{"title":"直升机座舱转向装置舒适性建模与优化设计","authors":"Yang Jun-chao, Guolong Ding, Shi Yue","doi":"10.1109/CCIENG.2011.6007954","DOIUrl":null,"url":null,"abstract":"Contrapose the problem of helicopter cockpit steering apparatus comfort, a 5 degrees freedom man upper arm movement model is established. Considering the influence of biostatics for pilot subjective comfort, the RULA method is introduced to the establishment of upper arm introduce model. Adopting China helicopter pilot anthropometric data, contrasting the result of CATIA system emulator, the rationality and practicability of the model is validated. Using collective pitch control layout design as example, the corresponding apparatus comfort curve and parameter are acquired. The results can provide effective reference for helicopter cockpit steering apparatus design.","PeriodicalId":6316,"journal":{"name":"2011 IEEE 2nd International Conference on Computing, Control and Industrial Engineering","volume":"201 1","pages":"50-53"},"PeriodicalIF":0.0000,"publicationDate":"2011-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Amenity modeling and optimal design of helicopter cockpit steering apparatus\",\"authors\":\"Yang Jun-chao, Guolong Ding, Shi Yue\",\"doi\":\"10.1109/CCIENG.2011.6007954\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Contrapose the problem of helicopter cockpit steering apparatus comfort, a 5 degrees freedom man upper arm movement model is established. Considering the influence of biostatics for pilot subjective comfort, the RULA method is introduced to the establishment of upper arm introduce model. Adopting China helicopter pilot anthropometric data, contrasting the result of CATIA system emulator, the rationality and practicability of the model is validated. Using collective pitch control layout design as example, the corresponding apparatus comfort curve and parameter are acquired. The results can provide effective reference for helicopter cockpit steering apparatus design.\",\"PeriodicalId\":6316,\"journal\":{\"name\":\"2011 IEEE 2nd International Conference on Computing, Control and Industrial Engineering\",\"volume\":\"201 1\",\"pages\":\"50-53\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2011-09-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2011 IEEE 2nd International Conference on Computing, Control and Industrial Engineering\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/CCIENG.2011.6007954\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2011 IEEE 2nd International Conference on Computing, Control and Industrial Engineering","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/CCIENG.2011.6007954","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Amenity modeling and optimal design of helicopter cockpit steering apparatus
Contrapose the problem of helicopter cockpit steering apparatus comfort, a 5 degrees freedom man upper arm movement model is established. Considering the influence of biostatics for pilot subjective comfort, the RULA method is introduced to the establishment of upper arm introduce model. Adopting China helicopter pilot anthropometric data, contrasting the result of CATIA system emulator, the rationality and practicability of the model is validated. Using collective pitch control layout design as example, the corresponding apparatus comfort curve and parameter are acquired. The results can provide effective reference for helicopter cockpit steering apparatus design.