Finite-time Dynamic Surface Fault-tolerant Control for Hypersonic Vehicle with Mismatched Disturbances

被引：9
|
作者：
Li, Peng [1 ]
Huang, Peng [1 ]
He, Chen-Yu [1 ]
Liu, Xiao-Qing [2 ]
机构：
[1] Xiangtan Univ, Sch Automat & Elect Informat, Xiangtan 411105, Hunan, Peoples R China
[2] Tsinghua Univ, Dept Precis Instrument, Beijing 100084, Peoples R China
来源：
INTERNATIONAL JOURNAL OF CONTROL AUTOMATION AND SYSTEMS | 2021年 / 19卷 / 07期
关键词：
Actuator faults; finite-time control; hypersonic vehicle; mismatched disturbances; MODE TRACKING CONTROL; ROBUST; INPUT; SATURATION;
D O I：
10.1007/s12555-020-0169-3
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 studies the tracking control problem of hypersonic vehicle in the process of external disturbance, parameters uncertainties and actuator faults. Firstly, a non-triangular velocity and altitude nonlinear subsystem with mismatched disturbances and actuator faults are established based on the feedback linearization model. Secondly, adaptive dynamic surface fault-tolerant controllers are designed for velocity and altitude subsystems by combining nonlinear filter, adaptive control and back-stepping method. Finally, the Lyapunov stability theory and numercial simulation are carried out to verify the availability of the proposed control strategy.
引用
收藏
页码：2309 / 2322
页数：14
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