Index

A

add_aacgm_coordinates() (in module pysatMissions.methods.magcoord)

add_quasi_dipole_coordinates() (in module pysatMissions.methods.magcoord) add_ram_pointing_sc_attitude_vectors() (in module pysatMissions.methods.spacecraft)

C

calculate_ecef_velocity() (in module pysatMissions.methods.spacecraft)

convert_from_keplerian() (in module pysatMissions.instruments.methods.orbits) convert_to_keplerian() (in module pysatMissions.instruments.methods.orbits)

I

init() (in module pysatMissions.instruments.missions_ephem) (in module pysatMissions.instruments.missions_sgp4) (in module pysatMissions.instruments.missions_skyfield)

L

load() (in module pysatMissions.instruments.missions_ephem) (in module pysatMissions.instruments.missions_sgp4) (in module pysatMissions.instruments.missions_skyfield)

M

module pysatMissions.instruments.methods.orbits pysatMissions.instruments.missions_ephem pysatMissions.instruments.missions_sgp4 pysatMissions.instruments.missions_skyfield pysatMissions.methods.magcoord pysatMissions.methods.spacecraft

N

normalize() (in module pysatMissions.methods.spacecraft)

P

preprocess() (in module pysatMissions.instruments.missions_ephem) project_ecef_vector_onto_sc() (in module pysatMissions.methods.spacecraft) pysatMissions.instruments.methods.orbits module pysatMissions.instruments.missions_ephem module pysatMissions.instruments.missions_sgp4 module

pysatMissions.instruments.missions_skyfield module pysatMissions.methods.magcoord module pysatMissions.methods.spacecraft module