Index

_

__init__() (poliastro.bodies.Body method) (poliastro.maneuver.Maneuver method) (poliastro.plotting.OrbitPlotter method) (poliastro.plotting.OrbitPlotter2D method) (poliastro.plotting.OrbitPlotter3D method)

A

apply_maneuver() (poliastro.twobody.orbit.Orbit method) argp (poliastro.twobody.classical.ClassicalState attribute)

asteroid_db() (in module poliastro.neos.dastcom5) atmospheric_drag (in module poliastro.core.perturbations)

B

beta (in module poliastro.core.thrust.change_a_inc) beta_0 (in module poliastro.core.thrust.change_a_inc)

bielliptic() (poliastro.maneuver.Maneuver class method) Body (class in poliastro.bodies) body_centered_to_icrs() (in module poliastro.coordinates)

C

c2 (in module poliastro.core.stumpff) c3 (in module poliastro.core.stumpff) change_a_inc() (in module poliastro.twobody.thrust.change_a_inc) change_argp() (in module poliastro.twobody.thrust.change_argp) change_ecc_quasioptimal() (in module poliastro.twobody.thrust.change_ecc_quasioptimal) change_inc_ecc() (in module poliastro.twobody.thrust.change_inc_ecc) churi (in module poliastro.examples) circular() (poliastro.twobody.orbit.Orbit class method) circular_velocity (in module poliastro.core.util)

circular_velocity() (in module poliastro.util) ClassicalState (class in poliastro.twobody.classical) coe2mee (in module poliastro.core.elements) coe2rv (in module poliastro.core.elements) comet_db() (in module poliastro.neos.dastcom5) compute_flyby() (in module poliastro.threebody.flybys) compute_parameters (in module poliastro.core.thrust.change_a_inc) compute_soi() (in module poliastro.patched_conics) cowell() (in module poliastro.twobody.propagation) cross (in module poliastro.core.util)

D

D_to_M() (in module poliastro.twobody.angles) D_to_nu() (in module poliastro.twobody.angles) delta_V (in module poliastro.core.thrust.change_a_inc) (in module poliastro.core.thrust.change_argp) (in module poliastro.core.thrust.change_ecc_quasioptimal) (in module poliastro.core.thrust.change_inc_ecc)

download_dastcom5() (in module poliastro.neos.dastcom5)

E

E_to_M() (in module poliastro.twobody.angles) E_to_nu() (in module poliastro.twobody.angles) ecc (poliastro.twobody.classical.ClassicalState attribute) entire_db() (in module poliastro.neos.dastcom5)

epoch (poliastro.twobody.orbit.Orbit attribute) extra_quantities (in module poliastro.core.thrust.change_a_inc) (in module poliastro.core.thrust.change_argp) (in module poliastro.core.thrust.change_ecc_quasioptimal) (in module poliastro.core.thrust.change_inc_ecc)

F

f (poliastro.twobody.equinoctial.ModifiedEquinoctialState attribute) F_to_M() (in module poliastro.twobody.angles) F_to_nu() (in module poliastro.twobody.angles) fp_angle() (in module poliastro.twobody.angles) frame (poliastro.twobody.orbit.Orbit attribute)

from_body_ephem() (poliastro.twobody.orbit.Orbit class method) from_classical() (poliastro.twobody.orbit.Orbit class method) from_equinoctial() (poliastro.twobody.orbit.Orbit class method) from_vectors() (poliastro.twobody.orbit.Orbit class method) func_twobody() (in module poliastro.twobody.propagation)

G

g (poliastro.twobody.equinoctial.ModifiedEquinoctialState attribute) get_frame() (in module poliastro.frames)

get_total_cost() (poliastro.maneuver.Maneuver method) get_total_time() (poliastro.maneuver.Maneuver method)

H

h (poliastro.twobody.equinoctial.ModifiedEquinoctialState attribute) HCRS (class in poliastro.frames)

HeliocentricEclipticJ2000 (class in poliastro.frames) hohmann() (poliastro.maneuver.Maneuver class method) hyp2f1b (in module poliastro.core.hyper)

I

icrs_to_body_centered() (in module poliastro.coordinates) impulse() (poliastro.maneuver.Maneuver class method)

inc (poliastro.twobody.classical.ClassicalState attribute) inertial_body_centered_to_pqw() (in module poliastro.coordinates) iss (in module poliastro.examples)

J

J2_perturbation (in module poliastro.core.perturbations)

J3_perturbation (in module poliastro.core.perturbations) JupiterICRS (class in poliastro.frames)

K

k (poliastro.twobody.equinoctial.ModifiedEquinoctialState attribute)

L

L (poliastro.twobody.equinoctial.ModifiedEquinoctialState attribute) lagrange_points() (in module poliastro.threebody.restricted)

lagrange_points_vec() (in module poliastro.threebody.restricted) lambert() (in module poliastro.iod.izzo) (in module poliastro.iod.vallado)

M

M_to_D() (in module poliastro.twobody.angles) M_to_E() (in module poliastro.twobody.angles) M_to_F() (in module poliastro.twobody.angles) M_to_nu() (in module poliastro.twobody.angles) Maneuver (class in poliastro.maneuver)

MarsICRS (class in poliastro.frames) mean_motion (in module poliastro.core.propagation) mee2coe() (in module poliastro.twobody.equinoctial) MercuryICRS (class in poliastro.frames) ModifiedEquinoctialState (class in poliastro.twobody.equinoctial) molniya (in module poliastro.examples)

N

NeptuneICRS (class in poliastro.frames) norm (in module poliastro.core.util) norm() (in module poliastro.util) nu (poliastro.twobody.classical.ClassicalState attribute)

nu_to_D() (in module poliastro.twobody.angles) nu_to_E() (in module poliastro.twobody.angles) nu_to_F() (in module poliastro.twobody.angles) nu_to_M() (in module poliastro.twobody.angles)

O

Orbit (class in poliastro.twobody.orbit) orbit_from_name() (in module poliastro.neos.dastcom5) (in module poliastro.neos.neows) orbit_from_record() (in module poliastro.neos.dastcom5)

orbit_from_spk_id() (in module poliastro.neos.neows) OrbitPlotter (class in poliastro.plotting) OrbitPlotter2D (class in poliastro.plotting) OrbitPlotter3D (class in poliastro.plotting)

P

p (poliastro.twobody.classical.ClassicalState attribute) (poliastro.twobody.equinoctial.ModifiedEquinoctialState attribute) parabolic() (poliastro.twobody.orbit.Orbit class method) plane (poliastro.twobody.orbit.Orbit attribute) Planes (class in poliastro.frames) plot() (in module poliastro.plotting) (poliastro.plotting.OrbitPlotter method) plot3d() (in module poliastro.plotting) plot_solar_system() (in module poliastro.plotting) plot_trajectory() (poliastro.plotting.OrbitPlotter method) PlutoICRS (class in poliastro.frames) poliastro.bodies (module) poliastro.cli (module) poliastro.constants (module) poliastro.coordinates (module) poliastro.core.angles (module) poliastro.core.elements (module) poliastro.core.hyper (module) poliastro.core.iod (module) poliastro.core.perturbations (module) poliastro.core.propagation (module) poliastro.core.stumpff (module) poliastro.core.thrust.change_a_inc (module) poliastro.core.thrust.change_argp (module) poliastro.core.thrust.change_ecc_quasioptimal (module) poliastro.core.thrust.change_inc_ecc (module) poliastro.core.util (module)

poliastro.examples (module) poliastro.frames (module) poliastro.iod (module) poliastro.iod.izzo (module) poliastro.iod.vallado (module) poliastro.maneuver (module) poliastro.neos (module) poliastro.neos.dastcom5 (module) poliastro.neos.neows (module) poliastro.patched_conics (module) poliastro.plotting (module) poliastro.threebody.flybys (module) poliastro.threebody.restricted (module) poliastro.twobody (module) poliastro.twobody.angles (module) poliastro.twobody.classical (module) poliastro.twobody.decorators (module) poliastro.twobody.equinoctial (module) poliastro.twobody.orbit (module) poliastro.twobody.propagation (module) poliastro.twobody.rv (module) poliastro.twobody.thrust.change_a_inc (module) poliastro.twobody.thrust.change_argp (module) poliastro.twobody.thrust.change_ecc_quasioptimal (module) poliastro.twobody.thrust.change_inc_ecc (module) poliastro.util (module) propagate() (in module poliastro.twobody.propagation) (poliastro.twobody.orbit.Orbit method)

R

r (poliastro.twobody.rv.RVState attribute) raan (poliastro.twobody.classical.ClassicalState attribute) radiation_pressure() (in module poliastro.core.perturbations) read_headers() (in module poliastro.neos.dastcom5) read_record() (in module poliastro.neos.dastcom5) record_from_name() (in module poliastro.neos.dastcom5)

represent_as() (poliastro.twobody.orbit.Orbit method) rotate (in module poliastro.core.util) rotate() (in module poliastro.util) rv2coe (in module poliastro.core.elements) rv_pqw (in module poliastro.core.elements) RVState (class in poliastro.twobody.rv)

S

sample() (poliastro.twobody.orbit.Orbit method) SaturnICRS (class in poliastro.frames) set_attractor() (poliastro.plotting.OrbitPlotter method) set_frame() (poliastro.plotting.OrbitPlotter method) shadow_function (in module poliastro.core.perturbations)

soyuz_gto (in module poliastro.examples) spk_id_from_name() (in module poliastro.neos.neows) state (poliastro.twobody.orbit.Orbit attribute) state_from_vector() (in module poliastro.twobody.decorators) string_record_from_name() (in module poliastro.neos.dastcom5)

T

third_body() (in module poliastro.core.perturbations) time_range() (in module poliastro.util) TimeScaleWarning to_classical() (poliastro.twobody.classical.ClassicalState method) (poliastro.twobody.equinoctial.ModifiedEquinoctialState method) (poliastro.twobody.rv.RVState method)

to_equinoctial() (poliastro.twobody.classical.ClassicalState method) to_icrs() (poliastro.twobody.orbit.Orbit method) to_vectors() (poliastro.twobody.classical.ClassicalState method) (poliastro.twobody.rv.RVState method) transform (in module poliastro.core.util) transform() (in module poliastro.coordinates) (in module poliastro.util)

U

UranusICRS (class in poliastro.frames)

V

v (poliastro.twobody.rv.RVState attribute)

VenusICRS (class in poliastro.frames)