def satpos(self):
"""Get actual satellite position in geodetic coordinates (WGS-84).
Evaluate orbit polynomials at the start time of the scan.
Returns: Longitude [deg east], Latitude [deg north] and Altitude [m]
"""
start_times_poly = get_cds_time(
days=self.nc['orbit_polynomial_start_time_day'].values,
msecs=self.nc['orbit_polynomial_start_time_msec'].values)
end_times_poly = get_cds_time(
days=self.nc['orbit_polynomial_end_time_day'].values,
msecs=self.nc['orbit_polynomial_end_time_msec'].values)
orbit_polynomials = {
'StartTime': np.array([start_times_poly]),
'EndTime': np.array([end_times_poly]),
'X': self.nc['orbit_polynomial_x'].values,
'Y': self.nc['orbit_polynomial_y'].values,
'Z': self.nc['orbit_polynomial_z'].values,
}
poly_finder = OrbitPolynomialFinder(orbit_polynomials)
orbit_polynomial = poly_finder.get_orbit_polynomial(self.start_time)
return get_satpos(
orbit_polynomial=orbit_polynomial,
time=self.start_time,
semi_major_axis=self.mda['projection_parameters']['a'],
semi_minor_axis=self.mda['projection_parameters']['b'],
)
def test_get_satpos(self, orbit_polynomial, time):
"""Test getting the position in geodetic coordinates."""
lon, lat, alt = get_satpos(orbit_polynomial=orbit_polynomial,
time=time,
semi_major_axis=6378169.00,
semi_minor_axis=6356583.80)
np.testing.assert_allclose(
[lon, lat, alt],
[-3.55117540817073, -0.5711243456528018, 35783296.150123544])
def satpos(self):
"""Get actual satellite position in geodetic coordinates (WGS-84).
Evaluate orbit polynomials at the start time of the scan.
Returns: Longitude [deg east], Latitude [deg north] and Altitude [m]
"""
poly_finder = OrbitPolynomialFinder(
self.header['15_DATA_HEADER']['SatelliteStatus']['Orbit']
['OrbitPolynomial'])
orbit_polynomial = poly_finder.get_orbit_polynomial(self.start_time)
return get_satpos(
orbit_polynomial=orbit_polynomial,
time=self.start_time,
semi_major_axis=self.mda['projection_parameters']['a'],
semi_minor_axis=self.mda['projection_parameters']['b'])
def satpos(self):
"""Get actual satellite position in geodetic coordinates (WGS-84).
Evaluate orbit polynomials at the start time of the scan.
Returns: Longitude [deg east], Latitude [deg north] and Altitude [m]
"""
a, b = self.get_earth_radii()
start_time = self.prologue['ImageAcquisition'][
'PlannedAcquisitionTime']['TrueRepeatCycleStart']
poly_finder = OrbitPolynomialFinder(
self.prologue['SatelliteStatus']['Orbit']['OrbitPolynomial'])
orbit_polynomial = poly_finder.get_orbit_polynomial(start_time)
return get_satpos(
orbit_polynomial=orbit_polynomial,
time=start_time,
semi_major_axis=a,
semi_minor_axis=b,
)