This paper presents an approximate analytic method which determines the characteristics of aircraft lateral-directional limit cycle oscillation induced by aerodynamic hysteresis.

本文给出近似解析公式，确定空气动力迟滞引起的飞机横航向极限环振荡特性。

youdao

It features simple structure, good process compatibility and function of temperature hysteresis which prevents the damage by thermal-oscillation.

电路结构简单、工艺兼容性好，同时具有温度的迟滞特性可以更好的保护芯片，避免热振荡的产生。

youdao