DocumentCode
2300860
Title
Aircraft route optimization using adaptive simulated annealing
Author
Kastella, Keith
Author_Institution
Unisys Electron. & Inf. Syst. Group, Eagan, MN, USA
fYear
1991
fDate
20-24 May 1991
Firstpage
1123
Abstract
It is demonstrated that simulated annealing (SA) is a viable optimization method for use in route optimization for aircraft flying in tactical attack roles at low altitude deep in enemy territory. It is found that adaptive control of the temperature based on a heuristic measure of equilibrium greatly reduces the algorithm´s sensitivity to the cooling rate while giving a 5- to 10-fold speed-up with no adverse impact on the quality of the solutions produced. These results scale nearly linearly with problem size
Keywords
adaptive control; aircraft; military systems; optimisation; scheduling; simulated annealing; adaptive control; adaptive simulated annealing; aircraft; analogy; cooling rate; equilibrium; heuristic measure; route optimization; tactical attack; Aerospace electronics; Aircraft; Cooling; Information systems; Leg; Meeting planning; Optimization methods; Simulated annealing; Stochastic processes; Temperature sensors;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace and Electronics Conference, 1991. NAECON 1991., Proceedings of the IEEE 1991 National
Conference_Location
Dayton, OH
Print_ISBN
0-7803-0085-8
Type
conf
DOI
10.1109/NAECON.1991.165900
Filename
165900
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