摘要
本文介绍一个自动驾驶仪的参数设计.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.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.
A design of autopilot parameters is presented in this paper. It is a automatic flight control system for three axes, and consists of analog control augmentation system and digital autopilot.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.
出处
《飞行力学》
CSCD
北大核心
1989年第2期33-38,共6页
Flight Dynamics
