DocumentCode
3266162
Title
Path Planning of Parafoil System Based on Particle Swarm Optimization
Author
Zhao, Liu ; Jianyi, Kong
Author_Institution
Coll. of Comput. Sci. & Technol., Wuhan Univ. of Sci. & Technol., Wuhan, China
Volume
1
fYear
2009
fDate
6-7 June 2009
Firstpage
450
Lastpage
453
Abstract
The paper describes the general controlling methods of controllable parafoil and designs a parafoil path planning method based on optimal control. To improve the accuracy of falling point and reducing manipulation quantity, this method transforms path planning of parafoil into parameter optimization by using the improved particle swarm optimization algorithm. Such an algorithm is effective for reaching a ideal solution, which is also the similar optimal solution of parafoil path planning. To verify the performance and the feasibility of this method, the traditional subdivision control method and optimal control method are compared respectively in simulation environment. Experiments show that the optimal control method of the parafoil path planning based on PSO can improve the accuracy of falling point and falling direction as well as reducing manipulation quantity.
Keywords
aerospace components; aerospace control; control system synthesis; optimal control; particle swarm optimisation; path planning; controllable parafoil; manipulation quantity; optimal control; parafoil system; particle swarm optimization; path planning; subdivision control method; Control systems; Educational institutions; Optimal control; Paper technology; Particle swarm optimization; Path planning; Proportional control; Space technology; Space vehicles; Wind; PSO algotithm; controllable parafoil; path planning;
fLanguage
English
Publisher
ieee
Conference_Titel
Computational Intelligence and Natural Computing, 2009. CINC '09. International Conference on
Conference_Location
Wuhan
Print_ISBN
978-0-7695-3645-3
Type
conf
DOI
10.1109/CINC.2009.131
Filename
5231102
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