STY: applies black.

- I did this changes by running `make format` at the root directory

Author: Gui-FernandesBR

docs/examples/halcyon_flight_sim.ipynb

@@ -44,11 +44,12 @@
    "metadata": {},
    "outputs": [],
    "source": [
-    "from rocketpy import Function,Environment, Flight, Rocket\n",
+    "from rocketpy import Function, Environment, Flight, Rocket\n",
     "from rocketpy.motors import CylindricalTank, Fluid, HybridMotor\n",
     "from rocketpy.motors.tank import MassFlowRateBasedTank\n",
-    "import datetime \n",
+    "import datetime\n",
     "import matplotlib.pyplot as plt\n",
+    "\n",
     "plt.style.use(\"seaborn-v0_8-colorblind\")"
    ]
   },
@@ -67,7 +68,7 @@
     }
    ],
    "source": [
-    "tomorrow = datetime.date(2023,10,13) + datetime.timedelta(days=1)\n",
+    "tomorrow = datetime.date(2023, 10, 13) + datetime.timedelta(days=1)\n",
     "\n",
     "Env = Environment(\n",
     "    latitude=39.388692,\n",
@@ -246,7 +247,7 @@
    "source": [
     "env = Environment(\n",
     "    gravity=9.80665,\n",
-    "    date=(2023,10,13,14),\n",
+    "    date=(2023, 10, 13, 14),\n",
     "    latitude=39.388692,\n",
     "    longitude=-8.287814,\n",
     "    elevation=120,\n",
@@ -264,7 +265,7 @@
     "    dictionary=\"ECMWF\",\n",
     ")\n",
     "env.max_expected_height = 4000\n",
-    "env.info()\n"
+    "env.info()"
    ]
   },
   {
@@ -301,7 +302,7 @@
     "\n",
     "hybrid_motor = HybridMotor(\n",
     "    thrust_source=\"../../data/astg/engine_Halcyon_4thHotfire.eng\",\n",
-    "    dry_mass=10670/ 1000,\n",
+    "    dry_mass=10670 / 1000,\n",
     "    dry_inertia=(1.668, 1.668, 0.026),\n",
     "    center_of_dry_mass_position=780 / 1000,\n",
     "    burn_time=5,\n",
@@ -319,7 +320,7 @@
     "    coordinate_system_orientation=\"nozzle_to_combustion_chamber\",\n",
     ")\n",
     "\n",
-    "hybrid_motor.add_tank(tank=oxidizer_tank, position=934.75/ 1000)\n"
+    "hybrid_motor.add_tank(tank=oxidizer_tank, position=934.75 / 1000)"
    ]
   },
   {
@@ -408,11 +409,7 @@
    "metadata": {},
    "outputs": [],
    "source": [
-    "NoseCone = HALCYON.add_nose(\n",
-    "    length=0.46, \n",
-    "    kind=\"vonKarman\", \n",
-    "    position=3556 / 1000\n",
-    ")\n",
+    "NoseCone = HALCYON.add_nose(length=0.46, kind=\"vonKarman\", position=3556 / 1000)\n",
     "\n",
     "FinSet = HALCYON.add_trapezoidal_fins(\n",
     "    n=4,\n",
@@ -440,7 +437,7 @@
     "    sampling_rate=100,\n",
     "    lag=5,\n",
     "    noise=(0, 8.3, 0.5),\n",
-    ")\n"
+    ")"
    ]
   },
   {
@@ -457,11 +454,7 @@
    "outputs": [],
    "source": [
     "test_flight = Flight(\n",
-    "    rocket=HALCYON, \n",
-    "    environment=env, \n",
-    "    inclination=85, \n",
-    "    heading=90, \n",
-    "    rail_length=12\n",
+    "    rocket=HALCYON, environment=env, inclination=85, heading=90, rail_length=12\n",
     ")"
    ]
   },
@@ -528,8 +521,8 @@
     "\n",
     "columns_map = {\n",
     "    \"ts\": \"time\",\n",
-    "    \"filtered_altitude_AGL\":\"altitude\" ,\n",
-    "    \"filtered_acceleration\":\"az\" ,\n",
+    "    \"filtered_altitude_AGL\": \"altitude\",\n",
+    "    \"filtered_acceleration\": \"az\",\n",
     "}\n",
     "\n",
     "cots_altimeter_flight = FlightDataImporter(\n",