Merge pull request #71 from tudat-team/docs/reorganize-notebooks

Reorganize notebooks

README.md

@@ -27,6 +27,7 @@ Examples related to state estimation.
 
 Examples related to mission design.
 
+- ``mga_trajectories``: simulation of Multiple Gravity Assist (MGA) transfer trajectories using high- and low-thrust transfers, as well as deep space maneuvers (DSMs).
 - ``cassini1_mga_optimization``: using PyGMO to optimize an interplanetary transfer trajectory simulated using the multiple gravity assist (MGA) module of Tudat.
 - ``hodographic_shaping_mga_optimization``: extension of the ``cassini1_mga_optimization`` example. Optimization of a low-thrust interplanetary transfer trajectory using the hodographic shaping method for the low-thrust legs.
 - ``earth_mars_transfer_window``: usage of the Tudatpy's `porkchop` module to determine an optimal launch window (departure and arrival date) for an Earth-Mars transfer mission.
@@ -52,7 +53,6 @@ Advanced examples:
 - ``separation_satellites_diff_drag``: shows the effects of differential drag for CubeSats in LEO.
 - ``coupled_translational_rotational_dynamics``: using a multi-type propagator to simulate the coupled translational-rotational dynamics of Phobos around Mars.
 - ``impact_manifolds_lpo_cr3bp``: setup and propagation of orbits and their invariant manifolds in the circular restricted three body problem (CR3BP) with a polyhedral secondary body.
-- ``mga_trajectories``: simulation of Multiple Gravity Assist (MGA) transfer trajectories using high- and low-thrust transfers, as well as deep space maneuvers (DSMs).
 
 ### Pygmo
 

estimation/full_estimation_example.ipynb

@@ -647,7 +647,7 @@
    "id": "a77ce688-d439-4a37-94ee-ea9cd10b0d3d",
    "metadata": {},
    "source": [
-    "# True Errors, Formal Errors\n",
+    "## True Errors, Formal Errors\n",
     "\n",
     "Since we have now estimated the actual parameters - unlike when only getting the initial covariance matrix over the course of the orbit, as done in [Delfi-C3 Covariance Analysis example](https://docs.tudat.space/en/latest/_src_getting_started/_src_examples/notebooks/estimation/covariance_estimated_parameters.html) - we are able to qualitatively compare the goodness-of-fit of the found parameters with the known ground truth ones. \n",
     "\n",
@@ -881,13 +881,10 @@
   }
  ],
  "metadata": {
-  "interpreter": {
-   "hash": "4a4d53b53330cd83e1499268313a4bcd5eafe4bf50523883929af79f2dd687b2"
-  },
   "kernelspec": {
-   "display_name": "tudat-bundle",
+   "display_name": "tudat-examples",
    "language": "python",
-   "name": "tudat-bundle"
+   "name": "python3"
   },
   "language_info": {
    "codemirror_mode": {
@@ -899,7 +896,7 @@
    "name": "python",
    "nbconvert_exporter": "python",
    "pygments_lexer": "ipython3",
-   "version": "3.11.9"
+   "version": "3.10.14"
   }
  },
  "nbformat": 4,

propagation/linear_sensitivity_analysis.ipynb

@@ -5,7 +5,7 @@
    "id": "1fe978b0-d823-4f3e-b3e6-86a3e25cedbc",
    "metadata": {},
    "source": [
-    "# Linear sensitivity analysis of perturbed orbit\n",
+    "# Linear sensitivity analysis using variational equations\n",
     "\n",
     "## Objectives\n",
     "This example is an extension of the Perturbed Satellite Orbit Application. It adopts the simulation setup from the Perturbed Satellite Orbit, considering a slightly reduced set of perturbing accelerations for the propagation of the vehicle.\n",
@@ -14,7 +14,6 @@
     "\n",
     "Via the `estimation_setup.parameter module`, the system parameters w.r.t. which the sensitivity is to be studied are defined and a `create_variational_equations_solver` function from the numerical_simulation module is used in order to setup and integrate the system's variational equations. After obtaining the state transition matrices from the integrated variational equations, the system's response to small perturbations can be tested via simple matrix multiplication.\n",
     "\n",
-    "\n",
     "The availability of variational equations in tudat enables many more, advanced functionalities, such as covariance analysis and precise orbit determination."
    ]
   },
@@ -563,9 +562,9 @@
  ],
  "metadata": {
   "kernelspec": {
-   "display_name": "tudat-bundle",
+   "display_name": "tudat-examples",
    "language": "python",
-   "name": "tudat-bundle"
+   "name": "python3"
   },
   "language_info": {
    "codemirror_mode": {
@@ -577,7 +576,7 @@
    "name": "python",
    "nbconvert_exporter": "python",
    "pygments_lexer": "ipython3",
-   "version": "3.11.9"
+   "version": "3.10.14"
   }
  },
  "nbformat": 4,

propagation/reentry_trajectory.ipynb

@@ -5,7 +5,7 @@
    "id": "fe6987ee-7907-4b32-b8b4-30927d4e7970",
    "metadata": {},
    "source": [
-    "# Re-entry trajectory\n",
+    "# Re-entry trajectory using custom aerodynamic guidance\n",
     "\n",
     "## Objectives\n",
     "\n",
@@ -995,9 +995,9 @@
  ],
  "metadata": {
   "kernelspec": {
-   "display_name": "tudat-bundle",
+   "display_name": "tudat-examples",
    "language": "python",
-   "name": "tudat-bundle"
+   "name": "python3"
   },
   "language_info": {
    "codemirror_mode": {
@@ -1009,7 +1009,7 @@
    "name": "python",
    "nbconvert_exporter": "python",
    "pygments_lexer": "ipython3",
-   "version": "3.11.9"
+   "version": "3.10.14"
   }
  },
  "nbformat": 4,

propagation/solar_system_propagation.ipynb

@@ -5,7 +5,7 @@
    "id": "a22ea1d1-e56f-464d-a03e-02b2f0e27bfb",
    "metadata": {},
    "source": [
-    "# Solar System Propagation\n",
+    "# Solar System Propagation using Multi-Body Dynamics\n",
     "Copyright (c) 2010-2022, Delft University of Technology. All rights reserved. This file is part of the Tudat. Redistribution and use in source and binary forms, with or without modification, are permitted exclusively under the terms of the Modified BSD license. You should have received a copy of the license with this file. If not, please or visit: http://tudat.tudelft.nl/LICENSE.\n",
     "\n",
     "## Objectives\n",
@@ -470,7 +470,7 @@
  ],
  "metadata": {
   "kernelspec": {
-   "display_name": "Python 3 (ipykernel)",
+   "display_name": "tudat-examples",
    "language": "python",
    "name": "python3"
   },
@@ -484,7 +484,7 @@
    "name": "python",
    "nbconvert_exporter": "python",
    "pygments_lexer": "ipython3",
-   "version": "3.11.9"
+   "version": "3.10.14"
   }
  },
  "nbformat": 4,