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首页> 外文期刊>Circuits, Systems, and Signal Processing >Fault Tolerant Control for Near Space Vehicles with Input Saturation Using Disturbance Observer and Neural Networks
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Fault Tolerant Control for Near Space Vehicles with Input Saturation Using Disturbance Observer and Neural Networks

机译:具有扰动观测器和神经网络的输入饱和的近空间飞行器容错控制。

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In this paper, a fault tolerant sliding mode control scheme is derived for near space vehicles with actuator faults, unknown external disturbance, system uncertainty and input saturation based on disturbance observer and neural networks (NNs). To deal with actuator faults, the radial basis function NNs are employed. The nonlinear disturbance observer is designed to eliminate the effect of external disturbance and system uncertainty. To tackle input saturation, the known bound of saturation is used to design the control law such that the control input is within the bounded range. Lyapunov stability analysis shows that the closed-loop system is stable and all closed-loop signals are uniformly ultimately bounded. Simulation results demonstrate the effectiveness of the developed fault tolerant control scheme, when actuator faults, unknown external disturbance, system uncertainty and input saturation appear simultaneously.
机译:本文基于扰动观测器和神经网络,推导了具有致动器故障,未知外部扰动,系统不确定性和输入饱和的近太空飞行器容错滑模控制方案。为了处理执行器故障,采用了径向基函数NNs。非线性干扰观测器旨在消除外部干扰和系统不确定性的影响。为了解决输入饱和,使用饱和的已知范围来设计控制律,以使控制输入在有界范围内。 Lyapunov稳定性分析表明,闭环系统是稳定的,并且所有闭环信号最终均一地有界。仿真结果表明,当执行器故障,未知外部干扰,系统不确定性和输入饱和同时出现时,所开发的容错控制方案的有效性。

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