Satellite Orbital Maneuver Simulation

This document presents a MATLAB program for satellite orbital maneuver simulation and demonstrates how to utilize GPS data for detailed analysis. Satellite orbital maneuver simulation involves creating a mathematical model to replicate a satellite's motion dynamics in orbit. The primary objective of this simulation is to predict and optimize orbital maneuvers, preventing potential collisions or interference with other satellites. In practical applications, such simulations are crucial for pre-launch satellite design/testing and ongoing orbital maintenance during operational phases.

Our implementation incorporates GPS data for validation and analysis. The Global Positioning System (GPS) provides precise location coordinates by receiving signals from navigation satellites. We leverage this data to verify the accuracy of our MATLAB simulation program and evaluate its practical applicability. The code utilizes orbital propagation algorithms (such as Runge-Kutta integration) and coordinate transformation functions to process ephemeris data from GPS satellites. Beyond GPS data, we also explore integrating other data sources like TLE (Two-Line Element) datasets and ground-based observation data to enhance simulation fidelity through multi-source data fusion techniques.