Merge remote-tracking branch 'origin/develop' into enh/parachute-inflation-modeling

Author: ArthurJWH

.github/workflows/linters.yml

@@ -16,7 +16,7 @@ jobs:
     runs-on: ubuntu-latest
     strategy:
       matrix:
-        python-version: ["3.9"]
+        python-version: ["3.10"]
     steps:
     - uses: actions/checkout@main
     - name: Set up Python ${{ matrix.python-version }}

.github/workflows/publish-to-pypi.yml

@@ -19,7 +19,7 @@ jobs:
       - name: Set up Python
         uses: actions/setup-python@main
         with:
-          python-version: "3.9"
+          python-version: "3.10"
       - name: Install dependencies
         run: |
           python -m pip install --upgrade pip

.github/workflows/test-pytest-slow.yaml

@@ -5,7 +5,7 @@ on:
     - cron: "0 17 * * 5"  # at 05:00 PM, only on Friday
   push:
     branches:
-      - main
+      - master
     paths:
       - "**.py"
       - ".github/**"
@@ -21,9 +21,10 @@ jobs:
     runs-on: ubuntu-latest
     strategy:
       matrix:
-        python-version: [3.9, 3.13]
+        python-version: ["3.10", "3.14"]
     env:
       PYTHON: ${{ matrix.python-version }}
+      MPLBACKEND: Agg
     steps:
       - uses: actions/checkout@main
       - name: Set up Python

.github/workflows/test_pytest.yaml

@@ -19,10 +19,11 @@ jobs:
     strategy:
       matrix:
         os: [ubuntu-latest, macos-latest, windows-latest]
-        python-version: [3.9, 3.13]
+        python-version: ["3.10", "3.14"]
     env:
       OS: ${{ matrix.os }}
       PYTHON: ${{ matrix.python-version }}
+      MPLBACKEND: Agg
     steps:
       - uses: actions/checkout@main
       - name: Set up Python

.pylintrc

@@ -88,7 +88,7 @@ persistent=yes
 
 # Minimum Python version to use for version dependent checks. Will default to
 # the version used to run pylint.
-py-version=3.9
+py-version=3.10
 
 # Discover python modules and packages in the file system subtree.
 recursive=no

CHANGELOG.md

@@ -32,20 +32,29 @@ Attention: The newest changes should be on top -->
 
 ### Added
 
-- EHN: Addition of ensemble variable to ECMWF dictionaries [#842] (https://github.com/RocketPy-Team/RocketPy/pull/842) 
+- ENH: Tank Fluids with Variable Density from Temperature and Pressure [#852](https://github.com/RocketPy-Team/RocketPy/pull/852)
+- ENH: Controller (AirBrakes) and Sensors Encoding [#849](https://github.com/RocketPy-Team/RocketPy/pull/849)
+- EHN: Addition of ensemble variable to ECMWF dictionaries [#842](https://github.com/RocketPy-Team/RocketPy/pull/842)
 - ENH: Added Crop and Clip Methods to Function Class [#817](https://github.com/RocketPy-Team/RocketPy/pull/817)
 - DOC: Add Flight class usage documentation and update index [#841](https://github.com/RocketPy-Team/RocketPy/pull/841)
-- ENH: Discretized and No-Pickle Encoding Options [#827] (https://github.com/RocketPy-Team/RocketPy/pull/827)
+- ENH: Discretized and No-Pickle Encoding Options [#827](https://github.com/RocketPy-Team/RocketPy/pull/827)
 - ENH: Add the Coriolis Force to the Flight class [#799](https://github.com/RocketPy-Team/RocketPy/pull/799)
 - ENH: Improve parachute geometric parametrization [#835](https://github.com/RocketPy-Team/RocketPy/pull/835)
+- ENH: Changing ellipses plot axis label [#855](https://github.com/RocketPy-Team/RocketPy/pull/855)
 
 ### Changed
 
+- MNT: allow for exporting of non apogee flights. [#863](https://github.com/RocketPy-Team/RocketPy/pull/863)
+- TST: remove remaining files after test session. [#862](https://github.com/RocketPy-Team/RocketPy/pull/862)
+- MNT: bumps min python version to 3.10 [#857](https://github.com/RocketPy-Team/RocketPy/pull/857)
+- DOC: Update docs dependencies and sub dependencies [#851](https://github.com/RocketPy-Team/RocketPy/pull/851)
+- MNT: extract flight data exporters [#845](https://github.com/RocketPy-Team/RocketPy/pull/845)
 - ENH: _MotorPrints inheritance - issue #460 [#828](https://github.com/RocketPy-Team/RocketPy/pull/828)
 - MNT: fix deprecations and warnings [#829](https://github.com/RocketPy-Team/RocketPy/pull/829)
 
 ### Fixed
 
+- BUG: correct encoding for trapezoidal sweep length and angle. [#861](https://github.com/RocketPy-Team/RocketPy/pull/861)
 - BUG: Fix no time initialization when passing initial_solution as array to Flight object [#844](https://github.com/RocketPy-Team/RocketPy/pull/844)
 
 

README.md

@@ -262,8 +262,8 @@ main = calisto.add_parachute(
     sampling_rate=105,
     lag=1.5,
     noise=(0, 8.3, 0.5),
-    parachute_radius=1.5,
-    parachute_height=1.5,
+    radius=1.5,
+    height=1.5,
     porosity=0.0432,
 )
 
@@ -274,8 +274,8 @@ drogue = calisto.add_parachute(
     sampling_rate=105,
     lag=1.5,
     noise=(0, 8.3, 0.5),
-    parachute_radius=1.5,
-    parachute_height=1.5,
+    radius=1.5,
+    height=1.5,
     porosity=0.0432,
 )
 ```

data/motors/liquid_motor_example/n2o_fluid_parameters.csv

@@ -0,0 +1,101 @@
+Temperature (K),Pressure (Pa),Density (kg/m³)
+193.150000,101325.000000,2.839688
+205.372222,101325.000000,2.659196
+217.594444,101325.000000,2.501930
+229.816667,101325.000000,2.363172
+242.038889,101325.000000,2.239591
+254.261111,101325.000000,2.128693
+266.483333,101325.000000,2.028539
+278.705556,101325.000000,1.937588
+290.927778,101325.000000,1.854594
+303.150000,101325.000000,1.778532
+193.150000,990733.333333,1206.532256
+205.372222,990733.333333,1168.931406
+217.594444,990733.333333,1129.335464
+229.816667,990733.333333,1087.042281
+242.038889,990733.333333,24.480299
+254.261111,990733.333333,22.807515
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+290.927778,990733.333333,19.178742
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+193.150000,5437775.000000,1213.241741
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docs/requirements.in

@@ -1,10 +1,10 @@
-nbsphinx==0.9.4
-pydata-sphinx-theme==0.15.2
+nbsphinx==0.9.7
+pydata-sphinx-theme==0.16.1
 jupyter-sphinx==0.5.3
-sphinx_design==0.5.0
-ipykernel==6.29.4
-pandas==2.2.2
-lxml_html_clean==0.1.1
+sphinx_design==0.6.1
+ipykernel==6.30.1
+pandas==2.3.2
+lxml_html_clean==0.4.2
 sphinx-copybutton==0.5.2
 sphinx-tabs==3.4.7
-plotly>=5
+plotly==6.3.0