{"title":"飞行中紧急情况下飞机空气动力学变化诊断","authors":"D. Shevchuk","doi":"10.1109/APUAVD.2013.6705276","DOIUrl":null,"url":null,"abstract":"Safety of aircraft during the flight is one of the most important problems that concerns of all aviation. Damage to the external contour of the aircraft by foreign objects always leads to a change in the characteristics of the aircraft, direct and indirect economic costs and sometimes to injury or death of passengers and crew. Real-time external contour diagnostics of the aircraft and wings makes it possible to warn or prevent emergency situations and thus improve safety. The modeling of such effects is necessary for the development of reconfiguration flight control systems to recover aircraft controllability from adverse, damage-related loss-of-control events, as well as for the estimation of aerodynamic characteristics from extra conditions in flight.","PeriodicalId":400843,"journal":{"name":"2013 IEEE 2nd International Conference Actual Problems of Unmanned Air Vehicles Developments Proceedings (APUAVD)","volume":"111 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2013-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Diagnostics of aircraft aerodynamics changes in emergency situation in flight\",\"authors\":\"D. Shevchuk\",\"doi\":\"10.1109/APUAVD.2013.6705276\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Safety of aircraft during the flight is one of the most important problems that concerns of all aviation. Damage to the external contour of the aircraft by foreign objects always leads to a change in the characteristics of the aircraft, direct and indirect economic costs and sometimes to injury or death of passengers and crew. Real-time external contour diagnostics of the aircraft and wings makes it possible to warn or prevent emergency situations and thus improve safety. The modeling of such effects is necessary for the development of reconfiguration flight control systems to recover aircraft controllability from adverse, damage-related loss-of-control events, as well as for the estimation of aerodynamic characteristics from extra conditions in flight.\",\"PeriodicalId\":400843,\"journal\":{\"name\":\"2013 IEEE 2nd International Conference Actual Problems of Unmanned Air Vehicles Developments Proceedings (APUAVD)\",\"volume\":\"111 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2013-10-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2013 IEEE 2nd International Conference Actual Problems of Unmanned Air Vehicles Developments Proceedings (APUAVD)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/APUAVD.2013.6705276\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2013 IEEE 2nd International Conference Actual Problems of Unmanned Air Vehicles Developments Proceedings (APUAVD)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/APUAVD.2013.6705276","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Diagnostics of aircraft aerodynamics changes in emergency situation in flight
Safety of aircraft during the flight is one of the most important problems that concerns of all aviation. Damage to the external contour of the aircraft by foreign objects always leads to a change in the characteristics of the aircraft, direct and indirect economic costs and sometimes to injury or death of passengers and crew. Real-time external contour diagnostics of the aircraft and wings makes it possible to warn or prevent emergency situations and thus improve safety. The modeling of such effects is necessary for the development of reconfiguration flight control systems to recover aircraft controllability from adverse, damage-related loss-of-control events, as well as for the estimation of aerodynamic characteristics from extra conditions in flight.