摘要
本文通过分析控制增稳系统前馈环节对飞机操纵特性的影响,讨论控制增稳系统(CAS)与机械操纵系统(MCS)的相容性问题.最后从飞行力学的角度上,提出系统设计时应注意的几个问题.
In this paper, after analysis the effect for feedforward parameter of control augmentation system to control characteristic of aircraft, the compatibility of control augmentation system and machinery control system is discussed. At last, make some suggestions for design of system in flight dynamics.
出处
《飞行力学》
CSCD
北大核心
1992年第4期24-30,共7页
Flight Dynamics
关键词
控制增稳系统
前馈环节
相容性
Control augmentation system
Machinery control system
Feedforward element
Compatibility
