Index

_

__call__() (twobody.PolynomialRVTrend method)

A

a (twobody.KeplerElements attribute) (twobody.TwoBodyKeplerElements attribute)

a_m_to_P() (in module twobody) a_P_to_m() (in module twobody)

B

Barycenter (class in twobody)

barycenter (twobody.KeplerOrbit attribute)

D

decompose() (twobody.UnitSystem method)

default_differential (twobody.ReferencePlaneFrame attribute) default_representation (twobody.ReferencePlaneFrame attribute)

E

e (twobody.KeplerElements attribute) (twobody.TwoBodyKeplerElements attribute)

eccentric_anomaly_from_mean_anomaly() (in module twobody) eccentric_anomaly_from_true_anomaly() (in module twobody)

F

frame_attributes (twobody.ReferencePlaneFrame attribute)

frame_specific_representation_info (twobody.ReferencePlaneFrame attribute)

G

get_body() (twobody.TwoBodyKeplerElements method)

get_constant() (twobody.UnitSystem method) get_m2_min() (in module twobody)

I

i (twobody.KeplerElements attribute) (twobody.TwoBodyKeplerElements attribute)

icrs() (twobody.KeplerOrbit method)

K

K (twobody.KeplerElements attribute)

KeplerElements (class in twobody) KeplerOrbit (class in twobody)

M

M0 (twobody.KeplerElements attribute) (twobody.TwoBodyKeplerElements attribute) m1 (twobody.TwoBodyKeplerElements attribute) m2 (twobody.TwoBodyKeplerElements attribute)

m_f (twobody.KeplerElements attribute) mean_anomaly_from_eccentric_anomaly() (in module twobody) module twobody

N

name (twobody.ReferencePlaneFrame attribute) names (twobody.KeplerElements attribute) (twobody.OrbitalElements attribute) (twobody.TwoBodyKeplerElements attribute)

O

Omega (twobody.KeplerElements attribute) omega (twobody.KeplerElements attribute) Omega (twobody.TwoBodyKeplerElements attribute)

omega (twobody.TwoBodyKeplerElements attribute) orbital_plane() (twobody.KeplerOrbit method) OrbitalElements (class in twobody) origin (twobody.ReferencePlaneFrame attribute)

P

P (twobody.KeplerElements attribute) (twobody.TwoBodyKeplerElements attribute) P_m_to_a() (in module twobody)

plot_rv() (twobody.KeplerOrbit method) PolynomialRVTrend (class in twobody) primary (twobody.TwoBodyKeplerElements attribute)

R

radial_velocity() (twobody.KeplerOrbit method) reference_plane() (twobody.KeplerOrbit method)

ReferencePlaneFrame (class in twobody) RVTrend (class in twobody)

S

secondary (twobody.TwoBodyKeplerElements attribute)

T

test() (in module twobody) to_dict() (twobody.UnitSystem method) true_anomaly_from_eccentric_anomaly() (in module twobody)

twobody module TwoBodyKeplerElements (class in twobody)

U

UnitSystem (class in twobody)

unscaled_radial_velocity() (twobody.KeplerOrbit method) UnsupportedPythonError