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Disturbance-Observer-Based Robust Flight Control for Hypersonic Vehicles Using Neural Networks

机译:基于神经网络的高超声速飞行器基于扰动观测器的鲁棒飞行控制

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In this paper, robust flight control schemes are proposed for the hypersonic vehicle with uncertainties and external disturbances using disturbance observer and neural networks. The nonlinear mathematic model of hypersonic vehicles is firstly transformed into a multivariable linear system with parametric uncertainty, function uncertainty and external disturbance. Considering the system disturbance generated by an external system, the disturbance observer is given to estimate the external disturbance. On the other hand, neural networks are introduced to approximate system function uncertainties. Combing disturbance observer with neural network, the robust flight control scheme is proposed for hypersonic vehicles. To explicitly tackle the control gain constraint problem, the constrained robust flight control is accordingly developed by combing disturbance observer with neural network. In both proposed robust flight control techniques for the hypersonic vehicle, the gain matrix of disturbance observer and the control gain matrix are solved via Linear Matrix Inequality (LMI). Simulation results are presented to illustrate the effectiveness of the proposed robust flight control schemes for the hypersonic vehicle.
机译:本文利用扰动观测器和神经网络,为不确定性和外部扰动的高超声速飞行器提出了鲁棒的飞行控制方案。首先将高超声速飞行器的非线性数学模型转化为具有参数不确定性,功能不确定性和外部干扰的多元线性系统。考虑到外部系统产生的系统干扰,给出了干扰观测器来估计外部干扰。另一方面,引入了神经网络来近似系统功能的不确定性。将干扰观测器与神经网络相结合,提出了高超声速飞行器鲁棒飞行控制方案。为了明确解决控制增益约束问题,通过将干扰观测器与神经网络相结合,发展了约束鲁棒飞行控制。在提出的用于超音速飞行器的鲁棒飞行控制技术中,扰动观测器的增益矩阵和控制增益矩阵都是通过线性矩阵不等式(LMI)求解的。仿真结果表明了所提出的高超音速飞行器鲁棒飞行控制方案的有效性。

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