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飞机刹车系统最佳滑移率性能研究
Research on Optimum Slip Ratio Characteristic of Aircraft Braking Systems
【摘要】 在飞机防滑刹车控制优化的研究中,针对飞机防滑刹车系统的非线性、时变和不确定性,从相对滑移率出发,推导了关于闭环PI型迭代学习控制算法的防滑刹车系统模型;利用粒子群算法对迭代控制中的PI参数进行在线实时更新。在参数保持一致的情况下,以matlab7.1为仿真平台、飞机减速率为目标函数,对系统进行仿真与分析,并与传统的PMB+PID算法进行了比较。仿真结果表明,方法效果明显优于PBM+PID算法,证明了ntfj算法在控制性能上的正确性、优越性,对飞机刹车系统优化设计提供了很好的理论依据。
【Abstract】 Due to the features of non- linearity,time- variety and uncertainty of aircraft anti- skid braking system,starting from the relative slip rate,a model of aircraft anti- skid braking system was derived based on closed-loop PI iterative learning control algorithm and the algorithm of Particle Swarm Optimization( PSO) which updates PI parameters of iterative control online and real- time. In the case of the same parameters,taken matlab7. 1 as the simulation platform and the aircraft deceleration rate as the objective function,the system was simulated and the results wer compared with the algorithm of PMB + PID. The simulation results show that the method adopted in the paper is obviously better than the algorithm of PMB + PID. Both the correctness and superiority of the algorithm control characteristic are proved. Simultaneously the method provides good theoretical references for the optimal design for aircraft brake system.
【Key words】 Slip ratio; Aircraft anti-skid braking; Iterative learning; PSO;
- 【文献出处】 计算机仿真 ,Computer Simulation , 编辑部邮箱 ,2014年10期
- 【分类号】V227
- 【被引频次】6
- 【下载频次】155