摘要
飞机金属表面振动的运动的数学模型具有非线性和自扰动性,通过鲁棒性控制,保障飞机稳定飞行,提出一种基于李雅普洛夫指数泛函的飞机金属表面振动鲁棒性控制算法。通过算法改进和仿真实验,实现飞机控制系统优化,研究结果表明,该控制算法的鲁棒性较好,飞机扰动误差收敛到零。
Dynamic nonlinear and self obsessed with the mathematical model of the motion of the surface vibration of metal plane, controlled by the robustness, stability of aircraft flight security proposed a metal surface vibration robust control algorithm based on Lyapunov exponent function of the aircraft. The results of the study show that the robustness of the control algorithm is better, aircraft disturbance error converges to zero.
出处
《世界有色金属》
2016年第2期106-107,共2页
World Nonferrous Metals