In this paper a new parameter plane method is proposed and is used to design the stability augmentation 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。
In this paper a new parameter plane method is proposed and is used to design the stability augmentation 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。
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