摘要
本文用连续系统数字仿真方法对某变后掠飞机-飞行操纵系统动态特性进行了计算和分析,并与地面模拟试验作了比较。这一仿真结果为新机研制提供了极有益的依据。
The computation and the analysis of the dynamic characteristics of a flight control system for aircraft with changeable swept-back wings are presented.A comparison between the computation and the ground simulation experiment is made. The simulation results provide an extremely valuable basis for the study and manufacture of new aircraft.
关键词
飞机
飞行操纵系统
动态特性
仿真
flight control system, simulation, dynamic characteristics, computative model
