Aircraft Orbit Simulation Model
Aircraft orbit simulation model developed with reference to standard flight vehicle textbooks, complete with code implementation framework
Satellite Orbit Computation
Essential for GPS positioning accuracy, this MATLAB-based program calculates satellite orbital coordinates through real-time monitoring and orbital position updates, incorporating algorithms for coordinate transformation and ephemeris data processing.
MATLAB Code Implementation for Satellite and Orbit Simulation
This program simulates satellites and orbits using MATLAB, providing learners with practical insights into orbital mechanics through working code examples and visualization techniques.
Establishing GEO and LEO Orbits with Parameter Calculations
Implementation of GEO (Geosynchronous Earth Orbit) and LEO (Low Earth Orbit) models with computational algorithms for azimuth, elevation angular velocities/accelerations, Doppler shifts, and other critical parameters.
Solving the Lambert Problem
This function solves the Lambert orbital boundary value problem by determining the velocity vectors at two specified position vectors given the transfer time between them. The implementation handles both short-way and long-way trajectories with numerical iteration methods to compute orbital parameters, though the approach may produce high delta-v requirements.