FiniteBurn.Y_Component Property 
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DescriptionThis property has been Deprecated. Please use the BurnDirection vector instead.
For AttitudeSystem = 0, MJ2000 Ydirected unit vector component of the maneuver. For AttitudeSystem = 1, Orbit Normal directed unit vector component of the maneuver. For AttitudeSystem = 2, Negative Orbit Normal directed unit vector component of the maneuver. For AttitudeSystem = 3, the Spacecraft's attitude is adjusted so that Spacecraft.EulerAngle2 is temporarily set to the value specified by FiniteBurn.Y_Component for the duration of the maneuver. The Euler angle is evaluated in degrees and is referenced to the Spacecraft's attitude reference frame. The Euler Sequence used by the FiniteBurn object is defined by the Spacecraft object's Euler Sequence. Individual thruster orientations defined in the Thruster object(s) are used for directing deltav. For AttitudeSystem = 4, Negative Orbit Normal directed unit vector component of the maneuver. For AttitudeSystem = 5, Velocity directed component of the maneuver.
Timing Precision Mode This page describes functionality in millisecond timing precision mode.
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