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Merge pull request #1567 from DhruvJ22/src_constants_mean_elements
Added GM of various moons and mean distances of multiple systems
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""" | ||
@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: | ||
* NASA. (n.d.). Approximate positions of the planets. NASA., | ||
from https://ssd.jpl.nasa.gov/planets/approx_pos.html | ||
Low precision mean distance between planet-moon were obtained from: | ||
* NASA. (n.d.). Planetary satellite mean elements. NASA. | ||
from https://ssd.jpl.nasa.gov/sats/elem/sep.html | ||
All computed at J2000, except "Pluto - Charon" -> Epoch: 2020-01-01.5 TDB | ||
""" | ||
|
||
from astropy import units as u | ||
from astropy.constants import Constant | ||
|
||
__all__ = [ | ||
"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", | ||
] | ||
|
||
mean_a_mercury = Constant( | ||
"mean_a_mercury", | ||
"Mercury's orbit mean semimajor axis around Sun", | ||
(0.38709927 * u.au.to(u.km)), | ||
"km", | ||
0, | ||
"NASA Planetary Satellite Mean Elements", | ||
system="si", | ||
) | ||
|
||
mean_a_venus = Constant( | ||
"mean_a_venus", | ||
"Venus's orbit mean semimajor axis around Sun", | ||
(0.72333566 * u.au.to(u.km)), | ||
"km", | ||
0, | ||
"NASA Planetary Satellite Mean Elements", | ||
system="si", | ||
) | ||
|
||
mean_a_earth = Constant( | ||
"mean_a_earth", | ||
"Earth's orbit mean semimajor axis around Sun", | ||
(1 * u.au.to(u.km)), | ||
"km", | ||
0, | ||
"NASA Planetary Satellite Mean Elements", | ||
system="si", | ||
) | ||
|
||
mean_a_mars = Constant( | ||
"mean_a_moon", | ||
"Mars's orbit mean semimajor axis around Sun", | ||
1.52371034 * u.au.to(u.km), | ||
"km", | ||
0, | ||
"NASA Approximate Position of Planets", | ||
system="si", | ||
) | ||
|
||
mean_a_jupiter = Constant( | ||
"mean_a_jupiter", | ||
"Jupiter's orbit mean semimajor axis around Sun", | ||
(5.20288700 * u.au.to(u.km)), | ||
"km", | ||
0, | ||
"NASA Planetary Satellite Mean Elements", | ||
system="si", | ||
) | ||
|
||
mean_a_saturn = Constant( | ||
"mean_a_saturn", | ||
"Saturn's orbit mean semimajor axis around Sun", | ||
(9.53667594 * u.au.to(u.km)), | ||
"km", | ||
0, | ||
"NASA Planetary Satellite Mean Elements", | ||
system="si", | ||
) | ||
|
||
mean_a_uranus = Constant( | ||
"mean_a_uranus", | ||
"Saturn's orbit mean semimajor axis around Sun", | ||
(19.18916464 * u.au.to(u.km)), | ||
"km", | ||
0, | ||
"NASA Planetary Satellite Mean Elements", | ||
system="si", | ||
) | ||
|
||
mean_a_neptune = Constant( | ||
"mean_a_neptune", | ||
"Neptune's orbit mean semimajor axis around Sun", | ||
(30.06992276 * u.au.to(u.km)), | ||
"km", | ||
0, | ||
"NASA Planetary Satellite Mean Elements", | ||
system="si", | ||
) | ||
|
||
mean_a_moon = Constant( | ||
"mean_a_moon", | ||
"Moon's orbit mean semimajor axis around Earth", | ||
384400, | ||
"km", | ||
0, | ||
"NASA Planetary Satellite Mean Elements", | ||
system="si", | ||
) | ||
|
||
mean_a_phobos = Constant( | ||
"mean_a_phobos", | ||
"Phobos's orbit mean semimajor axis around Mars", | ||
9400, | ||
"km", | ||
0, | ||
"NASA Planetary Satellite Mean Elements", | ||
system="si", | ||
) | ||
|
||
mean_a_deimos = Constant( | ||
"mean_a_deimos", | ||
"Deimos's orbit mean semimajor axis around Mars", | ||
23500, | ||
"km", | ||
0, | ||
"NASA Planetary Satellite Mean Elements", | ||
system="si", | ||
) | ||
|
||
mean_a_europa = Constant( | ||
"mean_a_europa", | ||
"Europa's orbit mean semimajor axis around Jupiter", | ||
671100, | ||
"km", | ||
0, | ||
"NASA Planetary Satellite Mean Elements", | ||
system="si", | ||
) | ||
|
||
mean_a_ganymede = Constant( | ||
"mean_a_ganymede", | ||
"Ganymede's orbit mean semimajor axis around Juputer", | ||
1070400, | ||
"km", | ||
0, | ||
"NASA Planetary Satellite Mean Elements", | ||
system="si", | ||
) | ||
|
||
mean_a_enceladus = Constant( | ||
"mean_a_enceladus", | ||
"Enceladus's orbit mean semimajor axis around Saturn", | ||
238400, | ||
"km", | ||
0, | ||
"NASA Planetary Satellite Mean Elements", | ||
system="si", | ||
) | ||
|
||
mean_a_titan = Constant( | ||
"mean_a_titan", | ||
"Titan's orbit mean semimajor axis around Saturn", | ||
1221900, | ||
"km", | ||
0, | ||
"NASA Planetary Satellite Mean Elements", | ||
system="si", | ||
) | ||
|
||
mean_a_titania = Constant( | ||
"mean_a_titania", | ||
"Titania's orbit mean semimajor axis around Uranus", | ||
436300, | ||
"km", | ||
0, | ||
"NASA Planetary Satellite Mean Elements", | ||
system="si", | ||
) | ||
|
||
mean_a_triton = Constant( | ||
"mean_a_triton", | ||
"Triton's orbit mean semimajor axis around Neptune", | ||
354800, | ||
"km", | ||
0, | ||
"NASA Planetary Satellite Mean Elements", | ||
system="si", | ||
) | ||
|
||
mean_a_charon = Constant( | ||
"mean_a_charon", | ||
"Charon's orbit mean semimajor axis around Pluto", | ||
19600, | ||
"km", | ||
0, | ||
"NASA Planetary Satellite Mean Elements", | ||
system="si", | ||
) |