Target_Vector_Outgoing_Asymptote

This attribute sets the values for Target Vector Outgoing Asymptote elements used to define the spacecraft's Initial State.

Syntax

Astrogator <Satellite Object Path> SetValue <Astrogator Object Path>.Target_Vector_Outgoing_Asymptote.{Element} <Value> <Unit>

Description

If you select Target Vector Outgoing Asymptote as the Coordinate Type, the elements to be specified are the same as those for the Target Vector Incoming Asymptote type, except that Right Ascension and Declination are defined in terms of the outgoing rather than the incoming asymptote.

Example

Astrogator */Satellite/Satellite1 SetValue MainSequence.SegmentList.Initial_State.InitialState.Target_Vector_Outgoing_Asymptote.rp 10000 km

STK Programming Interface 11.0.1