Research on Optimization Strategy of Missile Preliminary Design

• 出 处: Computer Aided Drafting,Design and Manufacturing
• 发表日期: 2004年01期
• 关键词: missile dimensionality propulsion trajectory Approximation preliminary weights s

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.

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.