Three weeks have passed since the coding phase began and new features have been added to the software:
- Lambert is now a
- A trail keyword in
StaticOrbitPlotterfor showing orbits' trails.
Lambert just needs now two orbits!
Although the raw algorithms are kept under the module
poliastro.iod, it is
possible now to simplify the process of solving this famous astrodynamics
problem by making use of the
Imagine that we want to solve the classical problem ongoing from Earth to Mars
for a trip of 600 days duration. Let us compare before and after
With 0.12 version:
from astropy import units as u from astropy.time import Time from poliastro.bodies import Earth, Mars, Sun from poliastro.iod.izzo import lambert from poliastro.twobody import Orbit LAUNCH = Time.now …