DocumentCode
1634161
Title
Multi-objective evolutionary guidance for swarms
Author
Hughes, Evan J.
Author_Institution
R. Mil. Coll. of Sci., Cranfield Univ., Shrivenham, UK
Volume
2
fYear
2002
fDate
6/24/1905 12:00:00 AM
Firstpage
1127
Lastpage
1132
Abstract
A novel approach for generating optimal flight paths for a swarm of missiles using an on-line, noise-aware, multi-objective evolutionary algorithm is introduced. The trajectory shape is controlled by flying via intermediate points which are adjusted dynamically by the evolutionary algorithm, then towards the point of impact with the target
Keywords
evolutionary computation; missile guidance; position control; flying; impact; intermediate points; missile swarm; multi-objective evolutionary guidance; on-line noise-aware multi-objective evolutionary algorithm; optimal flight path generation; trajectory shape control; Educational institutions; Evolutionary computation; Missiles; Multi-stage noise shaping; Noise generators; Noise robustness; Parameter estimation; Sensor phenomena and characterization; Shape control; Trajectory;
fLanguage
English
Publisher
ieee
Conference_Titel
Evolutionary Computation, 2002. CEC '02. Proceedings of the 2002 Congress on
Conference_Location
Honolulu, HI
Print_ISBN
0-7803-7282-4
Type
conf
DOI
10.1109/CEC.2002.1004401
Filename
1004401
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