Adaptive Neural Network-Based Fault-Tolerant Control of 2-DOF Helicopter With Output Constraints

Zhijia Zhao, Jian Zhang, Jianing Zhang, Tao Zou
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Abstract

In this paper, we propose an adaptive neural network-based fault-tolerant control for the two-degree of freedom (DOF) helicopter system with actuator fault and output constraints. First, the radial basis function neural network is used to estimate the uncertainty of the system. Moreover, adaptive auxiliary parameters are used to compensate the actuator failure. And then, the barrier Lyapunov function is adopted to deal with the output constraints in the system. By analyzing the stability of Lyapunov function, it is strictly proved that the closed-loop system is semi-globally uniform and bounded, and under the combined action of actuator fault and output constraints, accurate tracking control performance is achieved. Finally, the simulation results in the 2-DOF helicopter system show the effectiveness of the control strategy.
基于输出约束的二自由度直升机自适应神经网络容错控制
针对具有执行器故障和输出约束的二自由度直升机系统,提出了一种基于自适应神经网络的容错控制方法。首先,利用径向基函数神经网络对系统的不确定性进行估计。此外,采用自适应辅助参数对执行器故障进行补偿。然后,采用势垒Lyapunov函数来处理系统中的输出约束。通过分析Lyapunov函数的稳定性,严格证明了闭环系统是半全局一致有界的,并且在执行器故障和输出约束的共同作用下,实现了精确的跟踪控制性能。最后,对二自由度直升机系统进行了仿真,验证了该控制策略的有效性。
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