEE Aerospace Conference\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/AERO.2010.5446733\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2010 IEEE Aerospace Conference","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/AERO.2010.5446733","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Maneuver decision-making on air-to-air combat via hybrid control
In this paper, a maneuver decision-making strategy in air combat is investigated via a hybrid control theory. A Hybrid Input/Output Automaton (HIOA) model is established to describe a maneuver decision-making system for a flight vehicle in air combat.An evaluation index function is proposed considering angle, space range and acceleration of two aircraft. The two-point boundary value problem is converted into two single optimization ones, and a saddle point solution is obtained for an optimal problem. A hybrid decision-making algorithm is formulated. Simulation results show the effectiveness of the proposed method.