ccsds_ndm.models.ndmxml1.ndmxml_1_0_apm_1_0

This file was generated by xsdata, v26.1, on 2026-02-18 00:40:52

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

Classes

ApmBody(*, segment)
ApmData(*, comment, quaternion_state, ...)
ApmMetadata(*, comment, object_name, ...)
ApmRateFrameType(*values)
ApmSegment(*, metadata, data)
ApmType(*, header, body)
AttManeuverParametersType(*, comment, ...)
AttSpacecraftParametersType(*, comment, ...)
EulerElementsSpinType(*, comment, ...)
EulerElementsThreeType(*, comment, ...)
MomentType(*, value[, units])
MomentUnits(*values)
QuaternionStateType(*, comment, epoch, ...)
TorqueType(*, value[, units])
TorqueUnits(*values)

class ApmBody(*, segment: 'ApmSegment')

Parameters:

segment (ApmSegment)

class ApmData(*, comment: 'list[str]' = <factory>, quaternion_state: 'QuaternionStateType', euler_elements_three: 'None | EulerElementsThreeType' = None, euler_elements_spin: 'None | EulerElementsSpinType' = None, spacecraft_parameters: 'None | AttSpacecraftParametersType' = None, maneuver_parameters: 'list[AttManeuverParametersType]' = <factory>)

Parameters:

• comment (list[str])

• quaternion_state (QuaternionStateType)

• euler_elements_three (None | EulerElementsThreeType)

• euler_elements_spin (None | EulerElementsSpinType)

• spacecraft_parameters (None | AttSpacecraftParametersType)

• maneuver_parameters (list[AttManeuverParametersType])

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

Parameters:

• comment (list[str])

• object_name (str)

• object_id (str)

• center_name (None | str)

• time_system (TimeSystemType)

class ApmRateFrameType(*values)

class ApmSegment(*, metadata: 'ApmMetadata', data: 'ApmData')

Parameters:

• metadata (ApmMetadata)

• data (ApmData)

class ApmType(*, header: 'NdmHeader', body: 'ApmBody')

Parameters:

• header (NdmHeader)

• body (ApmBody)

class AttManeuverParametersType(*, comment: 'list[str]' = <factory>, man_epoch_start: 'str', man_duration: 'DurationType', man_ref_frame: 'str', man_tor_1: 'TorqueType', man_tor_2: 'TorqueType', man_tor_3: 'TorqueType')

Parameters:

• comment (list[str])

• man_epoch_start (str)

• man_duration (DurationType)

• man_ref_frame (str)

• man_tor_1 (TorqueType)

• man_tor_2 (TorqueType)

• man_tor_3 (TorqueType)

class AttSpacecraftParametersType(*, comment: 'list[str]' = <factory>, inertia_ref_frame: 'None | str' = None, i11: 'MomentType', i22: 'MomentType', i33: 'MomentType', i12: 'MomentType', i13: 'MomentType', i23: 'MomentType')

Parameters:

• comment (list[str])

• inertia_ref_frame (None | str)

• i11 (MomentType)

• i22 (MomentType)

• i33 (MomentType)

• i12 (MomentType)

• i13 (MomentType)

• i23 (MomentType)

class EulerElementsSpinType(*, comment: 'list[str]' = <factory>, spin_frame_a: 'str', spin_frame_b: 'str', spin_dir: 'None | RotDirectionType' = None, spin_alpha: 'None | AngleType' = None, spin_delta: 'None | AngleType' = None, spin_angle: 'None | AngleType' = None, spin_angle_vel: 'None | AngleRateType' = None, nutation: 'None | AngleType' = None, nutation_per: 'None | DurationType' = None, nutation_phase: 'None | AngleType' = None)

Parameters:

• comment (list[str])

• spin_frame_a (str)

• spin_frame_b (str)

• spin_dir (None | RotDirectionType)

• spin_alpha (None | AngleType)

• spin_delta (None | AngleType)

• spin_angle (None | AngleType)

• spin_angle_vel (None | AngleRateType)

• nutation (None | AngleType)

• nutation_per (None | DurationType)

• nutation_phase (None | AngleType)

class EulerElementsThreeType(*, comment: 'list[str]' = <factory>, euler_frame_a: 'None | str' = None, euler_frame_b: 'None | str' = None, euler_dir: 'None | RotDirectionType' = None, euler_rot_seq: 'None | RotseqType' = None, rate_frame: 'None | ApmRateFrameType' = None, rotation_angles: 'None | RotationAngleType' = None, rotation_rates: 'None | RotationRateType' = None)

Parameters:

• comment (list[str])

• euler_frame_a (None | str)

• euler_frame_b (None | str)

• euler_dir (None | RotDirectionType)

• euler_rot_seq (None | RotseqType)

• rate_frame (None | ApmRateFrameType)

• rotation_angles (None | RotationAngleType)

• rotation_rates (None | RotationRateType)

class MomentType(*, value: 'float', units: 'None | MomentUnits' = None)

Parameters:

• value (float)

• units (None | MomentUnits)

q()

Return this value as a pint or astropy Quantity.

class MomentUnits(*values)

class QuaternionStateType(*, comment: 'list[str]' = <factory>, epoch: 'str', q_frame_a: 'str', q_frame_b: 'str', q_dir: 'RotDirectionType', quaternion: 'QuaternionType', quaternion_rate: 'None | QuaternionRateType' = None)

Parameters:

• comment (list[str])

• epoch (str)

• q_frame_a (str)

• q_frame_b (str)

• q_dir (RotDirectionType)

• quaternion (QuaternionType)

• quaternion_rate (None | QuaternionRateType)

class TorqueType(*, value: 'float', units: 'None | TorqueUnits' = None)

Parameters:

• value (float)

• units (None | TorqueUnits)

q()

Return this value as a pint or astropy Quantity.

class TorqueUnits(*values)