Skip to content
This repository has been archived by the owner on Oct 14, 2023. It is now read-only.

Commit

Permalink
Merge pull request #1567 from DhruvJ22/src_constants_mean_elements
Browse files Browse the repository at this point in the history
Added GM of various moons and mean distances of multiple systems
  • Loading branch information
astrojuanlu committed Aug 12, 2022
2 parents 9785913 + 7aebadd commit d4ab8fa
Show file tree
Hide file tree
Showing 2 changed files with 344 additions and 0 deletions.
117 changes: 117 additions & 0 deletions src/poliastro/constants/general.py
Original file line number Diff line number Diff line change
Expand Up @@ -49,6 +49,15 @@
"GM_neptune",
"GM_pluto",
"GM_moon",
"GM_phobos",
"GM_deimos",
"GM_europa",
"GM_ganymede",
"GM_enceladus",
"GM_titan",
"GM_titania",
"GM_triton",
"GM_charon",
"M_earth",
"M_jupiter",
"M_sun",
Expand Down Expand Up @@ -239,6 +248,114 @@
system="si",
)

# NASA. (n.d.). Planetary satellite physical parameters. NASA.
# from https://ssd.jpl.nasa.gov/sats/phys_par/sep.html
GM_phobos = Constant(
"GM_phobos",
"Phobos gravitational constant",
0.0007087,
"km3 / (s2)",
0.0000006,
"NASA Planetary Satellite Physical Parameters",
system="si",
)

# NASA. (n.d.). Planetary satellite physical parameters. NASA.
# from https://ssd.jpl.nasa.gov/sats/phys_par/sep.html
GM_deimos = Constant(
"GM_deimos",
"Deimos gravitational constant",
0.0000962,
"km3 / (s2)",
0.0000028,
"NASA Planetary Satellite Physical Parameters",
system="si",
)

# NASA. (n.d.). Planetary satellite physical parameters. NASA.
# from https://ssd.jpl.nasa.gov/sats/phys_par/sep.html
GM_europa = Constant(
"GM_europa",
"Europa gravitational constant",
3202.71210,
"km3 / (s2)",
0.00050,
"NASA Planetary Satellite Physical Parameters",
system="si",
)

# NASA. (n.d.). Planetary satellite physical parameters. NASA.
# from https://ssd.jpl.nasa.gov/sats/phys_par/sep.html
GM_ganymede = Constant(
"GM_ganymede",
"Ganymede gravitational constant",
9887.83275,
"km3 / (s2)",
0.00017,
"NASA Planetary Satellite Physical Parameters",
system="si",
)

# NASA. (n.d.). Planetary satellite physical parameters. NASA.
# from https://ssd.jpl.nasa.gov/sats/phys_par/sep.html
GM_enceladus = Constant(
"GM_enceladus",
"Enceladus gravitational constant",
7.21037,
"km3 / (s2)",
0.00009,
"NASA Planetary Satellite Physical Parameters",
system="si",
)

# NASA. (n.d.). Planetary satellite physical parameters. NASA.
# from https://ssd.jpl.nasa.gov/sats/phys_par/sep.html
GM_titan = Constant(
"GM_titan",
"Titan gravitational constant",
8978.13710,
"km3 / (s2)",
0.00025,
"NASA Planetary Satellite Physical Parameters",
system="si",
)

# NASA. (n.d.). Planetary satellite physical parameters. NASA.
# from https://ssd.jpl.nasa.gov/sats/phys_par/sep.html
GM_titania = Constant(
"GM_titania",
"Titania gravitational constant",
226.9,
"km3 / (s2)",
4.61,
"NASA Planetary Satellite Physical Parameters",
system="si",
)

# NASA. (n.d.). Planetary satellite physical parameters. NASA.
# from https://ssd.jpl.nasa.gov/sats/phys_par/sep.html
GM_triton = Constant(
"GM_triton",
"Triton gravitational constant",
1428.49546,
"km3 / (s2)",
0.61603,
"NASA Planetary Satellite Physical Parameters",
system="si",
)

# NASA. (n.d.). Planetary satellite physical parameters. NASA.
# from https://ssd.jpl.nasa.gov/sats/phys_par/sep.html
GM_charon = Constant(
"GM_charon",
"Charon gravitational constant",
105.88,
"km3 / (s2)",
0.28,
"NASA Planetary Satellite Physical Parameters",
system="si",
)

# Archinal, B. A., Acton, C. H., A’Hearn, M. F., Conrad, A., Consolmagno,
# G. J., Duxbury, T., … Williams, I. P. (2018). Report of the IAU Working
# Group on Cartographic Coordinates and Rotational Elements: 2015. Celestial
Expand Down
227 changes: 227 additions & 0 deletions src/poliastro/constants/mean_elements.py
Original file line number Diff line number Diff line change
@@ -0,0 +1,227 @@
"""
@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",
)

0 comments on commit d4ab8fa

Please sign in to comment.