GroundVehicle: Astrogator Values: Target Vector
Data for incoming and outgoing asymptotes as well as C3 energy.
| Name |
Dimension |
Type |
Description |
| Time |
DateFormat |
Real Number |
Time. |
| C3_Energy |
Rate Squared |
Real Number |
An energy defined as -(mu/semi-major-axis). The
Calc Object allows a choice of a central body. The default is Earth.
|
| Incoming_Asymptote_Dec |
AngleUnit |
Real Number |
Declination of incoming asymptote or apsides. The
Calc Object allows a choice of coordinate systems. The default is Earth Centered Inertial.
|
| Incoming_Asymptote_RA |
AngleUnit |
Real Number |
Right Ascension of incoming asymptote or apsides. The
Calc Object allows a choice of coordinate systems. The default is Earth Centered Inertial.
|
| Incoming_Vel_Az_at_Periapsis |
AngleUnit |
Real Number |
Velocity azimuth at periapsis for incoming trajectory. The
Calc Object allows a choice of coordinate systems. The default is Earth Centered Inertial.
|
| Outgoing_Asymptote_Dec |
AngleUnit |
Real Number |
Declination of outgoing asymptote or apsides. The
Calc Object allows a choice of coordinate systems. The default is Earth Centered Inertial.
|
| Outgoing_Asymptote_RA |
AngleUnit |
Real Number |
Right Ascension of outgoing asymptote or apsides. The
Calc Object allows a choice of coordinate systems. The default is Earth Centered Inertial.
|
| Outgoing_Vel_Az_at_Periapsis |
AngleUnit |
Real Number |
Velocity azimuth at periapsis for outgoing trajectory. The
Calc Object allows a choice of coordinate systems. The default is Earth Centered Inertial.
|
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