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 augmentationsystem.
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。
3
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.