Source code for gdt.core.plot.earthplot

# CONTAINS TECHNICAL DATA/COMPUTER SOFTWARE DELIVERED TO THE U.S. GOVERNMENT WITH UNLIMITED RIGHTS
#
# Contract No.: CA 80MSFC17M0022
# Contractor Name: Universities Space Research Association
# Contractor Address: 7178 Columbia Gateway Drive, Columbia, MD 21046
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# Copyright 2017-2022 by Universities Space Research Association (USRA). All rights reserved.
#
# Developed by: William Cleveland and Adam Goldstein
#               Universities Space Research Association
#               Science and Technology Institute
#               https://sti.usra.edu
#
# Developed by: Daniel Kocevski
#               National Aeronautics and Space Administration (NASA)
#               Marshall Space Flight Center
#               Astrophysics Branch (ST-12)
#
# Licensed under the Apache License, Version 2.0 (the "License"); you may not use this file except
# in compliance with the License. You may obtain a copy of the License at
#
#    http://www.apache.org/licenses/LICENSE-2.0
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# Unless required by applicable law or agreed to in writing, software distributed under the License
# is distributed on an "AS IS" BASIS, WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or
# implied. See the License for the specific language governing permissions and limitations under the
# License.
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import numpy as np
import matplotlib.pyplot as plt
import matplotlib.ticker as mticker
import cartopy.crs as ccrs
from cartopy.mpl.gridliner import LONGITUDE_FORMATTER, LATITUDE_FORMATTER
    
from .plot import GdtPlot, SAA, EarthLine, EarthPoints
from .defaults import *
from gdt.core.geomagnetic import *
from gdt.core.time import time_range

__all__ = ['EarthPlot']

[docs]class EarthPlot(GdtPlot): """Class for plotting the Earth, primarily related to a spacecraft's position in orbit. Note: This class requires installation of Cartopy. Parameters: lat_range ((float, float), optional): The latitude range of the plot. Default value is (-90, 90) lon_range ((float, float), optional): The longitude range of the plot. Default value is (-180, 180). saa (:class:`~gdt.core.geomagnetic.SouthAtlanticAnomaly`, optional): If set, displays the SAA polygon. **kwargs: Options to pass to :class:`~gdt.core.plot.plot.GdtPlot` """ def __init__(self, lat_range=None, lon_range=None, saa=None, **kwargs): if lat_range is None: lat_range = (-90.0, 90.0) if lon_range is None: lon_range = (-180.0, 180.0) # scale figure size by lat and lon ranges xsize = (lon_range[1] - lon_range[0]) / 30.0 ysize = (lat_range[1] - lat_range[0]) / 30.0 figsize = (xsize, ysize) super().__init__(figsize=figsize, **kwargs) self._saa = None self._orbit = None self._sc = None self._ax.get_xaxis().set_visible(False) self._ax.get_yaxis().set_visible(False) self._ax.set_visible(False) # initialize the map, mercator projection proj = ccrs.PlateCarree() self._m = self.fig.add_axes([0.05, 0.1, 0.9, 0.80], projection=proj) self._m.set_xlim(lon_range) self._m.set_ylim(lat_range) self._m.coastlines() gl = self._m.gridlines(crs=proj, draw_labels=True, color='black') gl.xlocator = mticker.FixedLocator(np.arange(-180., 181., 30.)) gl.ylocator = mticker.FixedLocator(np.arange(-90., 91.0, 30.)) gl.xformatter = LONGITUDE_FORMATTER gl.yformatter = LATITUDE_FORMATTER gl.xlabel_style = {'size': PLOTFONTSIZE} gl.ylabel_style = {'size': PLOTFONTSIZE} gl.top_labels = False gl.right_labels = False if saa is not None: if not isinstance(saa, SouthAtlanticAnomaly): raise TypeError('saa must be of type SouthAtlanticAnomaly') self._saa = SAA(saa, proj, self._m, color='darkred', alpha=0.4) @property def geoaxes(self): """(cartopy.mpl.geoaxes.GeoAxesSubplot): The Cartopy axes""" return self._m @property def orbit(self): """(:class:`~gdt.core.plot.plot.EarthLine`): The orbital path""" return self._orbit @property def saa(self): """(:class:`~gdt.core.plot.plot.SAA`): The SAA polygon""" return self._saa @property def spacecraft(self): """(:class:`~gdt.core.plot.plot.EarthPoints`): A plot point representing the spacecraft position""" return self._sc
[docs] def add_spacecraft_frame(self, frame, tstart=None, tstop=None, step=1.0, trigtime=None, icon=None, **kwargs): """Add a SpacecraftFrame object to plot the orbital path and optionally the spacecraft position at a particular time. Args: frame (:class:`~gdt.core.coords.SpacecraftFrame`): The spacecraft frame containing position information tstart: (astropy.time.Time, optional): The start time to plot the orbit. If not set, then uses the first ``frame.obstime``. tstop: (astropy.time.Time, astropy.units.Quantity, or float, optional): Either a time value signifying the end of the range, the duration of the time range as a Quantity with appropriate unit, or an int/float representing the number of seconds. If not set, then uses the last ``frame.obstime``. step (datetime.TimeDelta, astropy.units.Quantity, or float, optional): Either a TimeDelta value, Quantity with appropriate unit, or an int/float representing the number of seconds. Default is 1.0 trigtime (astropy.time.Time): Set to a particular time of interest to plot the location. icon (:class:`~gdt.core.plot.plot.EarthPoints`): A subclass of EarthPoints that defines a specialized spacecraft icon. If not set, will default to standard matplotlib markers. **kwargs: Arguments to be passed to :class:`~gdt.core.plot.plot.EarthPoints` if ``icon`` is not set. """ if tstart is None: tstart = frame.obstime[0] if tstop is None: tstop = frame.obstime[-1] # get latitude and longitude over the time range and produce the orbit times = time_range(tstart, tstop, step) frame_interp = frame.at(times) lat = frame_interp.earth_location.lat.value lon = frame_interp.earth_location.lon.value self._orbit = EarthLine(lat, lon, self._m, color='black', alpha=0.4, lw=5.0) # if trigtime is set, produce spacecraft location if trigtime is not None: frame_interp = frame.at(trigtime) lat = frame_interp.earth_location.lat.value lon = frame_interp.earth_location.lon.value if icon is None: self._sc = EarthPoints(lat, lon, self._m, **kwargs) else: self._sc = icon(lat, lon, self._m, **kwargs)
[docs] def standard_title(self): """Add a standard plot title containing orbital position of the spacecraft. """ if self.spacecraft is not None: coord = self.spacecraft.coordinates title = 'Latitude, East Longitude: ({0}, {1})\n'.format(*coord) #mcl = '{:.2f}'.format(float(self._trig_mcilwain)) #title += 'McIlwain L: {}'.format(mcl) self._m.set_title(title)