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fix: astrodynamics notebooks (#116)
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* feat: fix astrodynamics notebooks

* feat: update Visualization notebook
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@vishwa2710
vishwa2710 authored May 7, 2024
1 parent 0d4421d commit d8310c5
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Showing 10 changed files with 216 additions and 414 deletions.
8 changes: 4 additions & 4 deletions ...ss Platform Validation/OSTk Cross Platform Validation (Mission Sequence Scenario 1).ipynb
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"tags": []
},
"source": [
"# Validation Plots "
"## Validation Plots "
]
},
{
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" )\n",
" )\n",
"\n",
"figure.show()"
"figure.show(\"svg\")"
]
},
{
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" )\n",
" )\n",
"\n",
"figure.show()"
"figure.show(\"svg\")"
]
}
],
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},
"nbformat": 4,
"nbformat_minor": 4
}
}
8 changes: 4 additions & 4 deletions ...ss Platform Validation/OSTk Cross Platform Validation (Mission Sequence Scenario 2).ipynb
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"tags": []
},
"source": [
"# Validation Plots "
"## Validation Plots "
]
},
{
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" )\n",
" )\n",
"\n",
"figure.show()"
"figure.show(\"svg\")"
]
},
{
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" )\n",
" )\n",
"\n",
"figure.show()"
"figure.show(\"svg\")"
]
}
],
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},
"nbformat": 4,
"nbformat_minor": 4
}
}
8 changes: 4 additions & 4 deletions ...ss Platform Validation/OSTk Cross Platform Validation (Mission Sequence Scenario 3).ipynb
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"tags": []
},
"source": [
"# Validation Plots "
"## Validation Plots "
]
},
{
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" )\n",
" )\n",
"\n",
"figure.show()"
"figure.show(\"svg\")"
]
},
{
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" )\n",
" )\n",
"\n",
"figure.show()"
"figure.show(\"svg\")"
]
}
],
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},
"nbformat": 4,
"nbformat_minor": 4
}
}
8 changes: 4 additions & 4 deletions ...ss Platform Validation/OSTk Cross Platform Validation (Mission Sequence Scenario 4).ipynb
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"tags": []
},
"source": [
"# Validation Plots "
"## Validation Plots "
]
},
{
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" )\n",
" )\n",
"\n",
"figure.show()"
"figure.show(\"svg\")"
]
},
{
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" )\n",
" )\n",
"\n",
"figure.show()"
"figure.show(\"svg\")"
]
}
],
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},
"nbformat": 4,
"nbformat_minor": 4
}
}
63 changes: 5 additions & 58 deletions notebooks/Astrodynamics/Orbit Computation/Access Computation.ipynb
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"\n",
"import plotly.graph_objs as go\n",
"\n",
"from ostk.mathematics.objects import RealInterval\n",
"from ostk.mathematics.object import RealInterval\n",
"\n",
"from ostk.physics import Environment\n",
"from ostk.physics.unit import Length\n",
Expand All @@ -43,18 +43,18 @@
"from ostk.physics.time import DateTime\n",
"from ostk.physics.time import Time\n",
"from ostk.physics.coordinate.spherical import LLA\n",
"from ostk.physics.coordinate.spherical import AER\n",
"from ostk.physics.coordinate import Position\n",
"from ostk.physics.coordinate import Frame\n",
"from ostk.physics.environment.object.celestial import Earth\n",
"\n",
"from ostk.astrodynamics import Trajectory\n",
"from ostk.astrodynamics.trajectory import Orbit\n",
"from ostk.astrodynamics.trajectory.orbit.model import Kepler\n",
"from ostk.astrodynamics.trajectory.orbit.model.kepler import COE\n",
"from ostk.astrodynamics.trajectory.orbit.model import SGP4\n",
"from ostk.astrodynamics.trajectory.orbit.model.sgp4 import TLE\n",
"from ostk.astrodynamics.access import Generator as AccessGenerator"
"from ostk.astrodynamics.access import Generator as AccessGenerator\n",
"from ostk.astrodynamics.utilities import compute_trajectory_geometry\n",
"from ostk.astrodynamics.utilities import compute_time_lla_aer_state"
]
},
{
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"metadata": {},
"outputs": [],
"source": [
"def compute_lla(state):\n",
" lla = LLA.cartesian(\n",
" state.get_position()\n",
" .in_frame(Frame.ITRF(), state.get_instant())\n",
" .get_coordinates(),\n",
" earth.get_equatorial_radius(),\n",
" earth.get_flattening(),\n",
" )\n",
"\n",
" return [\n",
" float(lla.get_latitude().in_degrees()),\n",
" float(lla.get_longitude().in_degrees()),\n",
" float(lla.get_altitude().in_meters()),\n",
" ]\n",
"\n",
"\n",
"def compute_aer(instant, from_lla, to_position):\n",
" nedFrame = earth.get_frame_at(from_lla, Earth.FrameType.NED)\n",
"\n",
" fromPosition_NED = from_position.in_frame(nedFrame, instant)\n",
" sunPosition_NED = to_position.in_frame(nedFrame, instant)\n",
"\n",
" aer = AER.from_position_to_position(fromPosition_NED, sunPosition_NED, True)\n",
"\n",
" return [\n",
" float(aer.get_azimuth().in_degrees()),\n",
" float(aer.get_elevation().in_degrees()),\n",
" float(aer.get_range().in_meters()),\n",
" ]\n",
"\n",
"\n",
"def compute_time_lla_aer_state(state):\n",
" instant = state.get_instant()\n",
"\n",
" lla = compute_lla(state)\n",
" aer = compute_aer(\n",
" instant,\n",
" from_lla,\n",
" state.get_position().in_frame(Frame.ITRF(), state.get_instant()),\n",
" )\n",
"\n",
" return [instant, lla[0], lla[1], lla[2], aer[0], aer[1], aer[2]]\n",
"\n",
"\n",
"def compute_trajectory_geometry(aTrajectory, anInterval):\n",
" return [\n",
" compute_lla(state)\n",
" for state in aTrajectory.get_states_at(\n",
" anInterval.generate_grid(Duration.minutes(1.0))\n",
" )\n",
" ]\n",
"\n",
"\n",
"def compute_access_geometry(access):\n",
" return [\n",
" compute_time_lla_aer_state(state)\n",
" compute_time_lla_aer_state(state, from_lla, environment)\n",
" for state in satellite_orbit.get_states_at(\n",
" access.get_interval().generate_grid(Duration.seconds(1.0))\n",
" )\n",
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2 changes: 1 addition & 1 deletion notebooks/Astrodynamics/Orbit Computation/Find RF Interference Accesses.ipynb
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Expand Up @@ -36,7 +36,7 @@
"\n",
"from tqdm.notebook import tqdm\n",
"\n",
"from ostk.mathematics.objects import RealInterval\n",
"from ostk.mathematics.object import RealInterval\n",
"\n",
"from ostk.physics import Environment\n",
"from ostk.physics.coordinate import Position\n",
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