{"title":"四旋翼飞行控制系统的综合","authors":"V. Larin, A. Tunik","doi":"10.1109/MSNMC.2016.7783095","DOIUrl":null,"url":null,"abstract":"The problem of the synthesis of the advanced algorithms for quad-rotor horizontal flight control is considered. The modified procedure of the linear quadratic synthesis is applied. Two kinds of algorithms are considered here. The control goal in the 1st case is the achieving the certain point in the given navigation frame, meanwhile for the 2nd case the control goal is the stabilization of the cruise speed. Represented examples prove the efficiency of both kinds of algorithms.","PeriodicalId":420538,"journal":{"name":"2016 4th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"224 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2016-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"8","resultStr":"{\"title\":\"Synthesis of the quad-rotor flight control system\",\"authors\":\"V. Larin, A. Tunik\",\"doi\":\"10.1109/MSNMC.2016.7783095\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The problem of the synthesis of the advanced algorithms for quad-rotor horizontal flight control is considered. The modified procedure of the linear quadratic synthesis is applied. Two kinds of algorithms are considered here. The control goal in the 1st case is the achieving the certain point in the given navigation frame, meanwhile for the 2nd case the control goal is the stabilization of the cruise speed. Represented examples prove the efficiency of both kinds of algorithms.\",\"PeriodicalId\":420538,\"journal\":{\"name\":\"2016 4th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)\",\"volume\":\"224 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2016-10-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"8\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2016 4th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/MSNMC.2016.7783095\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2016 4th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/MSNMC.2016.7783095","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
The problem of the synthesis of the advanced algorithms for quad-rotor horizontal flight control is considered. The modified procedure of the linear quadratic synthesis is applied. Two kinds of algorithms are considered here. The control goal in the 1st case is the achieving the certain point in the given navigation frame, meanwhile for the 2nd case the control goal is the stabilization of the cruise speed. Represented examples prove the efficiency of both kinds of algorithms.