Merge 4fbae33 into df2b6a2

CHANGELOG.md

@@ -2,7 +2,10 @@
 All notable changes to this project will be documented in this file.
 This project adheres to [Semantic Versioning](https://semver.org/).
 
-## [0.3.0] - XXXX-XX-XX
+## [0.3.0] - 2021-06-24
+* Add Keplerian orbital inputs into missions_sgp4
+* Update sgp4 interface to use new syntax for initialization from TLEs
+* Improve metadata generation in missions_sgp4
 * Documentation
   * Improve docstrings throughout
 * Testing

README.md

@@ -38,7 +38,7 @@ Python 3.7+.
 | numpy          | aacgmv2           |
 | pandas         | apexpy            |
 | pyEphem        | OMMBV             |
-| sgp4           | pysat>=3.0        |
+| sgp4>=2.7      | pysat>=3.0        |
 
 
 One way to install is through pip.  Just type

docs/installation.rst

@@ -23,7 +23,7 @@ Python 3.7+ and pysat 3.0.0+.
   numpy            aacgmv2
   pandas           apexpy
   pyEphem          OMMBV
-  sgp4             pysat>=3.0
+  sgp4>=2.7        pysat>=3.0
  ================ ==================
 
 

pysatMissions/instruments/__init__.py

@@ -1,5 +1,6 @@
 """Provides the instrument modules to be used with pysat."""
 
+from pysatMissions.instruments import methods  # noqa: F401
 from pysatMissions.instruments import missions_ephem
 from pysatMissions.instruments import missions_sgp4
 

pysatMissions/instruments/methods/__init__.py

@@ -0,0 +1,5 @@
+"""Methods to support multiple instrument files."""
+
+from pysatMissions.instruments.methods import orbits
+
+__all__ = ['orbits']

pysatMissions/instruments/methods/orbits.py

@@ -0,0 +1,138 @@
+"""Methods to convert orbital information for propagators."""
+
+import numpy as np
+import warnings
+
+
+def _check_orbital_params(kwargs=None):
+    """Check that a complete set of unconflicted orbital parameters exist.
+
+    Parameters
+    ----------
+    kwargs : dict
+        Dictionary of optional kwargs passed through upon initialization
+        of pysat instrument.
+
+    """
+
+    elements = list(kwargs['load'].keys())
+
+    keplerians = ['alt_periapsis', 'inclination']
+    tles = ['TLE1', 'TLE2']
+    errmsg = 'Insufficient kwargs.  Kwarg group requires {:}'
+    for group in [tles, keplerians]:
+        if any(v in elements for v in group):
+            if not all(v in elements for v in group):
+                raise KeyError(errmsg.format(', '.join(group)))
+    if all(v in elements for v in tles) and all(v in elements for v in keplerians):
+        warnings.warn(' '.join(['Cannot use both Keplerians and TLEs.',
+                                'Defaulting to Keplerians.']))
+
+    return
+
+
+def _get_constants(planet='Earth'):
+    """Retrieve planetary constants for calculations.
+
+    Parameters
+    ----------
+    planet : str
+        The name of the planet of interest.
+        (default='Earth')
+
+    Returns
+    -------
+    radius : float (km)
+        The average radius to the surface of a planet.
+    mass : float (kg)
+        The average mass of the planet.
+    gravity : float (m**3 kg / s**2)
+        Newton's gravitational constant
+    """
+
+    radius = {'Earth': 6371.2}
+    mass = {'Earth': 5.9742e24}
+    gravity = 6.6743e-11
+
+    if planet not in radius.keys():
+        raise KeyError('{:} is not yet a supported planet!'.format(planet))
+
+    return radius[planet], mass[planet], gravity
+
+
+def convert_to_keplerian(alt_periapsis, alt_apoapsis=None, planet='Earth'):
+    """Calculate orbital eccentricity from periapsis and apoapsis.
+
+    Parameters
+    ----------
+    alt_periapsis : float
+        The lowest altitude from the mean planet surface along the orbit (km)
+    alt_apoapsis : float or NoneType
+        The highest altitude from the mean planet surface along the orbit (km)
+        If None, assumed to be equal to periapsis. (default=None)
+    planet : str
+        The name of the planet of interest.  Used for radial calculations and
+        mass.
+        (default='Earth')
+
+    Returns
+    -------
+    eccentricity : float
+        The eccentricty of the orbit (unitless)
+    mean_motion : float
+        The mean angular speed of the orbit (rad/minute)
+
+    """
+
+    radius, mass, gravity = _get_constants(planet)
+    if alt_apoapsis is None:
+        alt_apoapsis = alt_periapsis
+
+    rad_apoapsis = alt_apoapsis + radius
+    rad_periapsis = alt_periapsis + radius
+    semimajor = 0.5 * (rad_apoapsis + rad_periapsis)
+
+    eccentricity = ((rad_apoapsis - rad_periapsis)
+                    / (rad_apoapsis + rad_periapsis))
+
+    # convert axis to m, mean_motion to rad / minute
+    mean_motion = np.sqrt(gravity * mass / (1000 * semimajor)**3) * 60
+
+    return eccentricity, mean_motion
+
+
+def convert_from_keplerian(eccentricity, mean_motion, planet='Earth'):
+    """Calculate orbital eccentricity from periapsis and apoapsis.
+
+    Parameters
+    ----------
+    eccentricity : float
+        The eccentricty of the orbit (unitless)
+    mean_motion : float
+        The mean angular speed of the orbit (rad/minute)
+    planet : string
+        The name of the planet of interest.  Used for radial calculations.
+        (default='Earth')
+
+    Returns
+    -------
+    alt_periapsis : float
+        The lowest altitude from the mean planet surface along the orbit (km)
+    alt_apoapsis : float
+        The highest altitude from the mean planet surface along the orbit (km)
+
+    """
+
+    radius, mass, gravity = _get_constants(planet)
+    # Convert mean_motion to rad / second before computing
+    semimajor = (gravity * mass / (mean_motion / 60)**2)
+    # Convert distance to km
+    semimajor = semimajor**(1 / 3) / 1000
+
+    rad_apoapsis = semimajor * (1 + eccentricity)
+    rad_periapsis = semimajor * (1 - eccentricity)
+
+    alt_apoapsis = rad_apoapsis - radius
+    alt_periapsis = rad_periapsis - radius
+
+    return alt_periapsis, alt_apoapsis