This paper introduces the research and application of flight dynamics in design of control augmentation system.
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。
It is a automatic flight control system for three axes, and consists of analog control augmentation system and digital autopilot.
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。
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.
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。
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.
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。
So the result shows that this system can be used to TM image classify and it has a potential to improve its precision with network pattern's augmentation.
即展示了其应用于针混交林tm遥感图像自动分类识别的能力，又验证了该系统具有随网络规模增大而分类精度提高的发展趋势。
Secondly, the stability of designed AFCS is analyzed and an amalgamation control mode of damper and stability augmentation control system is put forward in the paper.
其次，文中对设计的飞控系统进行了稳定性分析，提出阻尼器与增稳控制系统相融合的控制方式。
Lab tests showed that 55% thrust augmentation should be expected; however, differences in the scaled-up system dropped augmentation levels to 19% for the wing and a mere 6% in the canard.
实验室试验表明，55%加力应该有望，但在逐步扩大的制度不同程度下降扩增至19%的机翼和只有6%的谣传。
In this paper a new parameter plane method is proposed and is used to design the stability augmentation control system of a certain type of aircraft and satisfactory results are obtained.
本文提出了一种新的参数平面法，设计了某型歼击机的控制增稳系统，并取得了满意的结果。
The results show that the stability and control are sufficient, that the flying qualities are satisfactory after stability augmentation, and that the roll attitude protection system works as expected.
结果表明，稳定和控制是足够的，飞行品质满意后稳定性增强，滚动姿态保护系统的工作原理。
The results show that the stability and control are sufficient, that the flying qualities are satisfactory after stability augmentation, and that the roll attitude protection system works as expected.
结果表明，稳定和控制是足够的，飞行品质满意后稳定性增强，滚动姿态保护系统的工作原理。
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