Runge-Kutta 4th Order Orbit Simulation

Versión 1.0.0 (3,42 KB) por Ozan Kilic
Satellite Propagation with Runge-Kutta 4th Order Numerical Integration Method
4.8
(4)
1,3K Descargas
Actualizado 24 ene 2019

Ver licencia

In celestial mechanics numerical methods are widely used to solve differential equations. In this code, Runge-Kutta 4th Order method is used for numerical integration of equation of orbital motion according to Newton's law of gravitation to simulate object's trajectory around the Earth.

Inputs: Position and Velocity vector (x,y,z,vx,vy,vz)
OR
Keplerian Elements (a, e, i, Omega, w, M)
h = Step Size
steps = Number of Step
Output: Propagated Satellite PV Vector in ECI Frame of Reference

Call: [X_RK] = RK_4(X,h,steps)

Citar como

Ozan Kilic (2025). Runge-Kutta 4th Order Orbit Simulation (https://es.mathworks.com/matlabcentral/fileexchange/70076-runge-kutta-4th-order-orbit-simulation), MATLAB Central File Exchange. Recuperado .

Compatibilidad con la versión de MATLAB
Se creó con R2018b
Compatible con cualquier versión
Compatibilidad con las plataformas
Windows macOS Linux
Etiquetas Añadir etiquetas

Community Treasure Hunt

Find the treasures in MATLAB Central and discover how the community can help you!

Start Hunting!

Versión Publicado Notas de la versión
1.0.0