Minor corrections

estimation/covariance_estimated_parameters.py

@@ -28,11 +28,6 @@
 import numpy as np
 from matplotlib import pyplot as plt
 
-# Use custom compiled Tudat version
-import sys
-sys.path.insert(0, '/mnt/e/studio/professional/work/2023-2024 Tudat/repos/tudat-bundle/cmake-build-release-wsl/tudatpy/')
-
-
 # Load required tudatpy modules
 from tudatpy import constants
 from tudatpy.interface import spice

mission_design/earth_mars_transfer_window.ipynb

@@ -57,14 +57,6 @@
    "metadata": {},
    "outputs": [],
    "source": [
-    "# General imports\n",
-    "import os\n",
-    "import pickle\n",
-    "\n",
-    "# Use custom compiled Tudat version\n",
-    "import sys\n",
-    "sys.path.insert(0, '/mnt/e/studio/professional/work/2023-2024 Tudat/repos/tudat-bundle/cmake-build-release-wsl/tudatpy/')\n",
-    "\n",
     "# Tudat imports\n",
     "from tudatpy import constants\n",
     "from tudatpy.interface import spice_interface\n",
@@ -164,7 +156,8 @@
     "- The optimal departure-arrival date combination\n",
     "- The constant time-of-flight isochrones\n",
     "- And more"
-   ]
+   ],
+   "id": "99e7d88a0da10251"
   },
   {
    "cell_type": "code",
@@ -174,7 +167,6 @@
    "source": [
     "[departure_epochs, arrival_epochs, ΔV] = porkchop(\n",
     "    bodies,\n",
-    "    global_frame_orientation,\n",
     "    departure_body,\n",
     "    target_body,\n",
     "    earliest_departure_time,\n",
@@ -183,7 +175,8 @@
     "    latest_arrival_time,\n",
     "    time_resolution\n",
     ")"
-   ]
+   ],
+   "id": "f4d4f5b5ec813dcb"
   },
   {
    "cell_type": "markdown",
@@ -196,7 +189,8 @@
     "- Plot $\\Delta V$ (default) or C3 (specific energy), as well as choose whether to plot departure and arrival $\\Delta V$ together as the total $\\Delta V$ required for the transfer (default), or separately (in those cases in which the manoeuvre is performed in two burns, one at departure and one at arrival to the target planet).\n",
     "\n",
     "Let's make use of `plot_porkchop` to see all four combinations!"
-   ]
+   ],
+   "id": "abcd0ea6ba872500"
   },
   {
    "cell_type": "code",
@@ -221,7 +215,8 @@
     "        save             = True,\n",
     "        **case\n",
     "    )"
-   ]
+   ],
+   "id": "1c4f5e8a3da1c180"
   }
  ],
  "metadata": {

mission_design/earth_mars_transfer_window.py

@@ -124,7 +124,6 @@
 
     [departure_epochs, arrival_epochs, ΔV] = porkchop(
         bodies,
-        global_frame_orientation,
         departure_body,
         target_body,
         earliest_departure_time,