Adaptive sliding mode back-stepping control for hypersonic flight vehicle with state constraints and unmodeled disturbances

被引：0

作者：

Ma, Fei ^{[1
]}

Wu, Yunjie ^{[2
]}

Liu, Xiaocen ^{[3
]}

Li, Bohao ^{[3
]}

Liu, Xiaodong ^{[4
]}

机构：

[1] Beihang Univ, State Key Lab Virtual Real Technol & Syst, Beijing 100191, Peoples R China

[2] Beihang Univ, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R China

[3] Sci & Technol Aircraft Control Lab, Beijing 100191, Peoples R China

[4] Beijing Aerosp Automat Control Inst, Beijing 100854, Peoples R China

来源：

2020 IEEE 16TH INTERNATIONAL CONFERENCE ON CONTROL & AUTOMATION (ICCA) | 2020年

基金：

中国国家自然科学基金;

关键词：

Adaptive control; back-stepping control; barrier Lyapunov function; hypersonic flight vehicle; sliding mode control; BARRIER LYAPUNOV FUNCTIONS; OUTPUT-FEEDBACK CONTROL; TRACKING CONTROL; SYSTEMS;

D O I：

暂无

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 study presents a finite-time adaptive sliding mode back-stepping controller (FASMBC) for hypersonic flight vehicle (HFV), where the state constraints and unmodeled disturbances are considered. Firstly, the longitudinal model of HFV is decomposed into altitude subsystem and velocity subsystem. Then, sliding mode control and back-stepping logic based on barrier Lyapunov function are merged to design the robust controller for each subsystem. Besides, the adaptive strategy is applied to estimate the unmodeled disturbances. A tracking differentiator is introduced to avoid the "explosion of terms" problem involved in traditional back-stepping control. Finally, the simulation results is provided to illustrate the effectiveness of the proposed control scheme.

引用

页码：1547 / 1552

页数：6

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