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Variable-Structure Near-Space Vehicles with Time-Varying State Constraints Attitude Control Based on Switched Nonlinear System

机译:时变状态约束的变结构近空间飞行器基于切换非线性系统的姿态控制

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摘要

This study is concerned with the attitude control problem of variable-structure near-space vehicles (VSNSVs) with time-varying state constraints based on switched nonlinear system. The full states of vehicles are constrained in the bounded sets with asymmetric time-varying boundaries. Firstly, considering modeling uncertainties and external disturbances, an extended state observer (ESO), including two distinct linear regions, is proposed with the advantage of avoiding the peaking value problem. The disturbance observer is utilized to estimate the total disturbances of the attitude angle and angular rate subsystems, which are described in switched nonlinear systems. Then, based on the estimation values, the asymmetric time-varying barrier Lyapunov function (BLF) is employed to construct the active disturbance rejection controller, which can ensure the full state constraints are not violated. Furthermore, to resolve the ‘explosion of complexity’ problem in backstepping control, a modified dynamic surface control is proposed. Rigorous stability analysis is given to prove that all signals of the closed-loop system are bounded. Numerical simulations are carried out to demonstrate the effectiveness of the proposed control scheme.
机译:本研究涉及基于切换非线性系统的具有时变状态约束的变结构近太空飞行器(VSNSV)的姿态控制问题。车辆的完整状态被约束在具有不对称时变边界的有界集合中。首先,考虑到建模的不确定性和外部干扰,提出了一个扩展状态观察器(ESO),它包括两个不同的线性区域,其优点是避免了峰值问题。扰动观测器用于估计姿态角和角速率子系统的总扰动,这在开关非线性系统中进行了描述。然后,基于估计值,采用非对称时变屏障Lyapunov函数(BLF)构造有源干扰抑制控制器,可以确保不违反完整状态约束。此外,为解决反步控制中的“复杂性爆炸”问题,提出了一种改进的动态表面控制。进行了严格的稳定性分析,以证明闭环系统的所有信号都是有界的。进行了数值模拟,以证明所提出的控制方案的有效性。

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