autopilot steering control system 自动操舵控制系统
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 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。
On the basis of control scheme of autopilot, control law of stable loop and guidance law of automatic guidance system are given. Moreover, pro-proportional guidance law is realized by computer.
在参考自动驾驶仪控制方案的基础上,给出了稳定回路的控制规律和自动导引系统的导引规律,并说明了用计算机实现前置比例导引规律的方法。
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