Fuzzy terminal sliding-mode control for hypersonic vehicles

被引：4
|
作者：
He, Nai-Bao [1 ,2 ]
Gutierrez, Hector [2 ]
Gao, Qian [3 ]
Jiang, Chang-Sheng [4 ]
机构：
[1] Jiangsu Univ Technol, Sch Elect & Informat Engn, Changzhou 213001, Peoples R China
[2] Florida Inst Technol, Mech & Aerosp Engn, Melbourne, FL 32901 USA
[3] Jiangsu Univ Technol, Sch Comp Engn, Changzhou, Peoples R China
[4] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing, Jiangsu, Peoples R China
来源：
JOURNAL OF INTELLIGENT & FUZZY SYSTEMS | 2017年 / 33卷 / 03期
关键词：
Near-space hypersonic vehicles; fuzzy control; terminal sliding-mode control; variable domain; OUTPUT-FEEDBACK CONTROL; MARKOVIAN JUMP SYSTEMS; FAULT-TOLERANT CONTROL; TRACKING CONTROL;
D O I：
10.3233/JIFS-162404
中图分类号：
TP18 [人工智能理论];
学科分类号：
081104 ; 0812 ; 0835 ; 1405 ;
摘要：
In this paper, a novel flight control scheme is proposed by using the variable domain fuzzy control method. The proposed control strategy can improve control performance of near-space hypersonic vehicles (NHV) despite uncertainties and external disturbances. The control accuracy and anti-interference velocity are improved, and the calculated quantity is decreased by the change of fuzzy domain. To overcome the chattering phenomenon, the dynamic adaptive terminal sliding-mode control (TSMC) strategy is raised. The control law is designed by an intermediate auxiliary systems, step-by-step. Additionally, the Lyapunov method is used to prove that the tracking errors are converged in finite time.
引用
收藏
页码：1831 / 1839
页数：9
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