{"title":"轻型运动飞机自动着陆系统","authors":"J. Vlk, Peter Chudý, Milan Prustomersky","doi":"10.1109/DASC43569.2019.9081730","DOIUrl":null,"url":null,"abstract":"The paper introduces a description of an automatic landing system for a Light Sport Aircraft (LSA) along with related concept and experimental validation by means of flight testing. The designed Linear Quadratic Regulator (LQR) which has been implemented on a digital autopilot was subjected to performance evaluations considering requirements inspired aerospace standard SAE AS94900. The autopilot's design robustness was tested on a LSA.","PeriodicalId":129864,"journal":{"name":"2019 IEEE/AIAA 38th Digital Avionics Systems Conference (DASC)","volume":"63 4 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2019-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Light Sport Aircraft Auto-Land System\",\"authors\":\"J. Vlk, Peter Chudý, Milan Prustomersky\",\"doi\":\"10.1109/DASC43569.2019.9081730\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The paper introduces a description of an automatic landing system for a Light Sport Aircraft (LSA) along with related concept and experimental validation by means of flight testing. The designed Linear Quadratic Regulator (LQR) which has been implemented on a digital autopilot was subjected to performance evaluations considering requirements inspired aerospace standard SAE AS94900. The autopilot's design robustness was tested on a LSA.\",\"PeriodicalId\":129864,\"journal\":{\"name\":\"2019 IEEE/AIAA 38th Digital Avionics Systems Conference (DASC)\",\"volume\":\"63 4 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2019-09-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2019 IEEE/AIAA 38th Digital Avionics Systems Conference (DASC)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/DASC43569.2019.9081730\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2019 IEEE/AIAA 38th Digital Avionics Systems Conference (DASC)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/DASC43569.2019.9081730","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
The paper introduces a description of an automatic landing system for a Light Sport Aircraft (LSA) along with related concept and experimental validation by means of flight testing. The designed Linear Quadratic Regulator (LQR) which has been implemented on a digital autopilot was subjected to performance evaluations considering requirements inspired aerospace standard SAE AS94900. The autopilot's design robustness was tested on a LSA.
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