RESEARCH ON OPTIMIZATION STRATEGY OF MISSILE PRELIMINARY DESIGN

• 来源期刊: 计算机辅助绘图.设计与制造(英文版)
• 学科: 工学
• 关键词: 自动
• 年，卷（期）: 2004,（1）
• 页码范围: 1-6
• 页数: 6页
• 分类号: TJ760
• 语种: 中文

摘要

Two system optimization architectures are proposed for missile system preliminary design, taking into account aerodynamics, weights and sizing, propulsion and trajectory. Approximation methods are investigated in order to reduce problem dimensionality and to improve the efficiency of optimization process.