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Powered Parafoil Lateral-directional Attitude Angle Control with Adaptive Neural Network

机译:自适应神经网络动力翼型横向姿态角控制

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A lateral-directional relative yaw angle control scheme based on adaptive neural network used to identify online the dynamic erroris proposed to design the command-tracking controller for a powered parafoil system (PPS). The PPS has been studied as a two-body system, similar to a double pendulum, with flexible structure and 8 degrees of freedom (DOF); and, it is difficult to present a precision model. Due to the uncertainties of modeling and the external disturbances, an adaptive parameter adjuster is introduced into the RBF neural network to approximate the dynamic error, which effectively improves the original system's characteristic of poor damping of attitude oscillation. And the adaptive neural network system could not only improve the robustness of the system further, but also improve the tracking precision in the process of adaptive parameters converging. Simulation results show that the proposed scheme can track the maneuver command with higher precision and faster response speed than the natural one, and it is applicable to design the PPS attitude angle controller.
机译:提出了一种基于自适应神经网络的横向相对偏航角控制方案,用于在线识别动态误差,设计了动力翼型系统(PPS)的指令跟踪控制器。 PPS已被研究为类似于双摆的两体系统,具有灵活的结构和8个自由度(DOF)。而且,很难给出一个精确的模型。由于建模的不确定性和外部干扰,将自适应参数调节器引入到RBF神经网络中以近似动态误差,从而有效地改善了原始系统的姿态振荡阻尼性差的特性。自适应神经网络系统不仅可以进一步提高系统的鲁棒性,而且可以在自适应参数收敛的过程中提高跟踪精度。仿真结果表明,该方案比自然方案具有更高的跟踪精度和响应速度,适用于PPS姿态角控制器的设计。

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