update pyoorb class names

README.md

@@ -156,12 +156,13 @@ You will need to install either adam_core[pyoorb] or adam_core[assist], or anoth
 
 #### Propagation
 To propagate orbits with PYOORB (here we grab some orbits from Horizons first):
+
 ```python
 import numpy as np
 from astropy import units as u
 
 from adam_core.orbits.query import query_horizons
-from adam_core.propagator import PYOORB
+from adam_core.propagator import PYOORBPropagator
 from adam_core.time import Timestamp
 
 # Get orbits to propagate
@@ -170,7 +171,7 @@ object_ids = ["Duende", "Eros", "Ceres"]
 orbits = query_horizons(object_ids, initial_time)
 
 # Make sure PYOORB is ready
-propagator = PYOORB()
+propagator = PYOORBPropagator()
 
 # Define propagation times
 times = initial_time.from_mjd(initial_time.mjd() + np.arange(0, 100))
@@ -186,14 +187,21 @@ propagated_orbits = propagator.propagate_orbits(
 ```
 
 #### Ephemeris Generation
-The propagator class can also be used to generate ephemerides for a set of orbits and observers.
+Ephemeris generation requires a propagator that implements the EphemerisMixin interface. This is currently only implemented by the PYOORB propagator. The ephemeris generator will automatically map the propagated covariance matrices to the sky-plane.
+
+You will need to install adam-pyoorb in order to use the ephemeris generator.
+
+```sh
+pip install adam-core[pyoorb]
+```
+
 
 ```python
 import numpy as np
 from astropy import units as u
 
 from adam_core.orbits.query import query_horizons
-from adam_core.propagator import PYOORB
+from adam_core.propagator import PYOORBPropagator
 from adam_core.observers import Observers
 from adam_core.time import Timestamp
 
@@ -203,7 +211,7 @@ object_ids = ["Duende", "Eros", "Ceres"]
 orbits = query_horizons(object_ids, initial_time)
 
 # Make sure PYOORB is ready
-propagator = PYOORB()
+propagator = PYOORBPropagator()
 
 # Define a set of observers and observation times
 times = Timestamp.from_mjd(initial_time.mjd() + np.arange(0, 100))
@@ -278,7 +286,7 @@ import numpy as np
 from astropy import units as u
 
 from adam_core.orbits.query import query_sbdb
-from adam_core.propagator import PYOORB
+from adam_core.propagator import PYOORBPropagator
 from adam_core.observers import Observers
 from adam_core.dynamics import generate_ephemeris_2body
 from adam_core.time import Timestamp
@@ -288,7 +296,7 @@ object_ids = ["Duende", "Eros", "Ceres"]
 orbits = query_sbdb(object_ids)
 
 # Make sure PYOORB is ready
-propagator = PYOORB()
+propagator = PYOORBPropagator()
 
 # Define a set of observers and observation times
 times = Timestamp.from_mjd(np.arange(59000, 60000), scale="tdb")

src/adam_core/orbit_determination/tests/test_differential_correction.py

@@ -2,7 +2,7 @@
 
 import pytest
 
-from adam_core.propagator.adam_pyoorb import PYOORB
+from adam_core.propagator.adam_pyoorb import PYOORBPropagator
 
 from ..differential_correction import fit_least_squares
 
@@ -15,7 +15,7 @@ def test_fit_least_squares_pure_iod_orbit(pure_iod_orbit):
     # process using least squares
 
     orbit, orbit_members, observations = pure_iod_orbit
-    propagator = PYOORB()
+    propagator = PYOORBPropagator()
 
     fitted_orbit, fitted_orbit_members = fit_least_squares(
         orbit, observations, propagator

src/adam_core/orbit_determination/tests/test_evaluate.py

@@ -5,7 +5,7 @@
 import pytest
 import quivr as qv
 
-from adam_core.propagator.adam_pyoorb import PYOORB
+from adam_core.propagator.adam_pyoorb import PYOORBPropagator
 
 from ..evaluate import evaluate_orbits
 
@@ -17,7 +17,7 @@ def test_evaluate_orbits(pure_iod_orbit):
     # Test that evaluate_orbit correctly calculates residuals and other
     # parameters for an input orbit
     orbit, orbit_members, observations = pure_iod_orbit
-    propagator = PYOORB()
+    propagator = PYOORBPropagator()
 
     # Concatenate the orbit three times to test we can handle multiple orbits
     orbits = qv.concatenate([orbit, orbit, orbit])
@@ -64,7 +64,7 @@ def test_evaluate_orbits_outliers(pure_iod_orbit):
     # Test that evaluate_orbit correctly calculates residuals and other
     # parameters for an input orbit with outliers defined
     orbit, orbit_members, observations = pure_iod_orbit
-    propagator = PYOORB()
+    propagator = PYOORBPropagator()
 
     # Lets remove the last two observations
     outliers = observations.id.tolist()[-2:]

src/adam_core/propagator/__init__.py

@@ -7,5 +7,4 @@
     "EphemerisMixin",
     "OrbitType",
     "EphemerisType",
-    "PYOORB",
 ]