一种改进的基于神经网络的自主飞行器传感器故障检测与估计策略

Mati Ullah, Chunhui Zhao, Hamid Maqsood, Mahmood Ul Hassan, M. Humayun
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引用次数: 3

摘要

本文旨在设计一种自适应非线性策略,能够及时检测和重建自主飞行器姿态传感器的故障,并且比文献中其他传统方法具有更高的精度。该方案将基线非线性控制器与改进的径向基函数神经网络(IRBFNN)相结合,用于检测自主飞行器姿态传感器可能出现的各种异常和故障。采用积分滑模概念作为IRBFNN的自调谐权值更新律,以优化IRBFNN的学习能力,同时避免了计算复杂度。仿真结果和稳定性分析验证了该方法相对于其他传统方法的优越性。结果针对四旋翼飞行器突发性、初发性和间歇性故障,将该控制算法与传统径向基函数神经网络(RBFNN)、多层感知器神经网络(MLPNN)和高增益观测器(HGO)的控制性能进行了比较。仿真结果表明,该算法在故障检测和故障估计方面的性能相对较好。为了提高自主飞行器在飞行过程中的稳定性和安全性,姿态传感器故障的快速识别和重建一直起着至关重要的作用。高效的故障检测与估计方案是实现无人飞行器无差错安全飞行任务的必要条件。该方案引入RBFNN技术,对四旋翼姿态传感器故障和故障进行有效检测和估计。利用积分滑模效应作为网络的反向传播律,自动修改网络的学习参数,与传统的神经网络反向传播律相比,提高了网络的学习能力。与其他已研究的方法相比,该方法在各种故障的检测和估计方面取得了显著的效果。
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Improved neural network-based sensor fault detection and estimation strategy for an autonomous aerial vehicle
PurposeThis paper aims to design an adaptive nonlinear strategy capable of timely detection and reconstruction of faults in the attitude’s sensors of an autonomous aerial vehicle with greater accuracy concerning other conventional approaches in the literature.Design/methodology/approachThe proposed scheme integrates a baseline nonlinear controller with an improved radial basis function neural network (IRBFNN) to detect different kinds of anomalies and failures that may occur in the attitude’s sensors of an autonomous aerial vehicle. An integral sliding mode concept is used as auto-tune weight update law in the IRBFNN instead of conventional weight update laws to optimize its learning capability without computational complexities. The simulations results and stability analysis validate the promising contributions of the suggested methodology over the other conventional approaches.FindingsThe performance of the proposed control algorithm is compared with the conventional radial basis function neural network (RBFNN), multi-layer perceptron neural network (MLPNN) and high gain observer (HGO) for a quadrotor vehicle suffering from various kinds of faults, e.g. abrupt, incipient and intermittent. From the simulation results obtained, it is found that the proposed algorithm’s performance in faults detection and estimation is relatively better than the rest of the methodologies.Practical implicationsFor the improvement in the stability and safety of an autonomous aerial vehicle during flight operations, quick identification and reconstruction of attitude’s sensor faults and failures always play a crucial role. Efficient fault detection and estimation scheme are considered indispensable for an error-free and safe flight mission of an autonomous aerial vehicle.Originality/valueThe proposed scheme introduces RBFNN techniques to detect and estimate the quadrotor attitude’s sensor faults and failures efficiently. An integral sliding mode effect is used as the network’s backpropagation law to automatically modify its learning parameters accordingly, thereby speeding up the learning capabilities as compared to the conventional neural network backpropagation laws. Compared with the other investigated techniques, the proposed strategy achieve remarkable results in the detection and estimation of various faults.
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来源期刊
CiteScore
3.50
自引率
0.00%
发文量
21
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