Second-Order Dynamic Sliding-Mode Control for Nonminimum Phase Underactuated Hypersonic Vehicles

被引：85

作者：

Wang, Zhi ^{[1
]}

Bao, Weimin ^{[2
]}

Li, Huifeng ^{[1
]}

机构：

[1] Beihang Univ, Sch Astronaut, Beijing 100191, Peoples R China

[2] China Aerosp Sci & Technol Corp, Beijing 100048, Peoples R China

来源：

IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS | 2017年 / 64卷 / 04期

基金：

中国国家自然科学基金;

关键词：

Dynamic sliding manifold (DSM); nonminimum phase; second-order dynamic sliding-mode control (SODSMC); system decomposition; underactuated hypersonic vehicles; TRACKING; SYSTEMS; DESIGN;

D O I：

10.1109/TIE.2016.2633530

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

This paper deals with the second-order dynamic sliding-mode control (SODSMC) problem for nonminimum phase underactuated hypersonic vehicles. First, the underactuated hypersonic vehicle attitude control model is introduced. The normal form and the nonminimum phase nature for the vehicle are discussed. Thus, the nonminimum phase system is divided into the minimum phase subsystem and the nonminimum phase subsystem via the system decomposition approach. Second, the SODSMC scheme is developed. The conventional sliding-mode controller and the second-order dynamic sliding-mode controller are designed for the two subsystems. Besides, the dynamic sliding manifold is provided for the nonminimum phase subsystem. Simulation results for the nonminimum phase underactuated hypersonic vehicle are presented to demonstrate the effectiveness and robustness of the proposed control scheme.

引用

页码：3105 / 3112

页数：8

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