A research on state identification and control method based on extended state observer

被引：0

作者：

Wei, Zhenyan ^{[1
,2
]}

Wei, Yiyin ^{[2
]}

机构：

[1] BeiHang Univ, Sch Automat Sci & Elect Engn, Beijing, Peoples R China

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

来源：

2018 14TH IEEE/ASME INTERNATIONAL CONFERENCE ON MECHATRONIC AND EMBEDDED SYSTEMS AND APPLICATIONS (MESA) | 2018年

关键词：

hypersonic vehicle; extended state observer (ESO); equilibrium identification; DISTURBANCE REJECTION CONTROL;

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 paper focuses on the study of the transition control of hypersonic vehicles with two stages of flight. An active disturbance rejection controller with special instruction generation and double-loop extended state observers (ESO) is proposed, which realizes the identification and control of the equilibrium state. Both instruction and observers design method are present to ensure the accuracy as well as convergence. Simulation results show that this method is effective and feasible.

引用

页数：5

共 11 条

[1]

[陈增强 Chen Zengqiang], 2013, [自动化学报, Acta Automatica Sinica], V39, P574

[2]

Fiorentini L., 2007, AIAA GUIDANCE NAVIGA

[3] Robust feedback linearization using extended high-gain observers [J].

Freidovich, Leonid B. ;

Khalil, Hassan K. .

PROCEEDINGS OF THE 45TH IEEE CONFERENCE ON DECISION AND CONTROL, VOLS 1-14, 2006, :983-+

[4]

Gao ZQ, 2006, P AMER CONTR CONF, V1-12, P2399

[5]

Han J., 2008, Active Disturbance Rejection Control Technique-The Technique for Estimating and Compensating the Uncertainties

[6]

Hank J., 2008, 15 AIAA INT SPACE PL, P2540, DOI [10.2514/6.2008-2540, DOI 10.2514/6.2008-2540]

[7]

Heiser William H., 1994, HYPERSONIC AIRBREATH, P6

[8]

Jingqing H., 1995, CONTROL DECISION, V1

[9]

Lai Ai-fang, 2012, Control Theory & Applications, V29, P401

[10] A DSP-based active disturbance rejection control design for a 1-kW H-bridge dc-dc power converter [J].

Sun, BS ;

Gao, ZQ .

IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS, 2005, 52 (05) :1271-1277

← 1 2 →