首页 | 本学科首页   官方微博 | 高级检索  
     检索      

直接力控制飞机非常规响应耦合敏感性分析
作者姓名:Xu  Ruijuan
作者单位:Faculty 503 of Northwestern Polytechnical University,Xi'an,710072
摘    要: 针对当前直接力控制系统设计实践中遇到的直接力控制(DFC)飞机非常规响应耦合敏感性问题,借助闭环系统动力学和瞄准误差动力学理论进行推导与分析,进而通过实例计算,得出可供DFC系统设计及飞机飞行品质评定参考的重要结论。

关 键 词:
收稿时间:1994-02-20;

ANALYSIS OF COUPLING SENSITIVITY OF UNCONVENTIONAL RESPONSES FOR DIRECT FORCE CONTROL(DFC) AIRCRAFT
Xu Ruijuan.ANALYSIS OF COUPLING SENSITIVITY OF UNCONVENTIONAL RESPONSES FOR DIRECT FORCE CONTROL(DFC) AIRCRAFT[J].Acta Aeronautica et Astronautica Sinica,1995,16(4):25-31.
Authors:Xu Ruijuan
Institution:Faculty 503 of Northwestern Polytechnical University,Xi’an,710072
Abstract:The coupling sensitivity of unconventional responses of DFC aircraft is analyzed with the closed loop system dynamics and the aiming error dynamics,furthermore,the analytical results are verified through numerical examples,and finally some important conclusions are obtained on the coupling sensitivity,which can be referred to the system design and flying qualities rating for DFC aircraft.
Keywords:coupling sensitivity  aiming error  ideal decoupling  imperfect coupling
本文献已被 CNKI 等数据库收录!
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号