Robust adaptive control of UAV

被引：0

作者：

Zhang, Guobing ^{[1
]}

Tong, Guan ^{[1
]}

Chen, Pengyun ^{[1
]}

机构：

[1] North China Univ, Sch Mech & Elect Engn, Taiyuan 030051, Shanxi, Peoples R China

来源：

PROCEEDINGS OF THE 33RD CHINESE CONTROL AND DECISION CONFERENCE (CCDC 2021) | 2021年

关键词：

Robust control; linearization; weight function; MATLAB simulation;

D O I：

10.1109/CCDC52312.2021.9601561

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

Aiming at the problems of UAV dynamic modeling error and flight interference, robust control algorithm is introduced in this paper. Based on the establishment of UAV motion equation, the state equation of robust control is obtained by linearization, then the weight function is selected and the controller is designed. MATLAB simulation results show that Compared with PI control, robust longitudinal control of UAV has the characteristics of fast response, small overshoot, short adjustment time and insensitive to modeling error, which shows good control performance.

引用

页码：5181 / 5184

页数：4

共 12 条

[1] DEVELOPING A KNOWLEDGE PROCESS QUALITY MODEL EVALUATION SYSTEM USING COMMONKADS
Andrade, Javier
Ares, Juan
Garcia, Rafael
Rodriguez, Santiago
Suarez, Sonia
[J]. ICAART: PROCEEDINGS OF THE 4TH INTERNATIONAL CONFERENCE ON AGENTS AND ARTIFICIAL INTELLIGENCE, VOL 1, 2012, : 459 - 464
[2] Chunyu J.M., 2005, AERODYNAMIC MISSILE, P23
[3] Dai D, 2013, COMMAND INFORM SYSTE, V4, P7, DOI [10.3969/Lissn.1674-909X.2013.01.002, DOI 10.3969/LISSN.1674-909X.2013.01.002]
[4] Jeannerot R, 1999, J HIGH ENERGY PHYS
[5] Liu S., 2014, FLIGHT DYNAMICS CONT
[6] Qin M., 2007, AERODYNAMIC MISSILE, P36
[7] Szabolcsi Robert, 2018, LAND FORCES ACAD REV, V23
[8] Wang S.T., 2015, DESIGN FLIGHT CONTRO
[9] Wu X., 1997, J TSINGHUA U NAT SCI, P29, DOI [10.16511/j.cnki.qhdxxb.1997.01.007, DOI 10.16511/J.CNKI.QHDXXB.1997.01.007]
[10] Yuan PH, 2018, IEEE WIREL COMMUNN, P49, DOI 10.1109/WCNCW.2018.8369005

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