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.
这是一个三轴自动飞行控制系统，它由模拟式的控制增稳系统和数字式自动驾驶仪组成。
It is a automatic flight control system for three axes, and consists of analog control augmentation system and digital autopilot.
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.
在直升机飞行控制系统、尤其是控制增稳系统的地面仿真试验中，实施标准的、具有可重复性的杆操纵非常重要。
It is important but difficult to establish uniform and repeatable stick inputs in ground-based simulated experiments of flight control system, especially of stability and control augmentation system.
和实际飞行数据进行的比较表明，模型有相当的准确性，可以用于直升机增稳系统的控制设计。
Real flight data verify that the model is fairly accurate, and can be used in the design of stable augment control system of the helicopter.
和实际飞行数据进行的比较表明，模型有相当的准确性，可以用于直升机增稳系统的控制设计。
Real flight data verify that the model is fairly accurate, and can be used in the design of stable augment control system of the helicopter.
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