ostk.astrodynamics.trajectory.orbit.message.spacex.OPM¶

class OPM(self: ostk.astrodynamics.trajectory.orbit.message.spacex.OPM, header: ostk::astrodynamics::trajectory::orbit::message::spacex::OPM::Header, deployments: list[ostk::astrodynamics::trajectory::orbit::message::spacex::OPM::Deployment])¶

Bases: pybind11_object

The SpaceX OPM message.

See also

SpaceX OPM.

Constructor.

Parameters:

header (Header) -- The header of the OPM message.
deployments (list[Deployment]) -- The deployments of the OPM message.

Methods

`dictionary`	Build an OPM message from a dictionary.
`get_deployment_at`	Get the deployment at a given index.
`get_deployment_with_name`	Get the deployment with a given name.
`get_deployments`	Get the deployments of the OPM message.
`get_header`	Get the header of the OPM message.
`is_defined`	Check if the OPM message is defined.
`load`	Load an OPM message from a file.
`parse`	Parse an OPM message from a string.
`undefined`	Return an undefined OPM message.

class Deployment( self: ostk.astrodynamics.trajectory.orbit.message.spacex.OPM.Deployment, name: ostk.core.type.String, sequence_number: ostk.core.type.Integer, mission_time: ostk.physics.time.Duration, date: ostk.physics.time.Instant, position: ostk.physics.coordinate.Position, velocity: ostk.physics.coordinate.Velocity, mean_perigee_altitude: ostk.physics.unit.Length, mean_apogee_altitude: ostk.physics.unit.Length, mean_inclination: ostk.physics.unit.Angle, mean_argument_of_perigee: ostk.physics.unit.Angle, mean_longitude_ascending_node: ostk.physics.unit.Angle, mean_mean_anomaly: ostk.physics.unit.Angle, ballistic_coefficient: ostk.core.type.Real, )¶

Bases: pybind11_object

The deployment of the SpaceX OPM message.

Constructor.

Parameters:

name (str) -- The name of the deployment.
sequence_number (int) -- The sequence number of the deployment.
mission_time (Duration) -- The mission time of the deployment.
date (Instant) -- The date of the deployment.
position (Position) -- The position of the deployment.
velocity (Velocity) -- The velocity of the deployment.
mean_perigee_altitude (Length) -- The mean perigee altitude of the deployment.
mean_apogee_altitude (Length) -- The mean apogee altitude of the deployment.
mean_inclination (Angle) -- The mean inclination of the deployment.
mean_argument_of_perigee (Angle) -- The mean argument of perigee of the deployment.
mean_longitude_ascending_node (Angle) -- The mean longitude of the ascending node of the deployment.
mean_mean_anomaly (Angle) -- The mean mean anomaly of the deployment.
ballistic_coefficient (float) -- The ballistic coefficient of the deployment.

property ballistic_coefficient¶

Get the ballistic coefficient of the deployment.

Type:: float

property date¶

Get the date of the deployment.

Type:: Instant

property mean_apogee_altitude¶

Get the mean apogee altitude of the deployment.

Type:: Length

property mean_argument_of_perigee¶

Get the mean argument of perigee of the deployment.

Type:: Angle

property mean_inclination¶

Get the mean inclination of the deployment.

Type:: Angle

property mean_longitude_ascending_node¶

Get the mean longitude of the ascending node of the deployment.

Type:: Angle

property mean_mean_anomaly¶

Get the mean mean anomaly of the deployment.

Type:: Angle

property mean_perigee_altitude¶

Get the mean perigee altitude of the deployment.

Type:: Length

property mission_time¶

Get the mission time of the deployment.

Type:: Duration

property name¶

Get the name of the deployment.

Type:: str

property position¶

Get the position of the deployment.

Type:: Position

property sequence_number¶

Get the sequence number of the deployment.

Type:: int

to_state( self: ostk.astrodynamics.trajectory.orbit.message.spacex.OPM.Deployment, ) → ostk.astrodynamics.trajectory.State¶

Convert the deployment to a state.

Returns:: The state of the deployment.
Return type:: state (State)

property velocity¶

Get the velocity of the deployment.

Type:: Velocity

class Header( self: ostk.astrodynamics.trajectory.orbit.message.spacex.OPM.Header, generation_date: ostk.physics.time.Instant, launch_date: ostk.physics.time.Instant, )¶

Bases: pybind11_object

The header of the SpaceX OPM message.

Constructor.

Parameters:

generation_date (Instant) -- The date at which the OPM message was generated.
launch_date (Instant) -- The date at which the spacecraft was launched.

property generation_date¶

Get the date at which the OPM message was generated.

Returns:: The date at which the OPM message was generated.
Return type:: instant (Instant)

property launch_date¶

Get the date at which the spacecraft was launched.

Returns:: The date at which the spacecraft was launched.
Return type:: instant (Instant)

static dictionary( dictionary: ostk.core.container.Dictionary, ) → ostk.astrodynamics.trajectory.orbit.message.spacex.OPM¶

Build an OPM message from a dictionary.

Parameters:: dictionary (dict) -- The dictionary containing the OPM message information.
Returns:: The OPM message.
Return type:: opm (OPM)

get_deployment_at( self: ostk.astrodynamics.trajectory.orbit.message.spacex.OPM, index: int, ) → ostk::astrodynamics::trajectory::orbit::message::spacex::OPM::Deployment¶

Get the deployment at a given index.

Parameters:: index (int) -- The index of the deployment.
Returns:: The deployment at the given index.
Return type:: deployment (Deployment)

get_deployment_with_name( self: ostk.astrodynamics.trajectory.orbit.message.spacex.OPM, name: ostk.core.type.String, ) → ostk::astrodynamics::trajectory::orbit::message::spacex::OPM::Deployment¶

Get the deployment with a given name.

Parameters:: name (str) -- The name of the deployment.
Returns:: The deployment with the given name.
Return type:: deployment (Deployment)

get_deployments( self: ostk.astrodynamics.trajectory.orbit.message.spacex.OPM, ) → list[ostk::astrodynamics::trajectory::orbit::message::spacex::OPM::Deployment]¶

Get the deployments of the OPM message.

Returns:: The deployments of the OPM message.
Return type:: deployments (list[Deployment])

get_header( self: ostk.astrodynamics.trajectory.orbit.message.spacex.OPM, ) → ostk::astrodynamics::trajectory::orbit::message::spacex::OPM::Header¶