Design Methodology of a Mini-Missile Considering Flight Performance and Guidance Precision

Engineering

• Multidisciplinary Design Optimization 100%
• Optimum Design 100%
• Main Body 100%
• Control System 50%
• Aerodynamics 50%
• Optimisation Problem 50%
• Genetic Algorithm 50%
• Flight Dynamics 50%
• Navigation System 50%
• Guidance System 50%
• Shape Design 50%
• Design Objective 50%