SSAPy Toolkit
Contents:
Usage Guide
API Reference
Package
Subpackages
ssapy_toolkit.Accelerations
ssapy_toolkit.Compute
ssapy_toolkit.Coordinates
ssapy_toolkit.IO
ssapy_toolkit.Integrators
ssapy_toolkit.Orbital_Mechanics
ssapy_toolkit.Orbital_Mechanics.all_orbit_quanities
ssapy_toolkit.Orbital_Mechanics.burn_to_deltav
ssapy_toolkit.Orbital_Mechanics.calculate_finite_burn_acceleration
ssapy_toolkit.Orbital_Mechanics.deltav_to_burn
ssapy_toolkit.Orbital_Mechanics.ellipse_fit
ssapy_toolkit.Orbital_Mechanics.ellipse_from_rv
ssapy_toolkit.Orbital_Mechanics.ellipse_inject
ssapy_toolkit.Orbital_Mechanics.equally_spaced_ta
ssapy_toolkit.Orbital_Mechanics.gamma_and_heading
ssapy_toolkit.Orbital_Mechanics.keplerian
ssapy_toolkit.Orbital_Mechanics.lagrange_points
ssapy_toolkit.Orbital_Mechanics.launch_pads
ssapy_toolkit.Orbital_Mechanics.misc
ssapy_toolkit.Orbital_Mechanics.orbital_accel_model_comparisons
ssapy_toolkit.Orbital_Mechanics.orbital_comparison_stats
ssapy_toolkit.Orbital_Mechanics.rv_to_ellipse
ssapy_toolkit.Orbital_Mechanics.synthetic_orbit_population
ssapy_toolkit.Orbital_Mechanics.transfer_coplanar
ssapy_toolkit.Orbital_Mechanics.transfer_coplanar_continuous
ssapy_toolkit.Orbital_Mechanics.transfer_hohmann
ssapy_toolkit.Orbital_Mechanics.transfer_inclination_continuous
ssapy_toolkit.Orbital_Mechanics.transfer_lambertian
ssapy_toolkit.Orbital_Mechanics.transfer_rendezvous
ssapy_toolkit.Orbital_Mechanics.transfer_shooter
ssapy_toolkit.Orbital_Mechanics.transfer_shooter_continuous
ssapy_toolkit.Orbital_Mechanics.transfer_velocity_and_inclination_continuous
ssapy_toolkit.Orbital_Mechanics.transfer_velocity_continuous
ssapy_toolkit.Plots
ssapy_toolkit.Rockets
ssapy_toolkit.SSAPy_wrappers
ssapy_toolkit.Time_Functions
ssapy_toolkit.Yastropy
Top-level modules
SSAPy Toolkit
API Reference
ssapy_toolkit.Orbital_Mechanics
ssapy_toolkit.Orbital_Mechanics.ellipse_fit
View page source
ssapy_toolkit.Orbital_Mechanics.ellipse_fit
ssapy_toolkit.Orbital_Mechanics.
ellipse_fit
(
P1_m
,
P2_m
,
*
,
a_m
=
None
,
e
=
None
,
F2_m
=
None
,
inc
:
float
=
0.0
,
inc_deg
=
None
,
n_pts
:
int
=
1000
,
tol
=
1e-10
,
v_pref_m_s
=
None
,
plot
=
False
,
save_path
=
False
,
time_of_departure
=
None
,
time_of_arrival
=
None
)
[source]