Research on Optimization of Aircraft Vertical Tail Stealth Design Based on Airborne PD Radar

DOI

10.2991/icmse-15.2015.280How to use a DOI?

Keywords

Stealth; optimization design; Kriging model; penetration fight

Abstract

To solve optimization of aircraft vertical tail stealth design under airborne PD radar, the Kriging model based on agent tail stealth characteristics is proposed; Genetic algorithm is applied to optimization calculation based on the tail stealth agent model as objective function and the tail capacity as constraints. The calculation results show that: It is feasible to optimize the stealth design of vertical tail, which can better improve the aircraft lateral stealth performance under the condition of the penetration fight.

Copyright

© 2015, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Hongwei Wang
AU  - Haoran Huang
AU  - Peng Sun
AU  - Yu Cui
PY  - 2015/12
DA  - 2015/12
TI  - Research on Optimization of Aircraft Vertical Tail Stealth Design Based on Airborne PD Radar
BT  - Proceedings of the 2015 6th International Conference on Manufacturing Science and Engineering
PB  - Atlantis Press
SP  - 1552
EP  - 1555
SN  - 2352-5401
UR  - https://doi.org/10.2991/icmse-15.2015.280
DO  - 10.2991/icmse-15.2015.280
ID  - Wang2015/12
ER  -