MATLAB Implementation for Aircraft Design with Complete Workflow

This document covers the entire aircraft design process, starting from determining fundamental design elements such as overall aircraft parameters, aerodynamic curves, wing loading, and propeller characteristics, to more detailed aspects including airframe structure selection, material choices, flight control system design, and fuel management system planning. The implementation involves MATLAB algorithms for parameter optimization, aerodynamic coefficient calculations using lookup tables or polynomial fittings, and wing load distribution analysis through numerical integration methods. Additionally, the program includes simulation and testing modules for various flight scenarios, along with performance evaluation and monitoring systems for different aircraft components. Each design phase is thoroughly discussed and analyzed using computational methods, incorporating key functions like design constraint validation, performance metric calculations, and safety factor assessments to ensure the final aircraft design meets all technical requirements and demonstrates excellent performance in actual flight conditions.