{"title":"导弹射频制导仿真系统中的六自由度模型研究","authors":"Shi Chuan, He Rongmao, W. Lihua","doi":"10.1145/3351180.3351216","DOIUrl":null,"url":null,"abstract":"In the RF guidance simulation system, the software simulation of the missile flight model is one of the key technologies to be solved. This paper introduces the theoretical basis of missile flight modeling, and deeply studies the missile six degree of freedom mathematical model and its simulation algorithm. The missile flight trajectory simulation was carried out with Visual C++.Then the simulation results were used to analyze the accuracy and real-time of the two simulation algorithms, which provided a reference for the next modeling and simulation work.","PeriodicalId":375806,"journal":{"name":"Proceedings of the 2019 4th International Conference on Robotics, Control and Automation","volume":"26 2 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2019-07-26","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Research on Missile Six Degrees of Freedom Model in RF Guidance Simulation System\",\"authors\":\"Shi Chuan, He Rongmao, W. Lihua\",\"doi\":\"10.1145/3351180.3351216\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"In the RF guidance simulation system, the software simulation of the missile flight model is one of the key technologies to be solved. This paper introduces the theoretical basis of missile flight modeling, and deeply studies the missile six degree of freedom mathematical model and its simulation algorithm. The missile flight trajectory simulation was carried out with Visual C++.Then the simulation results were used to analyze the accuracy and real-time of the two simulation algorithms, which provided a reference for the next modeling and simulation work.\",\"PeriodicalId\":375806,\"journal\":{\"name\":\"Proceedings of the 2019 4th International Conference on Robotics, Control and Automation\",\"volume\":\"26 2 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2019-07-26\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Proceedings of the 2019 4th International Conference on Robotics, Control and Automation\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1145/3351180.3351216\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Proceedings of the 2019 4th International Conference on Robotics, Control and Automation","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1145/3351180.3351216","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Research on Missile Six Degrees of Freedom Model in RF Guidance Simulation System
In the RF guidance simulation system, the software simulation of the missile flight model is one of the key technologies to be solved. This paper introduces the theoretical basis of missile flight modeling, and deeply studies the missile six degree of freedom mathematical model and its simulation algorithm. The missile flight trajectory simulation was carried out with Visual C++.Then the simulation results were used to analyze the accuracy and real-time of the two simulation algorithms, which provided a reference for the next modeling and simulation work.