Multicriteria choice of a carrier aircraft and main design parameters of an air launcher decoy

The multicriteria optimization problem on joint choice of a carrier aircraft and main design parameters of an air launcher decoy are considered. The estimation of the design parameter values for the aerial decoy is based on the statistical data processing with the use of the methods for constructing...

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Bibliographic Details
Published in:Russian aeronautics 2011-03, Vol.54 (1), p.1-8
Main Authors: Moiseev, G. V., Poluboyarinov, P. S.
Format: Article
Language:English
Subjects:
Aerials
Aircraft
Aircraft Equipment
Automotive Engineering
Carriers
Decoys
Design parameters
Engineering
Launchers
Optimization
Regression
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Summary:The multicriteria optimization problem on joint choice of a carrier aircraft and main design parameters of an air launcher decoy are considered. The estimation of the design parameter values for the aerial decoy is based on the statistical data processing with the use of the methods for constructing nonlinear regression. The result of solving this problem is a set of Pareto-optimal geometry characteristics of the carrier aircraft and aerial decoy. A person who is responsible for decision-making should choose the most reasonable variant from these characteristics. An example of solving the problem is presented.
ISSN:1068-7998
1934-7901
DOI:10.3103/S1068799811010016