DOC: updated instrument headers

Updated the instrument headers with the NRL pub release.

pysatMissions/instruments/__init__.py

@@ -1,3 +1,9 @@
+# Full author list can be found in .zenodo.json file
+# DOI:10.5281/zenodo.3475498
+#
+# DISTRIBUTION STATEMENT A: Approved for public release. Distribution is
+# unlimited.
+# ----------------------------------------------------------------------------
 """Provides the instrument modules to be used with pysat."""
 
 from pysatMissions.instruments import methods  # noqa: F401

pysatMissions/instruments/_core.py

@@ -1,3 +1,9 @@
+# Full author list can be found in .zenodo.json file
+# DOI:10.5281/zenodo.3475498
+#
+# DISTRIBUTION STATEMENT A: Approved for public release. Distribution is
+# unlimited.
+# ----------------------------------------------------------------------------
 """Handles the default pysat functions for simulated instruments."""
 
 

pysatMissions/instruments/missions_ephem.py

@@ -1,4 +1,10 @@
 # -*- coding: utf-8 -*-
+# Full author list can be found in .zenodo.json file
+# DOI:10.5281/zenodo.3475498
+#
+# DISTRIBUTION STATEMENT A: Approved for public release. Distribution is
+# unlimited.
+# ----------------------------------------------------------------------------
 """Produce satellite orbit data.
 
 .. deprecated:: 0.3.0

pysatMissions/instruments/missions_sgp4.py

@@ -1,4 +1,10 @@
 # -*- coding: utf-8 -*-
+# Full author list can be found in .zenodo.json file
+# DOI:10.5281/zenodo.3475498
+#
+# DISTRIBUTION STATEMENT A: Approved for public release. Distribution is
+# unlimited.
+# ----------------------------------------------------------------------------
 """Simulate satellite orbit data using Two Line Elements (TLEs) and SGP4.
 
 Properties

pysatMissions/instruments/missions_skyfield.py

@@ -1,4 +1,10 @@
 # -*- coding: utf-8 -*-
+# Full author list can be found in .zenodo.json file
+# DOI:10.5281/zenodo.3475498
+#
+# DISTRIBUTION STATEMENT A: Approved for public release. Distribution is
+# unlimited.
+# ----------------------------------------------------------------------------
 """Simulate satellite orbit data using Two Line Elements (TLEs) and SGP4.
 
 Properties