Aerospace design optimization using a steady state real-coded genetic algorithm

DOI10.1016/J.AMC.2011.07.038zbMath1333.76064OpenAlexW2139327710MaRDI QIDQ426469

John D. Dyer, Roy J. Hartfield, John E. Burkhalter, Gerry V. Dozier

Publication date: 11 June 2012

Published in: Applied Mathematics and Computation (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.amc.2011.07.038

zbMATH Keywords

liquid propellantrocket propulsionsolid propellantworst performer

Mathematics Subject Classification ID

Flow control and optimization for compressible fluids and gas dynamics (76N25) Genetics and population dynamics (92D99)

Related Items (3)

Shape design optimization of cylindrical tank using B-spline curves ⋮ Improvement analysis and application of real-coded genetic algorithm for solving constrained optimization problems ⋮ Geometricity of genetic operators for real-coded representation

Cites Work

• Optimizing a solid rocket motor boosted ramjet powered missile using a genetic algorithm
• Control system optimization using genetic algorithms
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