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Adaptive dynamic surface control for a class of MIMO nonlinear systems with actuator failures

机译:具有执行器故障的一类MIMO非线性系统的自适应动态表面控制

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In this article, an adaptive dynamic surface control scheme for a class of MIMO nonlinear systems with actuator failures and uncertainties is presented. In the proposed control scheme, the dynamic changes and disturbances induced by actuator failures are detected and isolated by means of radial basis function neural networks, which also compensate system uncertainties that arise from the mismatch between nominal model and real plant. In the presence of unknown actuation functions, the effectiveness of the control scheme is guaranteed by imposing a structural condition on the actuation matrix. Moreover, the singularity problem that arises from the approximation of unknown actuation functions is circumvented, and thus the use parameter projection is avoided. In this work, the nominal plant is transformed into a suitable form via diffeomorphism. Dynamic surface control design technique is used to develop the control laws. The closed-loop signals are proven to be uniformly ultimately bounded through Lyapunov approach, and the output tracking error is shown to be bounded within a residual set which can be made arbitrarily small by appropriately tuning the controller parameters. Finally, the proposed adaptive control scheme effectiveness is verified by simulation of the longitudinal dynamics of a twin otter aircraft undergoing actuator failures.
机译:本文提出了一种具有执行器故障和不确定性的MIMO非线性系统的自适应动态表面控制方案。在提出的控制方案中,通过径向基函数神经网络检测并隔离了由执行器故障引起的动态变化和扰动,这也补偿了标称模型与实际设备之间不匹配引起的系统不确定性。在存在未知致动功能的情况下,通过在致动矩阵上施加结构条件,可以保证控制方案的有效性。此外,避免了由于未知致动函数的逼近而引起的奇异性问题,因此避免了使用参数投影。在这项工作中,通过变态将标称植物转化为合适的形式。动态表面控制设计技术用于制定控制律。事实证明,通过Lyapunov方法最终可以使闭环信号统一有界,并且输出跟踪误差显示为有界,可以通过适当调整控制器参数将其任意减小。最后,通过仿真双水獭飞机执行器故障的纵向动力学,验证了所提出的自适应控制方案的有效性。

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