pep8

Author: scivision

src/pymap3d/aer.py

@@ -165,7 +165,8 @@ def aer2geodetic(
 
 
 def eci2aer(
-    x: "ndarray", y: "ndarray", z: "ndarray", lat0: "ndarray", lon0: "ndarray", h0: "ndarray", t: datetime) -> typing.Tuple["ndarray", "ndarray", "ndarray"]:
+    x: "ndarray", y: "ndarray", z: "ndarray", lat0: "ndarray", lon0: "ndarray", h0: "ndarray", t: datetime
+) -> typing.Tuple["ndarray", "ndarray", "ndarray"]:
     """
     takes Earth Centered Inertial x,y,z ECI coordinates of point and gives az, el, slant range from Observer
 
@@ -213,7 +214,8 @@ def aer2eci(
     h0: "ndarray",
     t: datetime,
     ell=None,
-    deg: bool = True) -> typing.Tuple["ndarray", "ndarray", "ndarray"]:
+    deg: bool = True,
+) -> typing.Tuple["ndarray", "ndarray", "ndarray"]:
     """
     gives ECI of a point from an observer at az, el, slant range
 

tests/test_astropy.py

@@ -45,14 +45,14 @@ def test_anglesep_meeus():
 
 
 def test_eci_geodetic():
-    pytest.importorskip("numpy")
+    pytest.importorskip("astropy")
     t = "2013-01-15T12:00:05"
     lla = pm.eci2geodetic(*eci0, t)
-    assert lla == approx(lla0, rel=0.2)
+    assert lla == approx(lla0, rel=0.001)
 
 
 def test_eci_aer():
-    pytest.importorskip("numpy")
+    pytest.importorskip("astropy")
     t = "2013-01-15T12:00:05"
 
     aer1 = pm.eci2aer(*eci0, 42, -100, 0, t)

tests/test_eci.py

@@ -6,7 +6,7 @@
 
 def test_eci2ecef():
 
-    pytest.importorskip('astropy')
+    pytest.importorskip("astropy")
     # this example from Matlab eci2ecef docs
     eci = [-2981784, 5207055, 3161595]
     utc = datetime(2019, 1, 4, 12)
@@ -16,7 +16,7 @@ def test_eci2ecef():
 
 def test_ecef2eci():
 
-    pytest.importorskip('astropy')
+    pytest.importorskip("astropy")
     # this example from Matlab ecef2eci docs
     ecef = [-5762640, -1682738, 3156028]
     utc = datetime(2019, 1, 4, 12)