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
Link To Document :
بازگشت