Hybrid formation control of the Unmanned Aerial Vehicles

被引:39
作者
Karimoddini, Ali [1 ,2 ]
Lin, Hai [1 ]
Chen, Ben M. [1 ]
Lee, Tong Heng [1 ]
机构
[1] Natl Univ Singapore, Fac Engn, Dept Elect & Comp Engn, Singapore 117576, Singapore
[2] Natl Univ Singapore, Grad Sch Integrat Sci & Engn NGS, Ctr Life Sci CeLS, Singapore 117456, Singapore
关键词
Unmanned Aerial Vehicles (UAVs); Formation control; Hybrid supervisory control; Polar partitioning; UAV;
D O I
10.1016/j.mechatronics.2010.09.007
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
An essential issue in the formation control of Unmanned Aerial Vehicles (UAVs) is to design a reliable controller in their path planner level to handle all interactions between the continuous dynamics of the system and inherent discrete nature of the decision making unit, which has been embedded to coordinate the control submodules. In this paper, we have proposed a new approach of hybrid supervisory control of UAVs for a two-dimensional leader follower formation scenario. The approach is able to comprehensively capture internal relations between the path planner dynamics and the decision making unit of the UAVs. To design such a hybrid supervisory controller for the formation problem, we have introduced a new method of abstraction, based on polar partitioning of the state space. Furthermore, we have utilized the properties of multi-affine vector fields over the polar partitioned space. Within this framework, we design a modular decentralized supervisor in the path planner level of the UAVs to achieve two major goals: first, reaching the formation and second, keeping the formation. In addition, an inter-collision avoidance mechanism has been considered in the controller structure. The approach is robust against uncertainty in the initial state of the system, in the sense that it can bring the follower UAV to the desired position, starting from any arbitrary initial position inside the control horizon. Moreover, the velocity bounds are applied through the design procedure so that the generated velocity references can be given to the lower level of the control hierarchy, as the references to be followed. (C) 2010 Elsevier Ltd. All rights reserved.
引用
收藏
页码:886 / 898
页数:13
相关论文
共 40 条
[1]  
AHMADZADEH A, 2006, P AUVSI C UNM SYST
[2]   Discrete abstractions of hybrid systems [J].
Alur, R ;
Henzinger, TA ;
Lafferriere, G ;
Pappas, GJ .
PROCEEDINGS OF THE IEEE, 2000, 88 (07) :971-984
[3]  
ANTSAKLIS PJ, 1999, LECT NOTES COMPUTER, P1567
[4]   Experimental cooperative control of fixed-wing unmanned aerial vehicles [J].
Bayraktar, S ;
Fainekos, GE ;
Pappas, GJ .
2004 43RD IEEE CONFERENCE ON DECISION AND CONTROL (CDC), VOLS 1-5, 2004, :4292-4298
[5]   Constructing decidable hybrid systems with velocity bounds [J].
Belta, C ;
Habets, LCGJM .
2004 43RD IEEE CONFERENCE ON DECISION AND CONTROL (CDC), VOLS 1-5, 2004, :467-472
[6]   Controlling a class of nonlinear systems on rectangles [J].
Belta, Calin ;
Habets, Luc C. G. J. M. .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 2006, 51 (11) :1749-1759
[7]  
Bryson M, 2007, AEROSP CONF PROC, P862
[8]   Systematic design methodology and construction of UAV helicopters [J].
Cai, Guowei ;
Feng, Lin ;
Chen, Ben M. ;
Lee, Tong H. .
MECHATRONICS, 2008, 18 (10) :545-558
[9]  
Cassandras C. G., 2008, INTRO DISCRETE EVENT
[10]  
Chen Q, 2003, 42ND IEEE CONFERENCE ON DECISION AND CONTROL, VOLS 1-6, PROCEEDINGS, P516