飞机增稳 (stability augmentation of aircraft)
介绍了飞行力学在某型飞机控制增稳系统设计中的研究和应用。
This paper introduces the research and application of flight dynamics in design of control augmentation system.
文中在给出了固定增益的控制增稳系统的基本组成之后，着重介绍自动驾驶仪的参数选择特点及其对飞机飞行品质的影响。
This paper presents mainly parameter selection characteristic of autopilot and effect to flight quality of aircraft, after a basic configuration of fixed gain control augmentation system is shown.
针对电传控制增稳飞机进行了进场着陆的飞行品质地面模拟试验研究。
The studies of flying qualities during approach to landing for the fly—by—wire aircraft with control and augmented system were conducted on a fixed—base flying quality simulator in this paper.
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