Full Trajectory Simulation of Airborne Airdrop Precision-Guided Munitions

This is a complete trajectory simulation written in MATLAB for airborne airdrop precision-guided weapons. The simulation program models three distinct flight phases: airdrop phase, cruise phase, and terminal guidance phase, with detailed code comments that explain the underlying algorithms and mathematical models. The implementation likely employs numerical integration methods like Runge-Kutta for trajectory calculations and incorporates guidance laws for the terminal phase. This simulation serves as excellent material for research and learning, providing insights into weapon system dynamics and control logic. Furthermore, the program can be utilized for design validation and optimization to ensure weapon accuracy and reliability. Through further development and enhancement, this simulation framework can be extended to model other weapon types or applied in different domains, showcasing modular design principles that allow for easy adaptation of aerodynamic parameters and guidance algorithms.