{"title":"某型飞机颤振裕度试验系统控制律设计与试验","authors":"K. Koenig, R. Luckner","doi":"10.1109/ICCON.1989.770633","DOIUrl":null,"url":null,"abstract":"N ( J ~ o n l y flutter suppression but also load reduction has been ~ucc.c.s~l'ully demonstrated. Inspite of this, no flutter sup~)ressioii system has been certificated for a civil aircraft up t l J now Why? System risks have been estimated greater than polcn[ial benefits. This point of view might change in the future when modern transport airplanes with electric flight control systems will offer good opportunities for cheap and msy realization of additional control laws with an adequate ufeiy level i n their digital control computers.","PeriodicalId":131568,"journal":{"name":"Proceedings. ICCON IEEE International Conference on Control and Applications","volume":"8 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1989-04-03","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":"{\"title\":\"Control law design and test of an experimental flutter margin augmentation system for an airplane\",\"authors\":\"K. Koenig, R. Luckner\",\"doi\":\"10.1109/ICCON.1989.770633\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"N ( J ~ o n l y flutter suppression but also load reduction has been ~ucc.c.s~l'ully demonstrated. Inspite of this, no flutter sup~)ressioii system has been certificated for a civil aircraft up t l J now Why? System risks have been estimated greater than polcn[ial benefits. This point of view might change in the future when modern transport airplanes with electric flight control systems will offer good opportunities for cheap and msy realization of additional control laws with an adequate ufeiy level i n their digital control computers.\",\"PeriodicalId\":131568,\"journal\":{\"name\":\"Proceedings. ICCON IEEE International Conference on Control and Applications\",\"volume\":\"8 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1989-04-03\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"1\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Proceedings. ICCON IEEE International Conference on Control and Applications\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ICCON.1989.770633\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Proceedings. ICCON IEEE International Conference on Control and Applications","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICCON.1989.770633","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 1
摘要
除颤振抑制外，还能有效地降低载荷。年代~ l 'ully证明。尽管如此，到2010年为止，民用飞机上还没有通过抗颤振系统的认证。为什么?据估计，系统风险大于政策收益。这种观点在未来可能会改变，因为配备电动飞行控制系统的现代运输飞机将为在其数字控制计算机中以足够的高质量水平实现额外的控制律提供廉价和容易的机会。
Control law design and test of an experimental flutter margin augmentation system for an airplane
N ( J ~ o n l y flutter suppression but also load reduction has been ~ucc.c.s~l'ully demonstrated. Inspite of this, no flutter sup~)ressioii system has been certificated for a civil aircraft up t l J now Why? System risks have been estimated greater than polcn[ial benefits. This point of view might change in the future when modern transport airplanes with electric flight control systems will offer good opportunities for cheap and msy realization of additional control laws with an adequate ufeiy level i n their digital control computers.
求助内容：
应助结果提醒方式：
京公网安备 11010802042870号
