Robust Trajectory Tracking Control for Uncertain 3-DOF Helicopters With Prescribed Performance

被引:30
作者
Verginis, Christos K. [1 ]
Bechlioulis, Charalampos P. [2 ]
Soldatos, Argiris G. [3 ]
Tsipianitis, Dimitris [2 ]
机构
[1] Univ Texas, Oden Inst Computat Engn & Sci, Austin, TX 78705 USA
[2] Univ Patras, Div Syst & Control, Dept Elect & Comp Engn, Patras 26504, Greece
[3] Natl Tech Univ Athens, Dept Elect & Comp Engn, Zografos 15780, Greece
关键词
Prescribed performance; three-degree-of-freedom (DOF) helicopter; trajectory tracking control; LABORATORY HELICOPTER; ADAPTIVE-CONTROL; BENCHMARK; DESIGN; MOTION;
D O I
10.1109/TMECH.2021.3136046
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 article presents a robust control scheme for the trajectory tracking problem of a three-degree-of-freedom helicopter with prescribed transient and steady-state performance. The control design does not employ any information regarding the dynamics of the system. In addition, the transient and steady-state response of the system with respect to a given time-varying trajectory is a priori and explicitly imposed by certain designer-specified performance functions and is fully decoupled from the control gain selection and the dynamic model parameters. Finally, both simulation and experimental results verify the theoretical findings.
引用
收藏
页码:3559 / 3569
页数:11
相关论文
共 32 条
[1]  
Andrievsky B, 2007, P AMER CONTR CONF, P621
[2]   Robust Adaptive Control of Feedback Linearizable MIMO Nonlinear Systems With Prescribed Performance [J].
Bechlioulis, Charalampos P. ;
Rovithakis, George A. .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 2008, 53 (09) :2090-2099
[3]   A low-complexity global approximation-free control scheme with prescribed performance for unknown pure feedback systems [J].
Bechlioulis, Charalampos P. ;
Rovithakis, George A. .
AUTOMATICA, 2014, 50 (04) :1217-1226
[4]   Prescribed Performance Adaptive Control for Multi-Input Multi-Output Affine in the Control Nonlinear Systems [J].
Bechlioulis, Charalampos P. ;
Rovithakis, George A. .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 2010, 55 (05) :1220-1226
[5]  
Bressan A, 2007, INTRO MATH THEORY CO, V2
[6]   Robust regulation for a 3-DOF helicopter via sliding-mode observation and identification [J].
Ferreira de Loza, A. ;
Rios, H. ;
Rosales, A. .
JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS, 2012, 349 (02) :700-718
[7]  
Gao WN, 2016, P AMER CONTR CONF, P2512, DOI 10.1109/ACC.2016.7525294
[8]   Sampled-data-based adaptive optimal output-feedback control of a 2-degree-of-freedom helicopter [J].
Gao, Weinan ;
Huang, Mengzhe ;
Jiang, Zhong-Ping ;
Chai, Tianyou .
IET CONTROL THEORY AND APPLICATIONS, 2016, 10 (12) :1440-1447
[9]  
Iqbal A, 2005, IEEE DECIS CONTR P, P4047
[10]  
Khalil, 2002, CONTROL NONLINEAR SY