Target_Vector_Outgoing_Asymptote

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

Syntax

Astrogator_RM <Satellite Object Path> GetValue <Astrogator Object Path>.Target_Vector_Outgoing_Asymptote.{Element}

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

Initial State Segment

Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Initial_State.InitialState.Target_Vector_Outgoing_Asymptote

Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Initial_State.InitialState.Target_Vector_Outgoing_Asymptote.rp

Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Initial_State.FinalState.Target_Vector_Outgoing_Asymptote

Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Initial_State.FinalState.Target_Vector_Outgoing_Asymptote.rp

Hold Segment

Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Hold.InitialState.Target_Vector_Outgoing_Asymptote

Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Hold.InitialState.Target_Vector_Outgoing_Asymptote.rp

Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Hold.FinalState.Target_Vector_Outgoing_Asymptote

Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Hold.FinalState.Target_Vector_Outgoing_Asymptote.rp

Maneuver Segment

Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Maneuver.InitialState.Target_Vector_Outgoing_Asymptote

Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Maneuver.InitialState.Target_Vector_Outgoing_Asymptote.rp

Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Maneuver.FinalState.Target_Vector_Outgoing_Asymptote

Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Maneuver.FinalState.Target_Vector_Outgoing_Asymptote.rp

STK Programming Interface 11.0.1