beta release, v1.0.0

cyschneck · Nov 27, 2022 · b08e9f5 · b08e9f5
1 parent a0746ce
commit b08e9f5
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Showing 3 changed files with 13 additions and 5 deletions.
diff --git a/generate_examples_eot_charts.py b/generate_examples_eot_charts.py
@@ -14,7 +14,7 @@
 					["Neptune", 0.0086, 29.56, 30.0611]]
 
 	for planet in planet_lst:
-		if True:#planet[0] == "Earth":
+		if planet[0] == "Earth":
 			orbital_period_planet = muller_eot.calculateOrbitalPeriod(planet[3])
 
 			# Effect of Eccentricity

diff --git a/muller_eot/calculate_eot.py b/muller_eot/calculate_eot.py
@@ -30,7 +30,9 @@ def calculateDifferenceEOTMinutes(eccentricity=None,
 								orbit_period=None):
 	# Calculate the time difference (in minutes) for the Equation of Time
 
-	muller_eot.errorHandlingEOT(eccentricity, obliquity_deg, orbit_period)
+	muller_eot.errorHandlingEOT(eccentricity,
+								obliquity_deg,
+								orbit_period) # Verify argument behavior
 
 	distance_between_solistice_perhelion_deg = muller_eot.calculateDistanceBetweenSolisticePerhelion()
 	distance_between_solistice_perhelion_rad = np.deg2rad(distance_between_solistice_perhelion_deg)
@@ -95,7 +97,13 @@ def plotEOT(planet_name=None,
 			save_plot_name=None):
 	# Plot EOT Time Differences
 
-	muller_eot.errorHandlingPlotEOT(planet_name, orbital_period, eot_y, effect_title_str, figsize_n, figsize_dpi, save_plot_name)
+	muller_eot.errorHandlingPlotEOT(planet_name,
+									orbital_period,
+									eot_y,
+									effect_title_str,
+									figsize_n,
+									figsize_dpi,
+									save_plot_name) # Verify argument behavior
 
 	fig = plt.figure(figsize=(figsize_n,figsize_n), dpi=figsize_dpi)
 

diff --git a/setup.py b/setup.py
@@ -3,7 +3,7 @@
 # Python Package Setup
 from setuptools import setup, find_namespace_packages
 
-VERSION="0.0.4"
+VERSION="1.0.0"
 DESCRIPTION="A Python package for M. Müller implementation of the 'Equation of Time - Problem in Astronomy' to calculate EOT and the effect of eccentricity/obliquity"
 
 with open("README.md", "r") as f:
@@ -21,7 +21,7 @@
 	keywords=["astronomy", "python", "eot", "equation of time", "eccentricity", "obliquity"],
 	license="MIT",
 	classifiers=[
-		"Development Status :: 1 - Planning",
+		"Development Status :: 4 - Beta",
 		"Intended Audience :: Developers",
 		"Intended Audience :: Education",
 		"Intended Audience :: Science/Research",