摘要
针对飞机飞行仿真系统核心模块(飞行动力学和飞行控制模块)进行设计研究,建立了六自由度全量非线性飞行动力学模型适用于程序编程的解算方法,飞机飞行控制模块采用相应飞机的控制律。编制了核心模块程序并组建了通用的飞机飞行仿真系统,通过多次飞行模拟试验表明,所建立的飞行仿真系统具有良好的可操纵性和逼真度,人机界面良好。
This paper designs and researches the key modules （ flight dynamics and flight control） in aircraft flight simulation system, and establishes the compute method of integrated six - degree - freedom nonlinear equation, aircraft flight control system uses control law of the relevant aircraft type. The program of key modules is compiled and the universal aircraft flight simulation system is founded. Through making many flight experiments, the flight simulation system has favorable maneuverability, high fidelity and nice interface.
出处
《飞机设计》
2009年第3期28-32,共5页
Aircraft Design
关键词
飞行仿真
飞行动力学
飞行控制
flight simulation
flight dynamics
flight control
作者简介
龚松波（1978-），男，硕士，工程师。研究方向为飞行仿真。
