ImpulsiveBurn.X_Component Property 
Top 
DescriptionThis property has been Deprecated. Please use the BurnDirection vector instead.
For AttitudeSystem = 0, MJ2000 Xdirected unit vector component of the maneuver. For AttitudeSystem = 1, Velocity directed unit vector component of the maneuver. For AttitudeSystem = 2, CoVelocity directed unit vector component of the maneuver. For AttitudeSystem = 3, the Spacecraft's attitude is adjusted so that Spacecraft.EulerAngle1 is temporarily set to the value specified by FiniteBurn.X_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, Y cross Z directed unit vector component of the maneuver. For AttitudeSystem = 5, Position directed component of the maneuver.
Timing Precision Mode This page describes functionality in millisecond timing precision mode.
Attributes
Syntax
See also
