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
[1]   Trajectory-tracking and path-following of underactuated autonomous vehicles with parametric modeling uncertainty [J].
Aguiar, A. Pedro ;
Hespanha, Joao P. .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 2007, 52 (08) :1362-1379
[2]   The explicit linear quadratic regulator for constrained systems [J].
Bemporad, A ;
Morari, M ;
Dua, V ;
Pistikopoulos, EN .
AUTOMATICA, 2002, 38 (01) :3-20
[3]   State-dependent Riccati equation control for small autonomous helicopters [J].
Bogdanov, Alexander ;
Wan, Eric .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2007, 30 (01) :47-60
[4]  
Castillo C.L., 2007, P 15 MEDITERRANEAN C, P1, DOI 10.1109/MED.2007.4433726
[5]   Optimal control of nonlinear systems: a predictive control approach [J].
Chen, WH ;
Ballance, DJ ;
Gawthrop, PJ .
AUTOMATICA, 2003, 39 (04) :633-641
[6]   Nonlinear disturbance observer-enhanced dynamic inversion control of missiles [J].
Chen, WH .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2003, 26 (01) :161-166
[7]  
GAVRILETS V, 2003, THESIS MIT BOSTON
[8]   SYNTHESIS OF A HELICOPTER FULL-AUTHORITY CONTROLLER [J].
HEIGES, MW ;
MENON, PKA ;
SCHRAGE, DP .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1992, 15 (01) :222-227
[9]  
Isidori A, 1995, NONLINEAR CONTROL SYSTEMS DESIGN 1995, VOLS 1 AND 2, P87
[10]   Adaptive trajectory control for autonomous helicopters [J].
Johnson, EN ;
Kannan, SK .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2005, 28 (03) :524-538