摘要
在国外有关文献提出的驾驶员模型基础上,根据实际飞行的情况,对驾驶员的操纵速率提出了限制。研究了操纵速率变化时对驾驶员诱发振荡(PIO)的影响,着重研究了以杆力变化率表示的驾驶员操纵速率对人—机系统稳定性的影响。
In this paper, on the basis of the pilot mode proposed in reference and practical flight, the limits for control rate of stick are suggested. The influence of control rate on PIO is researched. When the limits of control rate of stick are changed the whole man-plane system's stability is also studied.
出处
《飞行力学》
CSCD
北大核心
1993年第2期79-83,共5页
Flight Dynamics
关键词
诱发振荡
操纵性
人-机系统
PIO (Pilot-Induced Oscillation) Control rate Man-plane system
