{"title":"应用动态规划方法确定区域间飞行中燃油经济性的可能性","authors":"S. Kumakshev, A. Shmatkov","doi":"10.1109/STAB.2018.8408376","DOIUrl":null,"url":null,"abstract":"The comparison of the time-optimal and fuel-optimal trajectories of the medium-range aircraft was carried out. The optimization was implemented for the flight as a whole, without the decomposition into the sections of the climb, maintaining the flight level and descending. The mathematical model is realistic enough and involves numerous limitations on the phase coordinates and control parameters.","PeriodicalId":395462,"journal":{"name":"2018 14th International Conference \"Stability and Oscillations of Nonlinear Control Systems\" (Pyatnitskiy's Conference) (STAB)","volume":"23 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2018-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"The application of a method of dynamic programming for the determination of the possibility for fuel economy during interregional flights\",\"authors\":\"S. Kumakshev, A. Shmatkov\",\"doi\":\"10.1109/STAB.2018.8408376\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The comparison of the time-optimal and fuel-optimal trajectories of the medium-range aircraft was carried out. The optimization was implemented for the flight as a whole, without the decomposition into the sections of the climb, maintaining the flight level and descending. The mathematical model is realistic enough and involves numerous limitations on the phase coordinates and control parameters.\",\"PeriodicalId\":395462,\"journal\":{\"name\":\"2018 14th International Conference \\\"Stability and Oscillations of Nonlinear Control Systems\\\" (Pyatnitskiy's Conference) (STAB)\",\"volume\":\"23 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2018-05-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2018 14th International Conference \\\"Stability and Oscillations of Nonlinear Control Systems\\\" (Pyatnitskiy's Conference) (STAB)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/STAB.2018.8408376\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2018 14th International Conference \"Stability and Oscillations of Nonlinear Control Systems\" (Pyatnitskiy's Conference) (STAB)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/STAB.2018.8408376","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
The application of a method of dynamic programming for the determination of the possibility for fuel economy during interregional flights
The comparison of the time-optimal and fuel-optimal trajectories of the medium-range aircraft was carried out. The optimization was implemented for the flight as a whole, without the decomposition into the sections of the climb, maintaining the flight level and descending. The mathematical model is realistic enough and involves numerous limitations on the phase coordinates and control parameters.