boinor.constants.mean_elements

@author: Dhruv Jain, Multi-Body Dynamics Research Group, Purdue University.

This module complements constants defined in astropy.constants with mean distances between sun-planet and planet-moon systems

Mean distances between the two bodies are required for CR3BP model CR3BP model’s goal is to approximate the behavior of a satellite in an ephemeris model. Thus, it is reasonable to us low precision mean distances values as for more comprehensive mission designs, the CR3BP trajectories are differentially corrected in an ephemeris model with high precision mean distances.

Low precision mean distance between sun-planet were obtained from:

Low precision mean distance between planet-moon were obtained from:

All computed at J2000, except “Pluto - Charon” -> Epoch: 2020-01-01.5 TDB

Attributes

mean_a_mercury

mean_a_venus

mean_a_earth

mean_a_mars

mean_a_jupiter

mean_a_saturn

mean_a_uranus

mean_a_neptune

mean_a_moon

mean_a_phobos

mean_a_deimos

mean_a_europa

mean_a_ganymede

mean_a_enceladus

mean_a_titan

mean_a_titania

mean_a_triton

mean_a_charon

Module Contents

boinor.constants.mean_elements.mean_a_mercury
boinor.constants.mean_elements.mean_a_venus
boinor.constants.mean_elements.mean_a_earth
boinor.constants.mean_elements.mean_a_mars
boinor.constants.mean_elements.mean_a_jupiter
boinor.constants.mean_elements.mean_a_saturn
boinor.constants.mean_elements.mean_a_uranus
boinor.constants.mean_elements.mean_a_neptune
boinor.constants.mean_elements.mean_a_moon
boinor.constants.mean_elements.mean_a_phobos
boinor.constants.mean_elements.mean_a_deimos
boinor.constants.mean_elements.mean_a_europa
boinor.constants.mean_elements.mean_a_ganymede
boinor.constants.mean_elements.mean_a_enceladus
boinor.constants.mean_elements.mean_a_titan
boinor.constants.mean_elements.mean_a_titania
boinor.constants.mean_elements.mean_a_triton
boinor.constants.mean_elements.mean_a_charon