Merge branch 'develop' into mnt/refactor-moment-of-inertia-conversions

CHANGELOG.md

@@ -32,17 +32,26 @@ and this project adheres to [Semantic Versioning](http://semver.org/).
 
 ### Added
 
+- ENH: Add new stability margin properties to Flight class [#572](https://github.com/RocketPy-Team/RocketPy/pull/572)
 - ENH: adds `Function.remove_outliers` method [#554](https://github.com/RocketPy-Team/RocketPy/pull/554)
 
 ### Changed
 
+- MNT: Refactor flight prints module [#579](https://github.com/RocketPy-Team/RocketPy/pull/579)
 - DOC: Convert CompareFlights example notebooks to .rst files [#576](https://github.com/RocketPy-Team/RocketPy/pull/576)
 - MNT: Refactor inertia calculations using parallel axis theorem [#573] (https://github.com/RocketPy-Team/RocketPy/pull/573)
 - ENH: Optional argument to show the plot in Function.compare_plots [#563](https://github.com/RocketPy-Team/RocketPy/pull/563)
 
 ### Fixed
+
 - BUG: export_eng 'Motor' method would not work for liquid motors. [#559](https://github.com/RocketPy-Team/RocketPy/pull/559) 
 
+## [v1.2.2] - 2024-03-22
+
+You can install this version by running `pip install rocketpy==1.2.2`
+
+- BUG: wrong rocket mass in parachute u dot method [#569](https://github.com/RocketPy-Team/RocketPy/pull/569)
+
 ## [v1.2.1] - 2024-02-22
 
 You can install this version by running `pip install rocketpy==1.2.1`

docs/conf.py

@@ -24,7 +24,7 @@
 author = "RocketPy Team"
 
 # The full version, including alpha/beta/rc tags
-release = "1.2.1"
+release = "1.2.2"
 
 
 # -- General configuration ---------------------------------------------------

docs/user/installation.rst

@@ -19,7 +19,7 @@ If you want to choose a specific version to guarantee compatibility, you may ins
 
 .. code-block:: shell
 
-    pip install rocketpy==1.2.1
+    pip install rocketpy==1.2.2
 
 
 Optional Installation Method: ``conda``