摘要
本文根据理论研究和飞行实测结果,探讨确定直升机四个操纵,即总距、纵向和横向周期操纵、尾桨距操纵范围的方法,以及应考虑的飞行状态。
The paper, based on theoretic resarch and flight tesl results, studies how to determine four controls of helicopter, it control range method of collective pitch. Longitudinal and lateral control, tail rotor collective pitch,and flight conditions that should be considered.
出处
《直升机技术》
2000年第1期1-6,共6页
Helicopter Technique
