论文部分内容阅读
本文介绍一种导弹尾翼/舵机非线性颤振分析方法,这种方法是以时域和频域模拟为基础的.文中列举了这种方法的两个应用实例,一是用于有间隙的液压舵机,二是用于有非线性气体动力学的气压舵机.全部研究是使用高级语言ACSL通过计算机仿真作出的.
This paper presents a method of non-linear flutter analysis of missile tail rotor / steering gear, which is based on time-domain and frequency-domain simulation. Two application examples of this method are listed in this paper. Hydraulic steering gear, and the second is for the pneumatic steering gear with nonlinear gas dynamics.All the research is done by computer simulation using high-level language ACSL.