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本文介绍了针对 BW—1变稳机而研制的实时在线识别飞机纵向短周期参数系统的原理及方法,并给出一部分试验结果,其中包括对安装于 SB—6试验台上的变稳系统识别结果.
In this paper, the principle and method of real-time on-line identification of longitudinal short cycle parameter system of aircraft developed for BW-1 variable stability machine are introduced. Some experimental results are given, including the identification of a stable system installed on the SB-6 test bench result.