Refactoring complete

estimation/covariance_estimated_parameters.ipynb

@@ -43,9 +43,9 @@
     "from matplotlib import pyplot as plt\n",
     "\n",
     "# Load required tudatpy modules\n",
-    "from tudatpy.kernel import constants\n",
+    "from tudatpy import constants\n",
     "from tudatpy.interface import spice\n",
-    "from tudatpy.kernel import numerical_simulation\n",
+    "from tudatpy import numerical_simulation\n",
     "from tudatpy.numerical_simulation import environment_setup\n",
     "from tudatpy.numerical_simulation import propagation_setup\n",
     "from tudatpy.numerical_simulation import estimation, estimation_setup\n",

estimation/covariance_estimated_parameters.py

@@ -29,9 +29,9 @@
 from matplotlib import pyplot as plt
 
 # Load required tudatpy modules
-from tudatpy.kernel import constants
+from tudatpy import constants
 from tudatpy.interface import spice
-from tudatpy.kernel import numerical_simulation
+from tudatpy import numerical_simulation
 from tudatpy.numerical_simulation import environment_setup
 from tudatpy.numerical_simulation import propagation_setup
 from tudatpy.numerical_simulation import estimation, estimation_setup

estimation/estimation_dynamical_models.py

@@ -28,9 +28,9 @@
 from mpl_toolkits.mplot3d import axes3d
 
 # Load required tudatpy modules
-from tudatpy.kernel import constants
+from tudatpy import constants
 from tudatpy.interface import spice
-from tudatpy.kernel import numerical_simulation
+from tudatpy import numerical_simulation
 from tudatpy.numerical_simulation import environment_setup
 from tudatpy.numerical_simulation import propagation_setup
 from tudatpy.numerical_simulation import estimation, estimation_setup

estimation/full_estimation_example.ipynb

@@ -45,9 +45,9 @@
     "from matplotlib import pyplot as plt\n",
     "\n",
     "# Load required tudatpy modules\n",
-    "from tudatpy.kernel import constants\n",
+    "from tudatpy import constants\n",
     "from tudatpy.interface import spice\n",
-    "from tudatpy.kernel import numerical_simulation\n",
+    "from tudatpy import numerical_simulation\n",
     "from tudatpy.numerical_simulation import environment_setup\n",
     "from tudatpy.numerical_simulation import propagation_setup\n",
     "from tudatpy.numerical_simulation import estimation, estimation_setup\n",

estimation/full_estimation_example.py

@@ -29,9 +29,9 @@
 from matplotlib import pyplot as plt
 
 # Load required tudatpy modules
-from tudatpy.kernel import constants
+from tudatpy import constants
 from tudatpy.interface import spice
-from tudatpy.kernel import numerical_simulation
+from tudatpy import numerical_simulation
 from tudatpy.numerical_simulation import environment_setup
 from tudatpy.numerical_simulation import propagation_setup
 from tudatpy.numerical_simulation import estimation, estimation_setup

estimation/galilean_moons_state_estimation.ipynb

@@ -37,9 +37,9 @@
     "\n",
     "# tudatpy imports\n",
     "from tudatpy import util\n",
-    "from tudatpy.kernel import constants\n",
+    "from tudatpy import constants\n",
     "from tudatpy.interface import spice\n",
-    "from tudatpy.kernel import numerical_simulation\n",
+    "from tudatpy import numerical_simulation\n",
     "from tudatpy.astro import time_conversion, element_conversion\n",
     "from tudatpy.numerical_simulation import environment_setup\n",
     "from tudatpy.numerical_simulation import propagation_setup\n",

estimation/galilean_moons_state_estimation.py

@@ -26,9 +26,9 @@
 
 # tudatpy imports
 from tudatpy import util
-from tudatpy.kernel import constants
+from tudatpy import constants
 from tudatpy.interface import spice
-from tudatpy.kernel import numerical_simulation
+from tudatpy import numerical_simulation
 from tudatpy.astro import time_conversion, element_conversion
 from tudatpy.numerical_simulation import environment_setup
 from tudatpy.numerical_simulation import propagation_setup

propagation/coupled_translational_rotational_dynamics.ipynb

@@ -90,7 +90,7 @@
     "from numpy.polynomial.polynomial import polyfit\n",
     "from tudatpy.util import result2array\n",
     "from tudatpy.interface import spice\n",
-    "from tudatpy.kernel import constants, numerical_simulation\n",
+    "from tudatpy import constants, numerical_simulation\n",
     "from tudatpy.numerical_simulation import environment_setup, propagation_setup\n",
     "from tudatpy.astro.element_conversion import rotation_matrix_to_quaternion_entries\n",
     "from tudatpy.astro.frame_conversion import inertial_to_rsw_rotation_matrix\n",

propagation/coupled_translational_rotational_dynamics.py

@@ -71,7 +71,7 @@
 from numpy.polynomial.polynomial import polyfit
 from tudatpy.util import result2array
 from tudatpy.interface import spice
-from tudatpy.kernel import constants, numerical_simulation
+from tudatpy import constants, numerical_simulation
 from tudatpy.numerical_simulation import environment_setup, propagation_setup
 from tudatpy.astro.element_conversion import rotation_matrix_to_quaternion_entries
 from tudatpy.astro.frame_conversion import inertial_to_rsw_rotation_matrix

propagation/impact_manifolds_lpo_cr3bp.ipynb

@@ -51,7 +51,7 @@
     "# Tudatpy imports\n",
     "import tudatpy\n",
     "from tudatpy.util import result2array\n",
-    "from tudatpy.kernel import numerical_simulation\n",
+    "from tudatpy import numerical_simulation\n",
     "from tudatpy.numerical_simulation import propagation_setup, environment_setup, estimation_setup\n",
     "from tudatpy.astro import polyhedron_utilities\n",
     "from tudatpy.math import interpolators, root_finders"

propagation/impact_manifolds_lpo_cr3bp.py

@@ -37,7 +37,7 @@
 # Tudatpy imports
 import tudatpy
 from tudatpy.util import result2array
-from tudatpy.kernel import numerical_simulation
+from tudatpy import numerical_simulation
 from tudatpy.numerical_simulation import propagation_setup, environment_setup, estimation_setup
 from tudatpy.astro import polyhedron_utilities
 from tudatpy.math import interpolators, root_finders

propagation/keplerian_satellite_orbit.ipynb

@@ -44,10 +44,10 @@
     "\n",
     "# Load tudatpy modules\n",
     "from tudatpy.interface import spice\n",
-    "from tudatpy.kernel import numerical_simulation\n",
+    "from tudatpy import numerical_simulation\n",
     "from tudatpy.numerical_simulation import environment_setup, propagation_setup\n",
     "from tudatpy.astro import element_conversion\n",
-    "from tudatpy.kernel import constants\n",
+    "from tudatpy import constants\n",
     "from tudatpy.util import result2array"
    ]
   },

propagation/keplerian_satellite_orbit.py

@@ -30,10 +30,10 @@
 
 # Load tudatpy modules
 from tudatpy.interface import spice
-from tudatpy.kernel import numerical_simulation
+from tudatpy import numerical_simulation
 from tudatpy.numerical_simulation import environment_setup, propagation_setup
 from tudatpy.astro import element_conversion
-from tudatpy.kernel import constants
+from tudatpy import constants
 from tudatpy.util import result2array
 
 

propagation/linear_sensitivity_analysis.ipynb

@@ -45,10 +45,10 @@
     "\n",
     "# Load tudatpy modules\n",
     "from tudatpy.interface import spice\n",
-    "from tudatpy.kernel import numerical_simulation\n",
+    "from tudatpy import numerical_simulation\n",
     "from tudatpy.numerical_simulation import environment_setup, propagation_setup, estimation_setup\n",
     "from tudatpy.astro import element_conversion\n",
-    "from tudatpy.kernel import constants\n",
+    "from tudatpy import constants\n",
     "from tudatpy.util import result2array"
    ]
   },

propagation/linear_sensitivity_analysis.py

@@ -30,10 +30,10 @@
 
 # Load tudatpy modules
 from tudatpy.interface import spice
-from tudatpy.kernel import numerical_simulation
+from tudatpy import numerical_simulation
 from tudatpy.numerical_simulation import environment_setup, propagation_setup, estimation_setup
 from tudatpy.astro import element_conversion
-from tudatpy.kernel import constants
+from tudatpy import constants
 from tudatpy.util import result2array
 
 

propagation/mga_trajectories.ipynb

@@ -72,7 +72,7 @@
     "from tudatpy.trajectory_design import transfer_trajectory, shape_based_thrust\n",
     "from tudatpy.numerical_simulation import environment_setup\n",
     "from tudatpy.util import result2array\n",
-    "from tudatpy.kernel import constants"
+    "from tudatpy import constants"
    ]
   },
   {

propagation/mga_trajectories.py

@@ -46,7 +46,7 @@
 from tudatpy.trajectory_design import transfer_trajectory, shape_based_thrust
 from tudatpy.numerical_simulation import environment_setup
 from tudatpy.util import result2array
-from tudatpy.kernel import constants
+from tudatpy import constants
 
 
 # First, let's explore an MGA transfer trajectory with no thrust applied during the transfer legs. In this case, the impulsive $\Delta$Vs are only applied during the gravity assists.

propagation/perturbed_satellite_orbit.ipynb

@@ -44,10 +44,10 @@
     "\n",
     "# Load tudatpy modules\n",
     "from tudatpy.interface import spice\n",
-    "from tudatpy.kernel import numerical_simulation\n",
+    "from tudatpy import numerical_simulation\n",
     "from tudatpy.numerical_simulation import environment_setup, propagation_setup\n",
     "from tudatpy.astro import element_conversion\n",
-    "from tudatpy.kernel import constants\n",
+    "from tudatpy import constants\n",
     "from tudatpy.util import result2array"
    ]
   },

propagation/perturbed_satellite_orbit.py

@@ -29,10 +29,10 @@
 
 # Load tudatpy modules
 from tudatpy.interface import spice
-from tudatpy.kernel import numerical_simulation
+from tudatpy import numerical_simulation
 from tudatpy.numerical_simulation import environment_setup, propagation_setup
 from tudatpy.astro import element_conversion
-from tudatpy.kernel import constants
+from tudatpy import constants
 from tudatpy.util import result2array
 
 

propagation/reentry_trajectory.ipynb

@@ -75,10 +75,10 @@
    "source": [
     "# Load tudatpy modules\n",
     "from tudatpy.interface import spice\n",
-    "from tudatpy.kernel import numerical_simulation\n",
+    "from tudatpy import numerical_simulation\n",
     "from tudatpy.numerical_simulation import environment_setup, environment, propagation_setup, propagation\n",
     "from tudatpy.astro import element_conversion\n",
-    "from tudatpy.kernel import constants\n",
+    "from tudatpy import constants\n",
     "from tudatpy.util import result2array"
    ]
   },

propagation/reentry_trajectory.py

@@ -37,10 +37,10 @@
 
 # Load tudatpy modules
 from tudatpy.interface import spice
-from tudatpy.kernel import numerical_simulation
+from tudatpy import numerical_simulation
 from tudatpy.numerical_simulation import environment_setup, environment, propagation_setup, propagation
 from tudatpy.astro import element_conversion
-from tudatpy.kernel import constants
+from tudatpy import constants
 from tudatpy.util import result2array
 
 

propagation/separation_satellites_diff_drag.ipynb

@@ -50,8 +50,8 @@
     "from scipy import interpolate\n",
     "\n",
     "# Load tudatpy modules\n",
-    "from tudatpy.kernel import constants\n",
-    "from tudatpy.kernel import numerical_simulation\n",
+    "from tudatpy import constants\n",
+    "from tudatpy import numerical_simulation\n",
     "from tudatpy.astro import element_conversion\n",
     "from tudatpy.interface import spice_interface\n",
     "from tudatpy.numerical_simulation import environment_setup, propagation_setup, propagation\n",

propagation/separation_satellites_diff_drag.py

@@ -30,8 +30,8 @@
 from scipy import interpolate
 
 # Load tudatpy modules
-from tudatpy.kernel import constants
-from tudatpy.kernel import numerical_simulation
+from tudatpy import constants
+from tudatpy import numerical_simulation
 from tudatpy.astro import element_conversion
 from tudatpy.interface import spice_interface
 from tudatpy.numerical_simulation import environment_setup, propagation_setup, propagation

propagation/solar_system_propagation.ipynb

@@ -48,9 +48,9 @@
     "\n",
     "# Load tudatpy modules\n",
     "from tudatpy.interface import spice\n",
-    "from tudatpy.kernel import numerical_simulation\n",
+    "from tudatpy import numerical_simulation\n",
     "from tudatpy.numerical_simulation import environment_setup, propagation_setup, propagation\n",
-    "from tudatpy.kernel import constants\n",
+    "from tudatpy import constants\n",
     "from tudatpy.util import result2array"
    ]
   },

propagation/solar_system_propagation.py

@@ -34,9 +34,9 @@
 
 # Load tudatpy modules
 from tudatpy.interface import spice
-from tudatpy.kernel import numerical_simulation
+from tudatpy import numerical_simulation
 from tudatpy.numerical_simulation import environment_setup, propagation_setup, propagation
-from tudatpy.kernel import constants
+from tudatpy import constants
 from tudatpy.util import result2array
 
 

propagation/thrust_between_Earth_Moon.ipynb

@@ -64,9 +64,9 @@
     "\n",
     "# # Load tudatpy modules\n",
     "from tudatpy.interface import spice\n",
-    "from tudatpy.kernel import numerical_simulation\n",
+    "from tudatpy import numerical_simulation\n",
     "from tudatpy.numerical_simulation import environment_setup, propagation_setup\n",
-    "from tudatpy.kernel import constants\n",
+    "from tudatpy import constants\n",
     "from tudatpy.util import result2array"
    ]
   },

propagation/thrust_between_Earth_Moon.py

@@ -40,9 +40,9 @@
 
 # Load tudatpy modules
 from tudatpy.interface import spice
-from tudatpy.kernel import numerical_simulation
+from tudatpy import numerical_simulation
 from tudatpy.numerical_simulation import environment_setup, propagation_setup
-from tudatpy.kernel import constants
+from tudatpy import constants
 from tudatpy.util import result2array
 
 

propagation/two_stage_rocket_ascent.ipynb

@@ -46,10 +46,10 @@
     "\n",
     "# Load tudatpy modules\n",
     "from tudatpy.interface import spice\n",
-    "from tudatpy.kernel import numerical_simulation\n",
+    "from tudatpy import numerical_simulation\n",
     "from tudatpy.numerical_simulation import environment, environment_setup, propagation, propagation_setup\n",
     "from tudatpy.astro import element_conversion, time_conversion\n",
-    "from tudatpy.kernel import constants\n",
+    "from tudatpy import constants\n",
     "from tudatpy.util import result2array"
    ]
   },

propagation/two_stage_rocket_ascent.py

@@ -34,10 +34,10 @@
 
 # Load tudatpy modules
 from tudatpy.interface import spice
-from tudatpy.kernel import numerical_simulation
+from tudatpy import numerical_simulation
 from tudatpy.numerical_simulation import environment, environment_setup, propagation, propagation_setup
 from tudatpy.astro import element_conversion, time_conversion
-from tudatpy.kernel import constants
+from tudatpy import constants
 from tudatpy.util import result2array
 
 

pygmo/asteroid_orbit_optimization/aoo_custom_environment.ipynb

@@ -60,11 +60,11 @@
     "\n",
     "# Load tudatpy modules\n",
     "from tudatpy.io import save2txt\n",
-    "from tudatpy.kernel import constants\n",
+    "from tudatpy import constants\n",
     "from tudatpy.interface import spice\n",
     "from tudatpy.astro import element_conversion\n",
     "from tudatpy.astro import frame_conversion\n",
-    "from tudatpy.kernel import numerical_simulation\n",
+    "from tudatpy import numerical_simulation\n",
     "from tudatpy.numerical_simulation import environment_setup\n",
     "from tudatpy.numerical_simulation import propagation_setup\n",
     "from tudatpy.util import pareto_optimums\n",

pygmo/asteroid_orbit_optimization/aoo_custom_environment.py

@@ -43,11 +43,11 @@
 
 # Load tudatpy modules
 from tudatpy.io import save2txt
-from tudatpy.kernel import constants
+from tudatpy import constants
 from tudatpy.interface import spice
 from tudatpy.astro import element_conversion
 from tudatpy.astro import frame_conversion
-from tudatpy.kernel import numerical_simulation
+from tudatpy import numerical_simulation
 from tudatpy.numerical_simulation import environment_setup
 from tudatpy.numerical_simulation import propagation_setup
 from tudatpy.util import pareto_optimums

pygmo/asteroid_orbit_optimization/aoo_design_space_exploration.ipynb

@@ -65,11 +65,11 @@
     "\n",
     "# Load tudatpy modules\n",
     "from tudatpy.io import save2txt\n",
-    "from tudatpy.kernel import constants\n",
+    "from tudatpy import constants\n",
     "from tudatpy.interface import spice\n",
     "from tudatpy.astro import element_conversion\n",
     "from tudatpy.astro import frame_conversion\n",
-    "from tudatpy.kernel import numerical_simulation\n",
+    "from tudatpy import numerical_simulation\n",
     "from tudatpy.numerical_simulation import environment_setup\n",
     "from tudatpy.numerical_simulation import propagation_setup\n",
     "import tudatpy.util as util\n",

pygmo/asteroid_orbit_optimization/aoo_design_space_exploration.py

@@ -51,11 +51,11 @@
 
 # Load tudatpy modules
 from tudatpy.io import save2txt
-from tudatpy.kernel import constants
+from tudatpy import constants
 from tudatpy.interface import spice
 from tudatpy.astro import element_conversion
 from tudatpy.astro import frame_conversion
-from tudatpy.kernel import numerical_simulation
+from tudatpy import numerical_simulation
 from tudatpy.numerical_simulation import environment_setup
 from tudatpy.numerical_simulation import propagation_setup
 import tudatpy.util as util