基于Lyapunov分析的高超声速飞行器咒骂飞行超扭滑模控制

C. Mu, Changyin Sun, Chengshan Qian, Ruimin Zhang
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引用次数: 8

摘要

本文研究了吸气式高超声速飞行器巡航飞行的跟踪控制问题,利用超扭转算法设计了连续控制器。利用非线性变换,建立了高超声速飞行器面向控制的模型。设计了一种基于超扭转算法的二阶滑模控制器,用于速度和高度的跟踪,并利用Lyapunov方法分析了闭环系统的稳定性,证明了滑模曲面在有限时间内收敛。超扭滑模控制不仅具有抑制抖振的能力,而且对变参数具有较强的鲁棒性。仿真结果表明,该方法有效地减少了抖振,并保证了鲁棒性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Super-twisting sliding mode control based on Lyapunov analysis for the cursing flight of hypersonic vehicles
In this paper, the tracking control for air-breathing hypersonic vehicles in cruising flight is studied, where the super-twisting algorithm is utilized to design a continuous controller. The nonlinear transformation is used to clarify a control-oriented model for hypersonic vehicles. A second order sliding mode controller based on the super-twisting algorithm is designed for the tracking of velocity and altitude, and Lyapunov approach is involved to analyze the stability of closed loop system, which also demonstrates that sliding mode surfaces converge in a finite time. The super-twisting sliding mode control has the ability to reduce chattering and also is robust against varying parameters. Simulations are shown to validate that the proposed method has reduced chattering efficiently and the robustness has been also guaranteed.
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