def utc2obt(self, utc_string):
# Utc to Ephemeris time (seconds past J2000)
ephemeris_time = spiceypy.utc2et(utc_string)
# Ephemeris time to Obt
#return ephemeris_time
obt_string = spiceypy.sce2s(self.solar_orbiter_naif_id, ephemeris_time)
time_fields = re.search('\/(.*?):(\d*)', obt_string)
group = time_fields.groups()
try:
return int(group[0]) + int(group[1]) / 65536.
except Exception as e:
#logger.warning(str(e))
return 0
def utc2scs_spice(tais, sc):
res = {}
try:
scid = sp.bods2c(sc)
for tai in tais:
et = sp.unitim(tai, 'tai', 'et')
obt = sp.sce2s(scid, et)
utc = sp.et2utc(et, 'isoc', 3)
res[utc] = obt
except sp.stypes.SpiceyError as ex:
raise GeometrySpiceError(ex.value)
else:
return res
def utc_to_scet(self, utc):
"""
Convert UTC ISO format to SCET time strings.
Parameters
----------
utc : `str`
UTC time string in ISO format e.g. '2019-10-24T13:06:46.682758'
Returns
-------
`str`
SCET time string
"""
# Utc to Ephemeris time (seconds past J2000)
ephemeris_time = spiceypy.utc2et(utc)
# Ephemeris time to Obt
return spiceypy.sce2s(SOLAR_ORBITER_ID, ephemeris_time)
def datetime_to_scet(self, adatetime):
"""
Convert datetime to SCET.
Parameters
----------
adatetime : `datetime.datetime` or `astropy.time.Time`
Time to convert to SCET
Returns
-------
`str`
SCET of datetime encoded as spacecraft clock string
"""
if isinstance(adatetime, ApTime):
adatetime = adatetime.to_datetime()
et = spiceypy.datetime2et(adatetime)
scet = spiceypy.sce2s(SOLAR_ORBITER_ID, et)
return scet
def utc2scet(self, utc):
# Utc to Ephemeris time (seconds past J2000)
ephemeris_time = spiceypy.utc2et(utc)
# Ephemeris time to Obt
return spiceypy.sce2s(self.solar_orbiter_naif_id, ephemeris_time)
def toSCL(self, utc):
'''Convert UTC to Spacecraft clock time'''
if not self.loaded:
self.load()
return spice.sce2s(self.sc, spice.str2et(utc))
def utc2scet(self, utc):
# Utc to Ephemeris time (seconds past J2000)
ephemeris_time = spiceypy.utc2et(utc)
# Ephemeris time to Obt
return spiceypy.sce2s(-144, ephemeris_time)