debian-skyfield/skyfield/jpllib.py

265 lines
9.5 KiB
Python

"""An interface between JPL ephemerides and Skyfield."""
import os
from collections import defaultdict
from jplephem.exceptions import OutOfRangeError
from jplephem.spk import SPK
from jplephem.names import target_name_pairs
from .constants import AU_KM, DAY_S
from .errors import EphemerisRangeError
from .timelib import calendar_date
from .vectorlib import VectorFunction, VectorSum, _jpl_code_name_dict
_jpl_name_code_dict = dict(
(name, target) for (target, name) in target_name_pairs
)
class SpiceKernel(object):
"""Ephemeris file in NASA .bsp format.
A "Spacecraft and Planet Kernel" (SPK) file from NASA provides
(x,y,z) coordinates for bodies in the Solar System like the Sun,
planets, moons, and spacecraft.
You can download a .bsp file yourself and use this class to open it,
or use the Skyfield ``load()`` function to automatically download a
popular ephemeris. Once loaded, you can print this object to the
screen to see a report on the segments that it includes:
>>> planets = load('de421.bsp')
>>> print(planets)
SPICE kernel file 'de421.bsp' has 15 segments
JD 2414864.50 - JD 2471184.50 (1899-07-28 through 2053-10-08)
0 -> 1 SOLAR SYSTEM BARYCENTER -> MERCURY BARYCENTER
0 -> 2 SOLAR SYSTEM BARYCENTER -> VENUS BARYCENTER
0 -> 3 SOLAR SYSTEM BARYCENTER -> EARTH BARYCENTER
0 -> 4 SOLAR SYSTEM BARYCENTER -> MARS BARYCENTER
0 -> 5 SOLAR SYSTEM BARYCENTER -> JUPITER BARYCENTER
0 -> 6 SOLAR SYSTEM BARYCENTER -> SATURN BARYCENTER
0 -> 7 SOLAR SYSTEM BARYCENTER -> URANUS BARYCENTER
0 -> 8 SOLAR SYSTEM BARYCENTER -> NEPTUNE BARYCENTER
0 -> 9 SOLAR SYSTEM BARYCENTER -> PLUTO BARYCENTER
0 -> 10 SOLAR SYSTEM BARYCENTER -> SUN
3 -> 301 EARTH BARYCENTER -> MOON
3 -> 399 EARTH BARYCENTER -> EARTH
1 -> 199 MERCURY BARYCENTER -> MERCURY
2 -> 299 VENUS BARYCENTER -> VENUS
4 -> 499 MARS BARYCENTER -> MARS
To retrieve the one or more vectors necessary to compute the
position of a body relative to the Solar System barycenter, look up
the body by its name or official SPICE identifying integer:
>>> planets['earth']
<VectorSum of 2 vectors 0 SOLAR SYSTEM BARYCENTER -> 399 EARTH>
>>> planets[499]
<VectorSum of 2 vectors 0 SOLAR SYSTEM BARYCENTER -> 499 MARS>
The result will be a :class:`~skyfield.vectorlib.VectorFunction`
instance that you can ask for a position at a given input time.
"""
def __init__(self, path):
self.path = path
self.filename = os.path.basename(path)
self.spk = SPK.open(path)
self.segments = [SPICESegment(self, s) for s in self.spk.segments]
self.codes = set(s.center for s in self.segments).union(
s.target for s in self.segments)
def __repr__(self):
return '<{0} {1!r}>'.format(type(self).__name__, self.path)
def __str__(self):
segments = self.spk.segments
lines = ['SPICE kernel file {0!r} has {1} segments'
.format(self.filename, len(segments))]
format_date = '{0}-{1:02}-{2:02}'.format
start = end = None
for s in segments:
if start != s.start_jd or end != s.end_jd:
start, end = s.start_jd, s.end_jd
starts = format_date(*calendar_date(int(start)))
ends = format_date(*calendar_date(int(end)))
lines.append(' JD {0:.2f} - JD {1:.2f} ({2} through {3})'
.format(start, end, starts, ends))
lines.append(_format_segment(s))
return '\n'.join(lines)
def close(self):
"""Close this ephemeris file."""
self.spk.close()
def comments(self):
"""Return the comments string of this kernel.
The resulting string often contains embedded newlines, and is
formatted for a human reader.
>>> print(planets.comments())
; de421.bsp LOG FILE
;
; Created 2008-02-12/11:33:34.00.
...
LEAPSECONDS_FILE = naif0007.tls
SPK_FILE = de421.bsp
...
"""
return self.spk.comments()
def names(self):
"""Return all target names that are valid with this kernel.
>>> pprint(planets.names())
{0: ['SOLAR_SYSTEM_BARYCENTER', 'SSB', 'SOLAR SYSTEM BARYCENTER'],
1: ['MERCURY_BARYCENTER', 'MERCURY BARYCENTER'],
2: ['VENUS_BARYCENTER', 'VENUS BARYCENTER'],
3: ['EARTH_BARYCENTER',
'EMB',
...
The result is a dictionary with target code keys and name lists
as values. The last name in each list is the one that Skyfield
uses when printing information about a body.
"""
d = defaultdict(list)
for code, name in target_name_pairs:
if code in self.codes:
d[code].append(name)
return dict(d)
def decode(self, name):
"""Translate a target name into its integer code.
>>> planets.decode('Venus')
299
Raises ``ValueError`` if you supply an unknown name, or
``KeyError`` if the target is missing from this kernel. You can
supply an integer code if you already have one and just want to
check whether it is present in this kernel.
"""
if isinstance(name, int):
code = name
else:
name = name.upper()
code = _jpl_name_code_dict.get(name)
if code is None:
raise ValueError('unknown SPICE target {0!r}'.format(name))
if code not in self.codes:
targets = ', '.join(_format_code_and_name(c) for c in self.codes)
raise KeyError('kernel {0!r} is missing {1!r} -'
' the targets it supports are: {2}'
.format(self.filename, name, targets))
return code
def __getitem__(self, target):
"""Return a vector function for computing the location of `target`."""
target = self.decode(target)
segments = self.segments
segment_dict = dict((segment.target, segment) for segment in segments)
chain = tuple(_center(target, segment_dict))
if len(chain) == 1:
return chain[0]
chain = chain[::-1]
center = chain[0].center
target = chain[-1].target
return VectorSum(center, target, chain, ())
def __contains__(self, name_or_code):
if isinstance(name_or_code, int):
code = name_or_code
else:
code = _jpl_name_code_dict.get(name_or_code.upper())
return code in self.codes
class SPICESegment(VectorFunction):
def __new__(cls, ephemeris, spk_segment):
if spk_segment.data_type == 2:
return object.__new__(ChebyshevPosition)
if spk_segment.data_type == 3:
return object.__new__(ChebyshevPositionVelocity)
raise ValueError('SPK data type {0} not yet supported'
.format(spk_segment.data_type))
def __init__(self, ephemeris, spk_segment):
self.ephemeris = ephemeris
self.center = spk_segment.center
self.target = spk_segment.target
self.spk_segment = spk_segment
def __str__(self):
return 'Segment {0!r} {1}'.format(
self.ephemeris.filename,
_format_segment_brief(self),
)
def __repr__(self):
return '<{0}>'.format(self)
class ChebyshevPosition(SPICESegment):
def _at(self, t):
segment = self.spk_segment
try:
position, velocity = segment.compute_and_differentiate(
t.whole, t.tdb_fraction)
except OutOfRangeError as e:
start_time = t.ts.tdb(jd=segment.start_jd)
end_time = t.ts.tdb(jd=segment.end_jd)
# TODO: switch to calendar dates in TDB to produce round numbers?
text = ('ephemeris segment only covers dates %s through %s UT'
% (start_time.utc_iso(' '), end_time.utc_iso(' ')))
mask = e.out_of_range_times
segment = self.spk_segment
e = EphemerisRangeError(text, start_time, end_time, mask, segment)
e.__cause__ = None # avoid exception chaining in Python 3
raise e
return position / AU_KM, velocity / AU_KM, None, None
class ChebyshevPositionVelocity(SPICESegment):
def _at(self, t):
pv = self.spk_segment.compute(t.whole, t.tdb_fraction)
return pv[:3] / AU_KM, pv[3:] * DAY_S / AU_KM, None, None
def _center(code, segment_dict):
"""Starting with `code`, follow segments from target to center."""
while code in segment_dict:
segment = segment_dict[code]
yield segment
code = segment.center
def _format_code_and_name(code):
name = _jpl_code_name_dict.get(code, None)
if name is None:
return str(code)
return '{0} {1}'.format(code, name)
def _format_segment(segment):
cname = _jpl_code_name_dict.get(segment.center, 'unknown')
tname = _jpl_code_name_dict.get(segment.target, 'unknown')
return ' {0:3} -> {1:<3} {2} -> {3}'.format(
segment.center, segment.target, cname, tname)
def _format_segment_brief(segment):
cname = _jpl_code_name_dict.get(segment.center)
tname = _jpl_code_name_dict.get(segment.target)
return '{0}{1}{2} -> {3}{4}{5}'.format(
segment.center,
' ' if cname else '',
cname,
segment.target,
' ' if tname else '',
tname,
)