DOC: run black

Author: LUCKIN13

docs/examples/camoes_flight_sim.ipynb

@@ -353,21 +353,27 @@
    "source": [
     "import numpy as np\n",
     "\n",
+    "\n",
     "def controller_function(\n",
     "    time, sampling_rate, state, state_history, observed_variables, air_brakes\n",
-    "):    \n",
-    "    new_deployment_level =0\n",
-    " \n",
-    "    if time<=11.4:\n",
-    "        new_deployment_level=1\n",
-    "    else: \n",
-    "        new_deployment_level=-0.002906*np.power(time,3) + 0.1497*np.power(time,2) + -2.563*time + 14.96\n",
-    "                \n",
-    "    if time>19.6:\n",
-    "         new_deployment_level=0\n",
-    "    \n",
-    "    if time<3.8: \n",
-    "        new_deployment_level=0\n",
+    "):\n",
+    "    new_deployment_level = 0\n",
+    "\n",
+    "    if time <= 11.4:\n",
+    "        new_deployment_level = 1\n",
+    "    else:\n",
+    "        new_deployment_level = (\n",
+    "            -0.002906 * np.power(time, 3)\n",
+    "            + 0.1497 * np.power(time, 2)\n",
+    "            + -2.563 * time\n",
+    "            + 14.96\n",
+    "        )\n",
+    "\n",
+    "    if time > 19.6:\n",
+    "        new_deployment_level = 0\n",
+    "\n",
+    "    if time < 3.8:\n",
+    "        new_deployment_level = 0\n",
     "\n",
     "    air_brakes.deployment_level = new_deployment_level\n",
     "\n",
@@ -519,7 +525,7 @@
     "    sampling_rate=10,\n",
     "    reference_area=None,\n",
     "    clamp=True,\n",
-    "    initial_observed_variables=(0,0),\n",
+    "    initial_observed_variables=(0, 0),\n",
     "    override_rocket_drag=True,\n",
     "    name=\"Air Brakes\",\n",
     ")"
@@ -635,7 +641,7 @@
    "source": [
     "import matplotlib.pyplot as plt\n",
     "\n",
-    "time_list, deployment_level_list= [], []\n",
+    "time_list, deployment_level_list = [], []\n",
     "\n",
     "obs_vars = test_flight.get_controller_observed_variables()\n",
     "\n",