Simulation of Geosynchronous Satellite Launch Process

In this MATLAB project simulating the geosynchronous satellite launch process, I invested considerable time and effort to master various programming techniques. Through systematic learning of MATLAB's computational methods, I successfully implemented a dynamic simulation that models orbital mechanics using numerical integration approaches like Runge-Kutta methods for trajectory calculations. The project goes beyond basic satellite launch simulation by incorporating advanced programming concepts. I utilized MATLAB's Aerospace Toolbox for celestial mechanics computations, developed custom functions for thrust profile modeling, and created scripts that simulate multi-stage rocket separation dynamics. The implementation includes gravitational force calculations, orbital velocity determinations, and Hohmann transfer orbit simulations using matrix operations and differential equation solvers. This hands-on project significantly enhanced my MATLAB programming skills while improving logical thinking and problem-solving abilities. I implemented coordinate system transformations for Earth-centered inertial frame calculations and developed visualization modules using MATLAB's plotting functions to display real-time trajectory data. The experience reinforced that programming serves not just as a technical tool but as a methodology for developing systematic problem-solving approaches. I hope this project serves as a practical learning resource for MATLAB enthusiasts, demonstrating how to implement complex physical simulations through functions like ode45 for differential equations and quiver plots for vector field visualization. May this example inspire learners to explore diverse programming techniques and computational methods in their own projects.