boinor.plotting.orbit.plotter¶
A module containing different orbit related plotters.
Classes¶
A class for collecting all information of a body within a plotter. |
|
A base class containing common attributes and methods for plotters. |
Module Contents¶
- class boinor.plotting.orbit.plotter.Trajectory¶
Bases:
namedtuple('Trajectory', ['coordinates','position','colors','dashed','label'])A class for collecting all information of a body within a plotter.
Information contains all the trajectory coordinates, the current position, the name of the label to be displayed in the plotter, the color to be used and if dashed mode is desired or not.
- class boinor.plotting.orbit.plotter.OrbitPlotter(backend=None, num_points=150, *, plane=None, length_scale_units=u.km)¶
A base class containing common attributes and methods for plotters.
- property backend¶
Backend instance used by the plotter.
- Returns:
An instance of
OrbitPlotterBackendused for rendendering the scene.- Return type:
OrbitPlotterBackend
- property plane¶
Reference plane to be used when drawing the scene.
- Returns:
Reference plane to be used when drawing the scene. Default to
- Return type:
Plane, optional
- property trajectories¶
List with all the Trajectory instances used in the plotter.
- Returns:
A list containing all the trajectories rendered in the scene.
- Return type:
List[Trajectory]
- property length_scale_units¶
Units of length used for representing distances.
- Returns:
length_units – Desired length units to be used when representing distances.
- Return type:
- set_attractor(attractor)¶
Set the desired plotting attractor.
- Parameters:
attractor (Body) – Central body.
- Raises:
NotImplementedError – Raised if attractor is already set.
- set_orbit_frame(orbit)¶
Set the perifocal frame based on an orbit.
- Parameters:
orbit (Orbit) – Orbit to use as frame.
- set_body_frame(body, epoch=None)¶
Set perifocal frame based on the orbit of a body at a particular epoch if given.
- Parameters:
body (boinor.bodies.SolarSystemPlanet) – Body.
epoch (astropy.time.Time, optional) – Epoch of current position.
- plot(orbit, *, color=None, label=None, trail=False, dashed=True)¶
Plot state and osculating orbit in their plane.
- plot_body_orbit(body, epoch, *, label=None, color=None, trail=False)¶
Plot complete revolution of body and current position.
- Parameters:
body (boinor.bodies.SolarSystemPlanet) – Body.
epoch (astropy.time.Time) – Epoch of current position.
label (str, optional) – Label of the orbit, default to the name of the body.
color (str, optional) – Color of the line and the position.
trail (bool, optional) – Fade the orbit trail, default to False.
- plot_ephem(ephem, epoch=None, *, label=None, color=None, trail=False)¶
Plot
Ephemobject over its sampling period.- Parameters:
ephem (Ephem) – Ephemerides to plot.
epoch (astropy.time.Time, optional) – Epoch of the current position, None is used if not given.
label (str, optional) – Label of the orbit, default to the name of the body.
color (str, optional) – Color of the line and the position.
trail (bool, optional) – Fade the orbit trail, default to False.
- plot_maneuver(initial_orbit, maneuver, label=None, color=None, trail=False)¶
Plot the maneuver trajectory applied to the provided initial orbit.
- Parameters:
- plot_coordinates(coordinates, *, position=None, label=None, color=None, trail=False, dashed=False)¶
Plot a precomputed trajectory.
- Parameters:
coordinates (CartesianRepresentation) – Trajectory to plot.
label (str, optional) – Label of the trajectory.
color (str, optional) – Color of the trajectory.
trail (bool, optional) – Fade the orbit trail, default to False.
dashed (bool, optional) –
Trueto use a dashed line style.Falseotherwise.
- Raises:
ValueError – An attractor must be set first.
- plot_trajectory(coordinates, *, label=None, color=None, trail=False, dashed=False)¶
Plot a precomputed trajectory.
- Parameters:
coordinates (CartesianRepresentation) – Trajectory to plot.
label (str, optional) – Label of the trajectory.
color (str, optional) – Color of the trajectory.
trail (bool, optional) – Fade the orbit trail, default to False.
dashed (bool, optional) –
Trueto use a dashed line style.Falseotherwise.
- Raises:
ValueError – An attractor must be set first.
- set_view(elevation_angle, azimuth_angle, distance=5 * u.km)¶
Change 3D view by setting the elevation, azimuth and distance.
- show()¶
Render the plot.