Aerodynamic Shape Optimization System of a Canard-Controlled Missile Using Trajectory-Dependent Aerodynamic Coefficients
Author:
Affiliation:
1. GyeongSang National University, Jinju, 660-701, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A32064
Reference21 articles.
1. Eugene, L. F., Tactical Missile Design, AIAA Education Series, AIAA, Reston, VA, 2001, pp.399-415.
2. Optimal External Configuration Design of Unguided Missiles
3. Three-Dimensional Aerodynamic Shape Optimization Using Genetic and Gradient Search Algorithms
4. Missile Aerodynamic Shape Optimization Using Genetic Algorithms
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