ccsds_ndm.models.ndmxml2.ndmxml_2_0_0_opm_2_0

This file was generated by xsdata, v26.1, on 2026-02-18 00:40:07

Generator: DataclassGenerator See: https://xsdata.readthedocs.io/

Classes

KeplerianElementsType(*, comment, ...)
ManeuverParametersType(*, comment, ...)
OpmBody(*, segment)
OpmData(*, comment, state_vector, ...)
OpmMetadata(*, comment, object_name, ...)
OpmSegment(*, metadata, data)
OpmType(*, header, body)

class KeplerianElementsType(*, comment: 'list[str]' = <factory>, semi_major_axis: 'DistanceType', eccentricity: 'float', inclination: 'InclinationType', ra_of_asc_node: 'AngleType', arg_of_pericenter: 'AngleType', true_anomaly: 'None | AngleType' = None, mean_anomaly: 'None | AngleType' = None, gm: 'GmType')

Parameters:

• comment (list[str])

• semi_major_axis (DistanceType)

• eccentricity (float)

• inclination (InclinationType)

• ra_of_asc_node (AngleType)

• arg_of_pericenter (AngleType)

• true_anomaly (None | AngleType)

• mean_anomaly (None | AngleType)

• gm (GmType)

class ManeuverParametersType(*, comment: 'list[str]' = <factory>, man_epoch_ignition: 'str', man_duration: 'DurationType', man_delta_mass: 'DeltamassType', man_ref_frame: 'str', man_dv_1: 'VelocityType', man_dv_2: 'VelocityType', man_dv_3: 'VelocityType')

Parameters:

• comment (list[str])

• man_epoch_ignition (str)

• man_duration (DurationType)

• man_delta_mass (DeltamassType)

• man_ref_frame (str)

• man_dv_1 (VelocityType)

• man_dv_2 (VelocityType)

• man_dv_3 (VelocityType)

class OpmBody(*, segment: 'OpmSegment')

Parameters:

segment (OpmSegment)

class OpmData(*, comment: 'list[str]' = <factory>, state_vector: 'StateVectorType', keplerian_elements: 'None | KeplerianElementsType' = None, spacecraft_parameters: 'None | SpacecraftParametersType' = None, covariance_matrix: 'None | OpmCovarianceMatrixType' = None, maneuver_parameters: 'list[ManeuverParametersType]' = <factory>, user_defined_parameters: 'None | UserDefinedType' = None)

Parameters:

• comment (list[str])

• state_vector (StateVectorType)

• keplerian_elements (None | KeplerianElementsType)

• spacecraft_parameters (None | SpacecraftParametersType)

• covariance_matrix (None | OpmCovarianceMatrixType)

• maneuver_parameters (list[ManeuverParametersType])

• user_defined_parameters (None | UserDefinedType)

class OpmMetadata(*, comment: 'list[str]' = <factory>, object_name: 'str', object_id: 'str', center_name: 'str', ref_frame: 'str', ref_frame_epoch: 'None | str' = None, time_system: 'str')

Parameters:

• comment (list[str])

• object_name (str)

• object_id (str)

• center_name (str)

• ref_frame (str)

• ref_frame_epoch (None | str)

• time_system (str)

class OpmSegment(*, metadata: 'OpmMetadata', data: 'OpmData')

Parameters:

• metadata (OpmMetadata)

• data (OpmData)

class OpmType(*, header: 'NdmHeader', body: 'OpmBody')

Parameters:

• header (NdmHeader)

• body (OpmBody)