本文简要地叙述了航天飞行器操纵品质要求研究现状，并与美国军用飞机飞行品质规范进行简单地对比分析。
This paper briefly describes the status of handling qualities requirements of space shuttle orbiter, and presents contrast to flying qualities specification for U. S. military airplanes.
在理解飞机飞行品质规范MIL- STD- 1797A基础上，采用等效系统准则评价了某机的俯仰轴飞行品质。
The handing qualities of aircraft for pitch axis are assessed using equivalent system criteria based on the flying qualities specifications(MIL STD 1797A).
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.
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