Explicit non-linear model predictive control for autonomous helicopters

被引:10
作者
Liu, C. [1 ]
Chen, W-H [1 ]
Andrews, J. [2 ]
机构
[1] Univ Loughborough, Dept Aeronaut & Automot Engn, Loughborough LE11 3TU, Leics, England
[2] Univ Nottingham, Nottingham Transportat Engn Ctr, Nottingham NG7 2RD, England
基金
英国工程与自然科学研究理事会;
关键词
TRACKING CONTROL; DESIGN; SYSTEM;
D O I
10.1177/0954410011418585
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Trajectory tracking is a basic function required for autonomous helicopters, but it also poses challenges to control design due to the complexity of helicopter dynamics. This article introduces an explicit model predictive control (MPC) to solve this problem, which inherits the advantages of non-linear MPC but eliminates time-consuming online optimization. The explicit solution to the non-linear MPC problem is derived using Taylor expansion and exploiting the helicopter model. With the explicit MPC solution, the control signals can be calculated instantaneously to respond to the fast dynamics of helicopters and suppress disturbances immediately. On the other hand, the online optimization process can be removed from the MPC framework, which can accelerate the software development and simplify onboard hardware. Due to these advantages of the proposed method, the overall control framework has a low complexity and high reliability, and it is easy to deploy on small-scale helicopters. The proposed explicit non-linear MPC has been successfully validated in simulations and in actual flight tests using a Trex-250 small-scale helicopter.
引用
收藏
页码:1171 / 1182
页数:12
相关论文
共 24 条
[11]  
Kim HJ, 2002, P AMER CONTR CONF, V1-6, P3576, DOI 10.1109/ACC.2002.1024483
[12]   A flight control system for aerial robots: algorithms and experiments [J].
Kim, HJ ;
Shim, DH .
CONTROL ENGINEERING PRACTICE, 2003, 11 (12) :1389-1400
[13]  
Koo TJ, 1998, IEEE DECIS CONTR P, P3635, DOI 10.1109/CDC.1998.761745
[14]   An experimental evaluation of Generalized Predictive Control for Tiltrotor aeroelastic stability augmentation in airplane mode of flight [J].
Kvaternik, RG ;
Piatak, DJ ;
Nixon, MW ;
Langston, CW ;
Singleton, JD ;
Bennett, RL ;
Brown, RK .
JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 2002, 47 (03) :198-208
[15]   Rapid prototyping flight test environment for autonomous unmanned aerial vehicles [J].
Liu, Cunjia ;
Clarke, Jonathan ;
Chen, Wen-Hua ;
Andrews, John .
INTERNATIONAL JOURNAL OF MODELLING IDENTIFICATION AND CONTROL, 2011, 12 (03) :200-209
[16]   Piecewise constant model predictive control for autonomous helicopters [J].
Liu, Cunjia ;
Chen, Wen-Hua ;
Andrews, John .
ROBOTICS AND AUTONOMOUS SYSTEMS, 2011, 59 (7-8) :571-579
[17]   Robust full degree-of-freedom tracking control of a helicopter [J].
Marconi, Lorenzo ;
Naldi, Roberto .
AUTOMATICA, 2007, 43 (11) :1909-1920
[18]   System identification Modeling of a small-scale unmanned rotorcraft for flight control design [J].
Mettler, B ;
Tischler, MB ;
Kanade, T .
JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 2002, 47 (01) :50-63
[19]   Control and perception techniques for aerial robotics [J].
Ollero, A ;
Merino, L .
ANNUAL REVIEWS IN CONTROL, 2004, 28 (02) :167-178
[20]   Design and implementation of an autonomous flight control law for a UAV helicopter [J].
Peng, Kemao ;
Cai, Guowei ;
Chen, Ben M. ;
Dong, Miaobo ;
Lum, Kai Yew ;
Lee, Tong H. .
AUTOMATICA, 2009, 45 (10) :2333-2338