航空学报 > 1997, Vol. 18 Issue (1): 117-119

共轴式直升机半差动航向操纵系统

冯亚昌, 杜惠芳   

  1. 北京航空航天大学303教研室, 北京, 100083
  • 收稿日期:1995-06-14 修回日期:1996-03-10 出版日期:1997-02-25 发布日期:1997-02-25

CONTROL SYSTEM OF SEMI DIFFERENTIAL YAWING FOR COAXIAL HELICOPTERS

Feng Yachang, Du Huifang   

  1. Faculty 303, Beijing University of Aeronautics and Astronautics,Beijing,100083
  • Received:1995-06-14 Revised:1996-03-10 Online:1997-02-25 Published:1997-02-25

摘要:

阐述共轴式直升机飞行原理,分析设计了半差动航向操纵系统,经试飞验证该系统的设计是成功的。

关键词: 直升机, 飞行原理, 操纵系统

Abstract:

A description is given on the flight principle of coaxial helicopters, and a control system of semi differential yawing is designed. It is verified through real flight test that the designed system is successful.

Key words: helicopters, flight-principles, control sysytem

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