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IAgVeIntegratedAttitude Interface

Description

Integrated Attitude interface generates an external attitude file for a satellite by numerically integrating Euler's equations for the current satellite.

Public Methods

Public Method InitFromAttInitializes the parameters using a satellite's attitude.
Public Method SaveToFileGenerates an external attitude file for a satellite by numerically integrating Euler's equations for the current satellite and save results to the specified file.

Public Properties

Public Property EpochEpoch of the attitude file. Uses DateFormat Dimension.
Public Property OrientationGet the initial orientation of the satellite in the Earth Inertial (ECI) frame.
Public Property StartTimeStart time for the attitude file. Uses DateFormat Dimension.
Public Property StopTimeStop time for the attitude file. Uses DateFormat Dimension.
Public Property TorqueGet the external torque data.
Public Property WxBody fixed wx rate: initial angular velocity rate about the satellite's X axis. Uses AngleRate Dimension.
Public Property WyBody fixed wy rate: initial angular velocity rate about the satellite's Y axis. Uses AngleRate Dimension.
Public Property WzBody fixed wz rate: initial angular velocity rate about the satellite's Z axis. Uses AngleRate Dimension.
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