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Modelling and fault tolerant control for near space vehicles with vertical tail loss

机译:具有垂直尾翼损失的近太空飞行器的建模和容错控制

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摘要

This work focuses on modelling and fault tolerant algorithm design of a damaged near space vehicle. A novel radial basis function (RBF) neural network backstepping fault-tolerant control methodology is developed for attitude control system with damage, which can make system stable and accurately track the desired signals in the presence of vertical tail loss. First, the changing aerodynamic parameters caused by vertical tail loss are used to model damaged attitude dynamics. Second, in view of the established damaged model, a nominal backstepping controller is designed. Then a RBF neural network technology is designed to update the related parameters, which can compensate effects caused by damage and make the system still stable and track the desired signals. Finally, simulation results are provided to show the effectiveness of the proposed RBF neural network backstepping fault-tolerant control scheme.
机译:这项工作的重点是受损近太空飞行器的建模和容错算法设计。针对具有姿态损伤的姿态控制系统,开发了一种新颖的径向基函数(RBF)神经网络backstepping容错控制方法,该方法可以使系统稳定并在垂直尾翼损失的情况下准确跟踪所需信号。首先,由垂直尾翼损失引起的不断变化的空气动力学参数被用来模拟受损的姿态动力学。其次,鉴于已建立的损坏模型,设计了名义上的反推控制器。然后设计了RBF神经网络技术来更新相关参数,该参数可以补偿损坏造成的影响,并使系统保持稳定并跟踪所需的信号。最后,仿真结果表明了所提出的RBF神经网络反推容错控制方案的有效性。

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