REL: Bump versioning to RocketPy v1.3.0

.github/workflows/test_pytest.yaml

@@ -6,6 +6,8 @@ on:
     paths:
       - "**.py"
       - ".github/**"
+      - "pyproject.toml"
+      - "requirements*"
 
 defaults:
   run:
@@ -16,8 +18,11 @@ jobs:
     runs-on: ${{ matrix.os }}
     strategy:
       matrix:
-        os: [ubuntu-latest, macos-latest, windows-latest]
+        os: [ubuntu-latest, windows-latest]
         python-version: [3.8, 3.12]
+        include:
+          - os: macos-latest
+            python-version: 3.12
     env:
       OS: ${{ matrix.os }}
       PYTHON: ${{ matrix.python-version }}

.readthedocs.yaml

@@ -7,9 +7,9 @@ version: 2
 
 # Set the version of Python and other tools
 build:
-  os: ubuntu-20.04
+  os: ubuntu-22.04
   tools:
-    python: "3.9"
+    python: "3.12"
 
 # Build documentation in the docs/ directory with Sphinx
 sphinx:

CHANGELOG.md

@@ -25,20 +25,46 @@ and this project adheres to [Semantic Versioning](http://semver.org/).
 
 -->
 
-## [Unreleased] - yyyy-mm-dd
+## [1.3.0] - 2024-06-01
 
-<!-- These are the changes that were not release yet, please add them correctly.
-  Attention: The newest changes should be on top -->
+You can install this version by running `pip install rocketpy==1.3.0`
 
 ### Added
 
+- DOC: Adds prometheus data, Spaceport America 2022 [#601](https://github.com/RocketPy-Team/RocketPy/pull/601)
+- ENH: Pre-calculate attributes in Rocket class [#595](https://github.com/RocketPy-Team/RocketPy/pull/595)
+- ENH: Complex step differentiation [#594](https://github.com/RocketPy-Team/RocketPy/pull/594)
+- ENH: Exponential backoff decorator (fix #449) [#588](https://github.com/RocketPy-Team/RocketPy/pull/588)
+- ENH: Function Validation Rework & Swap `np.searchsorted` to `bisect_left` [#582](https://github.com/RocketPy-Team/RocketPy/pull/582)
+- 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
 
+- ENH: Adds StochasticModel.visualize_attributes() method [#612](https://github.com/RocketPy-Team/RocketPy/pull/612)
+- DOC: Monte carlo documentation updates [#607](https://github.com/RocketPy-Team/RocketPy/pull/607)
+- MNT: refactor u_dot parachute method [#596](https://github.com/RocketPy-Team/RocketPy/pull/596)
+- BLD: Change setup.py to pyproject.toml [#589](https://github.com/RocketPy-Team/RocketPy/pull/589)
+- DEP: delete deprecated rocketpy.tools.cached_property [#587](https://github.com/RocketPy-Team/RocketPy/pull/587)
+- ENH: Flight simulation speed up [#581] (https://github.com/RocketPy-Team/RocketPy/pull/581) 
+- MNT: Modularize Rocket Draw [#580](https://github.com/RocketPy-Team/RocketPy/pull/580)
+- DOC: Improvements of Environment docstring phrasing [#565](https://github.com/RocketPy-Team/RocketPy/pull/565)
+- 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
 
-## [v1.2.2] - 2024-03-09
+- DOC: Solve Dependencies Conflicts and pyproject build [#613](https://github.com/RocketPy-Team/RocketPy/pull/613)
+- BUG: Fixes nose cone bluffness issue #610 [#611](https://github.com/RocketPy-Team/RocketPy/pull/611)
+- BUG: plot drag curves when function source is callable [#599](https://github.com/RocketPy-Team/RocketPy/pull/599)
+- BUG: Fix minor type hinting problems [#598](https://github.com/RocketPy-Team/RocketPy/pull/598)
+- BUG: Optional Dependencies Naming in pyproject.toml. [#592](https://github.com/RocketPy-Team/RocketPy/pull/592)
+- BUG: Swap rocket.total_mass.differentiate for motor.total_mass_flow rate [#585](https://github.com/RocketPy-Team/RocketPy/pull/585)
+- 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`
 

data/motors/cesaroni/Cesaroni_7579M1520-P.eng

@@ -0,0 +1,13 @@
+; Pro98-3G 7579M1520-BS P
+M1520-BS 98 548 P 3.737 6.718 CTI
+   0.04 1427.795
+   0.082 1706.389
+   0.176 1620.489
+   0.748 1734.249
+   1.652 1827.113
+   2.676 1715.676
+   3.89 1423.152
+   4.399 1404.579
+   4.616 661.661
+   4.877 69.649
+   4.897 0.0

docs/conf.py

@@ -13,18 +13,19 @@
 import os
 import sys
 
-sys.path.insert(0, os.path.abspath("../"))
-
+package_path = os.path.abspath("../")
+sys.path.insert(0, package_path)
+os.environ["PYTHONPATH"] = ":".join((package_path, os.environ.get("PYTHONPATH", "")))
 
 # -- Project information -----------------------------------------------------
 
 project = "RocketPy"
-copyright = "2023, RocketPy Team"
+copyright = "2024, RocketPy Team"
 
 author = "RocketPy Team"
 
 # The full version, including alpha/beta/rc tags
-release = "1.2.2"
+release = "1.3.0"
 
 
 # -- General configuration ---------------------------------------------------

docs/examples/index.rst

@@ -16,4 +16,5 @@ If you want to see your rocket here, please contact the maintainers!
    valetudo_flight_sim.ipynb
    SEB_liquid_motor.ipynb
    juno3_flight_sim.ipynb
+   prometheus_2022_flight_sim.ipynb
 

docs/notebooks/dispersion_analysis/dispersion_analysis.ipynb → docs/notebooks/monte_carlo_analysis/monte_carlo_analysis.ipynb

@@ -20,6 +20,13 @@
     "We hope you enjoy the flight(s) in this notebook just like everyone in LASC19 did it in real-time!"
    ]
   },
+  {
+   "cell_type": "markdown",
+   "metadata": {},
+   "source": [
+    "**NOTE:** There is a new `MonteCarlo` class in RocketPy v1.2.0. This notebook is still here just for reference, but it is recommended to use the new class. See the `Monte Carlo class usage` page in the documentation for more information."
+   ]
+  },
   {
    "attachments": {},
    "cell_type": "markdown",
@@ -384,7 +391,7 @@
    ],
    "source": [
     "# Basic analysis info\n",
-    "filename = \"dispersion_analysis_outputs/valetudo_rocket_v0\"\n",
+    "filename = \"monte_carlo_analysis_outputs/valetudo_rocket_v0\"\n",
     "number_of_simulations = 100\n",
     "\n",
     "# Create data files for inputs, outputs and error logging\n",
@@ -404,7 +411,7 @@
     "Env.max_expected_height = 1500\n",
     "Env.set_atmospheric_model(\n",
     "    type=\"Ensemble\",\n",
-    "    file=\"dispersion_analysis_inputs/LASC2019_reanalysis.nc\",\n",
+    "    file=\"monte_carlo_analysis_inputs/LASC2019_reanalysis.nc\",\n",
     "    dictionary=\"ECMWF\",\n",
     ")\n",
     "\n",
@@ -428,7 +435,7 @@
     "\n",
     "    # Create motor\n",
     "    Keron = SolidMotor(\n",
-    "        thrust_source=\"dispersion_analysis_inputs/thrustCurve.csv\",\n",
+    "        thrust_source=\"monte_carlo_analysis_inputs/thrustCurve.csv\",\n",
     "        burn_time=5.274,\n",
     "        reshape_thrust_curve=(setting[\"burn_time\"], setting[\"impulse\"]),\n",
     "        nozzle_radius=setting[\"nozzle_radius\"],\n",
@@ -460,8 +467,8 @@
     "            setting[\"rocket_inertia_11\"],\n",
     "            setting[\"rocket_inertia_33\"],\n",
     "        ),\n",
-    "        power_off_drag=\"dispersion_analysis_inputs/Cd_PowerOff.csv\",\n",
-    "        power_on_drag=\"dispersion_analysis_inputs/Cd_PowerOn.csv\",\n",
+    "        power_off_drag=\"monte_carlo_analysis_inputs/Cd_PowerOff.csv\",\n",
+    "        power_on_drag=\"monte_carlo_analysis_inputs/Cd_PowerOn.csv\",\n",
     "        center_of_mass_without_motor=0,\n",
     "        coordinate_system_orientation=\"tail_to_nose\",\n",
     "    )\n",
@@ -574,7 +581,7 @@
     }
    ],
    "source": [
-    "filename = \"dispersion_analysis_outputs/valetudo_rocket_v0\"\n",
+    "filename = \"monte_carlo_analysis_outputs/valetudo_rocket_v0\"\n",
     "\n",
     "# Initialize variable to store all results\n",
     "dispersion_general_results = []\n",
@@ -20354,7 +20361,7 @@
     "from matplotlib.patches import Ellipse\n",
     "\n",
     "# Import background map\n",
-    "img = imread(\"dispersion_analysis_inputs/Valetudo_basemap_final.jpg\")\n",
+    "img = imread(\"monte_carlo_analysis_inputs/Valetudo_basemap_final.jpg\")\n",
     "\n",
     "# Retrieve dispersion data por apogee and impact XY position\n",
     "apogee_x = np.array(dispersion_results[\"apogee_x\"])\n",