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On-line RNN compensated second order nonsingular terminal sliding mode control for hypersonic vehicle

机译:高超声速飞行器的在线RNN补偿二阶非奇异终端滑模控制

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摘要

Purpose - The purpose of this paper is to design a robust control scheme to achieve robust tracking of velocity and altitude commands for a general hypersonic vehicle (HSV) in the presence of parameter variations and external disturbances. Design/methodology/approach - The robust control scheme is composed of nonsingular terminal sliding mode control (NTSMC), super twisting control algorithm (STC) and recurrent neural network (RNN). First, by combing a novel NTSMC and STC algorithm, a second order NTSMC approach for HSV is proposed to provide fast, continuous and high precision tracking control. Second to relax the requirements for the bounds of the lumped uncertainties in control design, a RNN disturbance observer is presented to increase the robustness of the control system: The weights of RNN are updated by adaptive laws based on Lyapunov theorem, thus the closed-loop stability can be guaranteed. Findings - Simulation results demonstrate that the proposed method is effective, leading to promising performance. Originality/value - The main contributions of this work are: first, both parameter variations and external disturbances are considered in control design for the longitudinal dynamic model of HSV; and second, the proposed controller can remove chattering and achieve more favorable tracking performances than conventional sliding mode control.
机译:目的-本文的目的是设计一种鲁棒的控制方案,以在存在参数变化和外部干扰的情况下实现对通用超音速飞行器(HSV)的速度和高度命令的鲁棒跟踪。设计/方法/方法-鲁棒控制方案由非奇异终端滑模控制(NTSMC),超扭曲控制算法(STC)和递归神经网络(RNN)组成。首先,通过结合新颖的NTSMC和STC算法,提出了一种用于HSV的二阶NTSMC方法,以提供快速,连续和高精度的跟踪控制。其次,为了放宽对控制设计中集总不确定性范围的要求,提出了一种RNN扰动观测器,以提高控制系统的鲁棒性:根据Lyapunov定理,通过自适应定律更新RNN的权重,从而实现闭环可以保证稳定性。研究结果-仿真结果表明,该方法是有效的,可带来令人鼓舞的性能。原创性/价值-这项工作的主要贡献是:首先,在HSV纵向动态模型的控制设计中考虑了参数变化和外部干扰。其次,与传统的滑模控制相比,所提出的控制器可以消除颤动并获得更好的跟踪性能。

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