RocketPy-Team · Gui-FernandesBR · Feb 13, 2025 · Jan 20, 2025 · Jan 20, 2025 · Feb 8, 2025
@@ -28,14 +28,11 @@ jobs:
         python -m pip install --upgrade pip
         pip install .[all]
         pip install .[tests]
-        pip install pylint isort black
-    - name: Run isort
-      run: isort --check-only rocketpy/ tests/ docs/ --profile black
-    - name: Run black
-      uses: psf/black@stable
-      with:
-        options: "--check rocketpy/ tests/ docs/"
-        jupyter: true
-    - name: Run pylint
+        pip install pylint ruff
+    - name: Ruff (lint)
+      run: ruff check --output-format=github .
+    - name: Ruff (format)
+      run: ruff format --check .
+    - name: Pylint
       run: |
-        pylint rocketpy/ tests/
+        pylint rocketpy/ tests/ docs/
@@ -51,6 +51,7 @@ coverage.xml
 .pytest_cache/
 cover/
 .pylint-report.txt
+.ruff-report.txt
 
 # Translations
 *.mo

@@ -46,7 +46,7 @@ fail-under=10
 #from-stdin=
 
 # Files or directories to be skipped. They should be base names, not paths.
-ignore=CVS, docs, data, 
+ignore=CVS, docs, data,
 
 # Add files or directories matching the regular expressions patterns to the
 # ignore-list. The regex matches against paths and can be in Posix or Windows
@@ -214,7 +214,7 @@ good-names=FlightPhases,
            HIRESW_dictionary,
            prop_I_11,
            Kt, # transformation matrix transposed
-           clalpha2D, 
+           clalpha2D,
            clalpha2D_incompressible,
            r_NOZ, # Nozzle position vector
            rocket_dry_I_33,
@@ -475,7 +475,7 @@ disable=raw-checker-failed,
         file-ignored,
         suppressed-message,
         useless-suppression,
-        deprecated-pragma, # because we have some peniding deprecations in the code. 
+        deprecated-pragma, # because we have some pending deprecations in the code.
         use-symbolic-message-instead,
         use-implicit-booleaness-not-comparison-to-string,
         use-implicit-booleaness-not-comparison-to-zero,
@@ -492,13 +492,14 @@ disable=raw-checker-failed,
         too-many-function-args, # gives false positives for Function calls
         method-hidden, # avoids some errors in tank_geometry and flight classes
         missing-timeout, # not a problem to use requests without timeout
-        protected-access, # we use private attriubutes out of the class (maybe we should fix this)
+        protected-access, # we use private attributes out of the class (maybe we should fix this)
         duplicate-code, # repeating code is a bad thing, but should we really care about it?
         line-too-long, # black already takes care of this
         missing-function-docstring, # this is too verbose.
         redefined-outer-name, # too verbose, and doesn't add much value
         method-cache-max-size-none,
         no-else-raise, # pointless
+        unnecessary-lambda-assignment, # ruff already checks this
 
 
 

@@ -51,6 +51,7 @@
         "bmatrix",
         "boldsymbol",
         "brentq",
+        "Bressan",
         "bysource",
         "Calebe",
         "calisto",
@@ -145,6 +146,7 @@
         "headlength",
         "headwidth",
         "hemis",
+        "Henrique",
         "hgtprs",
         "hgtsfc",
         "HIRESW",
@@ -188,6 +190,7 @@
         "LSODA",
         "lvhaack",
         "Mandioca",
+        "Marinho",
         "Marte",
         "Masatoshi",
         "Mateus",
@@ -239,7 +242,9 @@
         "prettytable",
         "Projeto",
         "prometheus",
+        "pycodestyle",
         "pydata",
+        "pydocstyle",
         "pylint",
         "pylintrc",
         "PYPI",
@@ -274,6 +279,7 @@
         "seblm",
         "seealso",
         "setrail",
+        "setuptools",
         "simplekml",
         "SIRGAS",
         "Sobol",

@@ -23,21 +23,17 @@ install:
 	pip install -r requirements-optional.txt
 	pip install -e .
 
-format: isort black
+format:
+	ruff check --select I --fix rocketpy/ tests/ docs/
+	ruff format rocketpy/ tests/ docs/
 
-isort:
-	isort --profile black rocketpy/ tests/ docs/
+lint: ruff-lint pylint
 
-black:
-	black rocketpy/ tests/ docs/
-
-lint: flake8 pylint
-
-flake8:
 	flake8 rocketpy/ tests/
+ruff-lint:
+	ruff check rocketpy/ tests/ docs/ --output-file=.ruff-report.txt
 
 pylint:
-	-pylint rocketpy/ tests/ --output=.pylint-report.txt
+	-pylint rocketpy/ tests/ docs/ --output=.pylint-report.txt
 
 build-docs:
 	cd docs && $(PYTHON) -m pip install -r requirements.txt && make html

@@ -37,15 +37,15 @@
    "outputs": [],
    "source": [
     "from rocketpy import (\n",
+    "    CylindricalTank,\n",
+    "    Environment,\n",
+    "    Flight,\n",
+    "    Fluid,\n",
     "    Function,\n",
     "    LiquidMotor,\n",
-    "    UllageBasedTank,\n",
     "    MassBasedTank,\n",
-    "    Fluid,\n",
     "    Rocket,\n",
-    "    Flight,\n",
-    "    Environment,\n",
-    "    CylindricalTank,\n",
+    "    UllageBasedTank,\n",
     ")"
    ]
   },

@@ -31,16 +31,14 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 3,
+   "execution_count": null,
    "metadata": {},
    "outputs": [],
    "source": [
-    "from rocketpy import Function, Environment, Flight, Rocket, SolidMotor\n",
-    "from rocketpy.motors import CylindricalTank, SolidMotor\n",
-    "from rocketpy.motors.tank import MassFlowRateBasedTank\n",
-    "\n",
     "import matplotlib.pyplot as plt\n",
     "\n",
+        "from rocketpy import Environment, Flight, Function, Rocket, SolidMotor\n",
+    "\n",
     "plt.style.use(\"seaborn-v0_8-colorblind\")"
    ]
   },
@@ -452,7 +450,6 @@
    "source": [
     "from rocketpy.simulation.flight_data_importer import FlightDataImporter\n",
     "\n",
-    "\n",
     "columns_map = {\n",
     "    \"t(s)\": \"time\",\n",
     "    \"alt(m)\": \"altitude\",\n",

@@ -42,17 +42,20 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 62,
+   "execution_count": null,
    "metadata": {},
    "outputs": [],
    "source": [
-    "from rocketpy import Function, Environment, Flight, Rocket, SolidMotor\n",
-    "from rocketpy import AirBrakes, _Controller\n",
-    "from rocketpy.motors import CylindricalTank, SolidMotor\n",
-    "from rocketpy.motors.tank import MassFlowRateBasedTank\n",
-    "\n",
     "import matplotlib.pyplot as plt\n",
     "\n",
+    "from rocketpy import (\n",
+    "    Environment,\n",
+    "    Flight,\n",
+    "    Function,\n",
+    "    Rocket,\n",
+    "    SolidMotor,\n",
+    ")\n",
+    "\n",
     "plt.style.use(\"seaborn-v0_8-colorblind\")"
    ]
   },
@@ -65,7 +68,7 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 63,
+   "execution_count": null,
    "metadata": {},
    "outputs": [
     {
@@ -813,7 +816,7 @@
  ],
  "metadata": {
   "kernelspec": {
-   "display_name": "RocketPy",
+   "display_name": ".venv",
    "language": "python",
    "name": "python3"
   },
@@ -827,7 +830,7 @@
    "name": "python",
    "nbconvert_exporter": "python",
    "pygments_lexer": "ipython3",
-   "version": "3.12.7"
+   "version": "3.13.1"
   }
  },
  "nbformat": 4,

@@ -37,11 +37,10 @@
    "metadata": {},
    "outputs": [],
    "source": [
-    "from rocketpy import Function, Environment, Flight, Rocket, SolidMotor\n",
-    "from rocketpy.motors import SolidMotor\n",
-    "\n",
     "import matplotlib.pyplot as plt\n",
     "\n",
+    "from rocketpy import Environment, Flight, Function, Rocket, SolidMotor\n",
+    "\n",
     "plt.style.use(\"seaborn-v0_8-colorblind\")"
    ]
   },
@@ -377,7 +376,6 @@
    "source": [
     "from rocketpy.simulation.flight_data_importer import FlightDataImporter\n",
     "\n",
-    "\n",
     "columns_map = {\n",
     "    \"ts\": \"time\",\n",
     "    \"altitude[m]\": \"altitude\",\n",
@@ -461,7 +459,7 @@
    "name": "python",
    "nbconvert_exporter": "python",
    "pygments_lexer": "ipython3",
-   "version": "3.10.11"
+   "version": "3.13.1"
   }
  },
  "nbformat": 4,

@@ -25,10 +25,11 @@
    "metadata": {},
    "outputs": [],
    "source": [
-    "from rocketpy import Function, Environment, Rocket, Flight\n",
+    "import datetime\n",
+    "\n",
+    "from rocketpy import Environment, Flight, Function, Rocket\n",
     "from rocketpy.motors import CylindricalTank, Fluid, HybridMotor\n",
-    "from rocketpy.motors.tank import MassFlowRateBasedTank\n",
-    "import datetime"
+    "from rocketpy.motors.tank import MassFlowRateBasedTank"
    ]
   },
   {
@@ -127,13 +128,13 @@
    "metadata": {},
    "outputs": [],
    "source": [
-    "oxidizer_liq = Fluid(name='N2O_l', density=960)\n",
-    "oxidizer_gas = Fluid(name='N2O_g', density=1.9277)\n",
+    "oxidizer_liq = Fluid(name=\"N2O_l\", density=960)\n",
+    "oxidizer_gas = Fluid(name=\"N2O_g\", density=1.9277)\n",
     "\n",
     "tank_shape = CylindricalTank(0.0665, 1.79)\n",
     "\n",
     "oxidizer_tank = MassFlowRateBasedTank(\n",
-    "    name='oxidizer_tank',\n",
+    "    name=\"oxidizer_tank\",\n",
     "    geometry=tank_shape,\n",
     "    flux_time=(6.5),\n",
     "    liquid=oxidizer_liq,\n",
@@ -146,15 +147,15 @@
     "    gas_mass_flow_rate_out=0,\n",
     ")\n",
     "\n",
-    "''' Defining the thrust curve'''\n",
+    "\"\"\" Defining the thrust curve\"\"\"\n",
     "\n",
     "\n",
     "def thrust_fuction(t):\n",
     "    return 5750 * 2 ** (-t / 200)\n",
     "\n",
     "\n",
     "hybrid_motor = HybridMotor(\n",
-    "    thrust_source='../../data/rockets/defiance/Thrust_curve.csv',\n",
+    "    thrust_source=\"../../data/rockets/defiance/Thrust_curve.csv\",\n",
     "    dry_mass=13.832,\n",
     "    dry_inertia=(1.801, 1.801, 0.0305),\n",
     "    center_of_dry_mass_position=780 / 1000,\n",
@@ -167,9 +168,9 @@
     "    grain_density=920,\n",
     "    nozzle_radius=0.0447,\n",
     "    throat_radius=0.0234,\n",
-    "    interpolation_method='linear',\n",
+    "    interpolation_method=\"linear\",\n",
     "    grains_center_of_mass_position=0.377,\n",
-    "    coordinate_system_orientation='nozzle_to_combustion_chamber',\n",
+    "    coordinate_system_orientation=\"nozzle_to_combustion_chamber\",\n",
     ")\n",
     "\n",
     "hybrid_motor.add_tank(tank=oxidizer_tank, position=2.2)"
@@ -205,9 +206,9 @@
     "    # inertia = (180.142, 180.142, 0.262),\n",
     "    inertia=(94.14, 94.14, 0.09),\n",
     "    center_of_mass_without_motor=3.29,\n",
-    "    power_off_drag='../../data/rockets/defiance/DragCurve.csv',\n",
-    "    power_on_drag='../../data/rockets/defiance/DragCurve.csv',\n",
-    "    coordinate_system_orientation='tail_to_nose',\n",
+    "    power_off_drag=\"../../data/rockets/defiance/DragCurve.csv\",\n",
+    "    power_on_drag=\"../../data/rockets/defiance/DragCurve.csv\",\n",
+    "    coordinate_system_orientation=\"tail_to_nose\",\n",
     ")\n",
     "\n",
     "defiance.add_motor(hybrid_motor, position=0.2)\n",
@@ -220,10 +221,10 @@
     "\n",
     "defiance.add_tail(top_radius=0.07, bottom_radius=0.064, length=0.0597, position=0.1)\n",
     "\n",
-    "defiance.add_parachute(name='main', cd_s=2.2, trigger=305, sampling_rate=100, lag=0)\n",
+    "defiance.add_parachute(name=\"main\", cd_s=2.2, trigger=305, sampling_rate=100, lag=0)\n",
     "\n",
     "defiance.add_parachute(\n",
-    "    name='drogue', cd_s=1.55, trigger='apogee', sampling_rate=100, lag=0\n",
+    "    name=\"drogue\", cd_s=1.55, trigger=\"apogee\", sampling_rate=100, lag=0\n",
     ")"
    ]
   },

@@ -31,16 +31,14 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 3,
+   "execution_count": null,
    "metadata": {},
    "outputs": [],
    "source": [
-    "from rocketpy import Function, Environment, Flight, Rocket, SolidMotor\n",
-    "from rocketpy.motors import CylindricalTank, SolidMotor\n",
-    "from rocketpy.motors.tank import MassFlowRateBasedTank\n",
-    "\n",
     "import matplotlib.pyplot as plt\n",
     "\n",
+    "from rocketpy import Environment, Flight, Function, Rocket, SolidMotor\n",
+    "\n",
     "plt.style.use(\"seaborn-v0_8-colorblind\")"
    ]
   },
@@ -384,7 +382,6 @@
    "source": [
     "from rocketpy.simulation.flight_data_importer import FlightDataImporter\n",
     "\n",
-    "\n",
     "columns_map = {\n",
     "    \"t\": \"time\",\n",
     "    \"alt\": \"altitude\",\n",