poliastro.plotting.porkchop
¶
This is the implementation of porkchop plot
Module Contents¶
Classes¶
Class Implementation for Porkchop Plot |
Attributes¶
- poliastro.plotting.porkchop.targetting_vec¶
- class poliastro.plotting.porkchop.PorkchopPlotter(departure_body, target_body, launch_span, arrival_span, ax=None, tfl=True, vhp=True, max_c3=45.0 * u.km ** 2 / u.s ** 2, max_vhp=5 * u.km / u.s)¶
Class Implementation for Porkchop Plot
- Parameters
departure_body (poliastro.bodies.Body) – Body from which departure is done
target_body (poliastro.bodies.Body) – Body for targetting
launch_span (astropy.time.Time) – Time span for launch
arrival_span (astropy.time.Time) – Time span for arrival
ax (matplotlib.axes.Axes) – For custom figures
tfl (bool) – For plotting time flight contour lines
vhp (bool) – For plotting arrival velocity contour lines
max_c3 (float) – Sets the maximum C3 value for porkchop
max_vhp (float) – Sets the maximum arrival velocity for porkchop
- porkchop(self)¶
Plots porkchop between two bodies.
- Returns
dv_launch (numpy.ndarray) – Launch delta v
dv_arrival (numpy.ndarray) – Arrival delta v
c3_launch (numpy.ndarray) – Characteristic launch energy
c3_arrrival (numpy.ndarray) – Characteristic arrival energy
tof (numpy.ndarray) – Time of flight for each transfer
Examples
>>> from poliastro.plotting.porkchop import PorkchopPlotter >>> from poliastro.bodies import Earth, Mars >>> from poliastro.util import time_range >>> launch_span = time_range("2005-04-30", end="2005-10-07") >>> arrival_span = time_range("2005-11-16", end="2006-12-21") >>> porkchop_plot = PorkchopPlotter(Earth, Mars, launch_span, arrival_span) >>> dv_launch, dev_dpt, c3dpt, c3arr, tof = porkchop_plot.porkchop()