DocumentCode :
2253843
Title :
Coordination and control of multiple UAVs with timing constraints and loitering
Author :
Alighanbari, Mehdi ; Kuwata, Yoshiaki ; How, Jonathan P.
Author_Institution :
Space Syst. Lab., Massachusetts Inst. of Technol., USA
Volume :
6
fYear :
2003
fDate :
4-6 June 2003
Firstpage :
5311
Abstract :
This paper describes methods for optimizing the task allocation problem for a fleet of unmanned aerial vehicles (UAVs) with tightly coupled tasks and rigid relative timing constraints. The overall objective is to minimize the mission completion time for the fleet, and the task assignment must account for differing UAV capabilities and no-fly zones. Loitering times are included as extra degrees of freedom in the problem to help meet the timing constraints. The overall problem is formulated using mixed-integer linear programming (MILP), which gives the globally optimal solution. An approximate decomposition solution method is also used to overcome the computational issues that arise when using MILP for larger problems. The problem is also posed in a way that can be solved using Tabu search. This approach is demonstrated to provide good solutions in reasonable computation times for large problems that are very difficult to solve using the exact or approximate decomposition methods.
Keywords :
aircraft control; linear programming; remotely operated vehicles; search problems; timing; MILP; Tabu search; approximate decomposition solution method; globally optimal solution; mission completion time; mixed-integer linear programming; multiple UAV control; multiple UAV coordination; timing constraints; unmanned aerial vehicles; Constraint optimization; Control systems; Costs; Laboratories; Linear programming; Navigation; Resource management; Space technology; Timing; Unmanned aerial vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 2003. Proceedings of the 2003
ISSN :
0743-1619
Print_ISBN :
0-7803-7896-2
Type :
conf
DOI :
10.1109/ACC.2003.1242572
Filename :
1242572
Link To Document :
بازگشت