Control Surface Geometry Surrogate-Based Optimization for Spin-Stabilized Projectile Course Correction-Reference-Cited by-同舟云学术

Control Surface Geometry Surrogate-Based Optimization for Spin-Stabilized Projectile Course Correction

Published:2020-02 Issue:2 Volume:58 Page:550-560
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Arnoult Guillaume¹,Zeidler Mickael¹,Garnier Eric²

Affiliation:

1. Nexter Munitions, 18023 Bourges, France

2. ONERA–The French Aerospace Lab, 92190 Meudon, France

Funder

ONERA-The French Aerospace Lab

Nexter Munitions

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference28 articles.

1. DietrichF. “Simulation Numerique du Couplage Entre la Mecanique du vol et L’aerodynamique des Projectiles,” Ph.D. Thesis, Univ. de Poitiers, Poitiers, France, 2003.

2. WhyteH. R. “SPIN-73 an Updated Version of the SPINNER Computer Program,” Picatinny Arsenal TR 11, Dover, NJ, 1973.

3. Comparison of Surrogate Models in a Multidisciplinary Optimization Framework for Wing Design

4. Simulation and Optimization of Flow Control Strategies for Novel High-Lift Configurations

5. Multi-Objective Aerodynamic Exploration of Elements' Setting for High-Lift Airfoil Using Kriging Model

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