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Sliding mode adaptive control for flying robot based on recurrent CMAC algorithm

机译:基于递归CMAC算法的飞行机器人滑模自适应控制

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Sliding mode adaptive control algorithm with recurrent cerebellar model articulatory controller(CMAC) was proposed for a class of uncertain nonlinear systems whose threshold value of lumped disturbance is difficult to measure in practice. The system is divided into nominal model and lumped disturbance term which is composed of modeling error, parameter uncertainties, disturbances, and unmodeled dynamics. Adaptive control is adopted to approach the uncertain input coefficient of the system, robust control is introduced to reduce the lumped disturbance to an acceptant bound within finite time, and sliding mode control is adopted to enable the tracking errors of the uncertain nonlinear system to approximate to zero ultimately. Because the threshold value of lumped disturbance is difficult to measure in practical applications, the recurrent CMAC is used as an observer to approximate it in real time. The asymptotically stability was proved based on Lyapunov stability theory, and simulation results of micro flying robot attitude control indicated that the proposed algorithm improves transient performance and robustness. Research conclusions provide the basis for effective control of complex nonlinear systems.
机译:针对一类不确定的非线性系统,在实践中难以测量集总扰动的阈值,提出了一种基于递归小脑模型关节控制器的滑模自适应控制算法。该系统分为名义模型和集总扰动项,集扰动项由建模误差,参数不确定性,扰动和非建模动力学组成。采用自适应控制来逼近系统的不确定输入系数,引入鲁棒控制以在有限时间内将集总扰动减小到可接受的范围内,并采用滑模控制使不确定非线性系统的跟踪误差近似为最终为零。由于集总扰动的阈值在实际应用中难以测量,因此将循环CMAC用作观察者以实时对其进行逼近。基于Lyapunov稳定性理论证明了渐近稳定性,微型飞行机器人姿态控制的仿真结果表明,该算法提高了暂态性能和鲁棒性。研究结论为有效控制复杂非线性系统提供了基础。

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