Off-Line Offset-Free Output Feedback Model Predictive Control for a Constrained Hypersonic Vehicle Using Polyhedral Invariant Sets

被引：0

作者：

Gao, Haiyan ^{[1
]}

Fu, Bin ^{[1
]}

Zheng, Yunhong ^{[1
]}

Lin, Zhiyong ^{[1
]}

Tang, Weiqiang ^{[2
]}

机构：

[1] Xiamen Univ Technol, Sch Elect Engn & Automat, Xiamen, Peoples R China

[2] Lanzhou Univ Technol, Coll Elect & Informat Engn, Lanzhou, Peoples R China

来源：

2020 CHINESE AUTOMATION CONGRESS (CAC 2020) | 2020年

基金：

中国国家自然科学基金;

关键词：

Hypersonic Vehicle; Output Feedback; Model Predictive Control; Offset-free; Polyhedral Invariant Set; CONTROL DESIGN; FLIGHT CONTROL; DISTURBANCE; TRACKING; SYSTEMS;

D O I：

10.1109/CAC51589.2020.9327743

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

An off-line offset-free output feedback model predictive control (OFMPC) is investigated for a generic hypersonic vehicle (HV) under interferences and parameter uncertainties. Off-line, the disturbance model is constructed, a nonlinear observer and the predictive control laws are designed. On-line, the MPC law is obtained by searching the minimum polyhedron set containing the translation state. Simulation results show that the given reference values of velocity and altitude can be tracked accurately even in the case of uncertain parameters and external disturbances.

引用

页码：4060 / 4065

页数：6

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