摘要
根据航空惯性试验台刹车控制系统设计需要和系统的特点,提出了飞机刹车装置动力学模型的总体框架,通过MATLAB/Simulink建立了仿真模型并进行仿真。结果表明,本文建立的刹车装置动力学模型简单实用,具有较好的真实性和可靠性,为航空惯性试验台刹车控制系统设计定型与控制算法整定提供了一个很好的研究平台。
According to the design needs and the characteristics of the brake control system of the aviation inertial test bench,the overall framework of the dynamic model of the aircraft brake device is proposed,and the simulation model is established by MATLAB/Simulink.The results show that the dynamic model of the brake device established in the paper is simple and practical,and has good authenticity and reliability.It can provide a good research platform for the design and control algorithm tuning of the brake control system of aviation inertial test bench.
作者
王甘牛
Wang Ganniu(Aircraft Strength Research Institute of China,Xi′an710065,Shaanxi,China)
出处
《工程与试验》
2023年第2期43-46,共4页
Engineering and Test
关键词
航空惯性试验台
刹车装置
仿真
aviation inertial test bench
brake device
simulation
