Lunar High precision Orbit Propagator

Lunar High precision Orbit Propagator
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Actualizado 13 Sep 2017

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Two main codes are provided:
1) LHPOP runs a GUI to set the all the required inputs as the forces' model for the propagation of a lunar orbiter. The perturbations taken into account are the asymmetry of the lunar gravity field up to 165x165 harmonics, the Sun and Earth attractions, the solar radiation pressure and the Earth's albedo, the general relativity.
2) ORBIT3D permits the visualization and animation in a 3D window and on a planisphere of the motion of the orbiter.
IMPORTANT: mice toolbox (NAIF) is required.
1) Download mice toolbox from https://naif.jpl.nasa.gov/naif/toolkit_MATLAB_PC_Linux_GCC_MATLAB7.x_64bit.html
2) Add the following paths to the default paths of Matlab:
*) mice\lib
*) mice\src\mice
3) Download the ephemerides file "de430.bsp" from https://naif.jpl.nasa.gov/pub/naif/generic_kernels/spk/planets/
4) Copy the ephemerides file into the "ker" folder.

Citar como

Ennio Condoleo (2024). Lunar High precision Orbit Propagator (https://www.mathworks.com/matlabcentral/fileexchange/64408-lunar-high-precision-orbit-propagator), MATLAB Central File Exchange. Recuperado .

Compatibilidad con la versión de MATLAB
Se creó con R2017a
Compatible con cualquier versión
Compatibilidad con las plataformas
Windows macOS Linux
Agradecimientos

Inspirado por: DRAGZOOM - Drag and zoom tool

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Versión Publicado Notas de la versión
1.0