{"title":"优化火箭轨迹：MATLAB/simulink 中的高级数学建模","authors":"Bobomurod Muxammadkarimovich Muxammedov, Andrey Anatolievich Sanko, Davron Aslonqulovich Juraev, Ebrahim E. Elsayed","doi":"10.1007/s41870-024-02162-9","DOIUrl":null,"url":null,"abstract":"<p>The article presents a methodology for generating a simulation Simulink model of a rocket. The use of the MATLAB/Simulink environment for simulating the flight of a rocket and calculating its aerodynamic characteristics is described in detail. The principles of forming blocks for calculating the parameters of a standard atmosphere, aerodynamic characteristics, power plant thrust, flight angles, altitude and flight range are described. The results of numerical experiments carried out using the MATLAB/Simulink environment are presented.</p>","PeriodicalId":14138,"journal":{"name":"International Journal of Information Technology","volume":"12 1","pages":""},"PeriodicalIF":0.0000,"publicationDate":"2024-09-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Optimizing rocket trajectories: advanced mathematical modeling in MATLAB/simulink\",\"authors\":\"Bobomurod Muxammadkarimovich Muxammedov, Andrey Anatolievich Sanko, Davron Aslonqulovich Juraev, Ebrahim E. Elsayed\",\"doi\":\"10.1007/s41870-024-02162-9\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<p>The article presents a methodology for generating a simulation Simulink model of a rocket. The use of the MATLAB/Simulink environment for simulating the flight of a rocket and calculating its aerodynamic characteristics is described in detail. The principles of forming blocks for calculating the parameters of a standard atmosphere, aerodynamic characteristics, power plant thrust, flight angles, altitude and flight range are described. The results of numerical experiments carried out using the MATLAB/Simulink environment are presented.</p>\",\"PeriodicalId\":14138,\"journal\":{\"name\":\"International Journal of Information Technology\",\"volume\":\"12 1\",\"pages\":\"\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2024-09-11\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"International Journal of Information Technology\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1007/s41870-024-02162-9\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"International Journal of Information Technology","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1007/s41870-024-02162-9","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Optimizing rocket trajectories: advanced mathematical modeling in MATLAB/simulink
The article presents a methodology for generating a simulation Simulink model of a rocket. The use of the MATLAB/Simulink environment for simulating the flight of a rocket and calculating its aerodynamic characteristics is described in detail. The principles of forming blocks for calculating the parameters of a standard atmosphere, aerodynamic characteristics, power plant thrust, flight angles, altitude and flight range are described. The results of numerical experiments carried out using the MATLAB/Simulink environment are presented.
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