Secondly, the stability of designed AFCS is analyzed and an amalgamation control mode of damper and stabilityaugmentation 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。
2
In this paper a new parameter plane method is proposed and is used to design the stabilityaugmentation 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。
3
The results show that the stability and control are sufficient, that the flying qualities are satisfactory after stabilityaugmentation, and that the roll attitude protection system works as expected.