Return information about VectorTool components.
VectorTool_R <ScenarioPath> {Option} [<Parameters>]
The VectorTool_R command can be used to return information about VectorTool components.
{Option} | <Parameters> | Description |
---|---|---|
Exists | [Template] "<ComponentSpec>" | Returns a 1 if the specified "<ComponentSpec>" exists, otherwise 0 will be returned. Use the Template keyword if the component is a template. |
Details | [Template] "<ComponentSpec>" [IncludeDescriptions] | Returns information about the component
in a single string with newline characters. Use the Template
keyword if the component is a template.
With the IncludeDescriptions keyword the component type description and user description, if available, will also be returned. Use the VectorTool_RM command to return information in a list of strings. |
Status | "<ComponentSpec>" | Returns one of these strings
The Status option is not valid for a template. |
ConvertSystem | "<FromSystemSpec>" "<ToSystemSpec>" {TimeInstant} <x> <y> <z> [<xv> <yv> <zv>] | Convert a position/velocity from one system to another at the specified time instant. <x>, <y>, and <z> values are entered in Connect distance units. <xv>, <yv>, and <zv> values are optional and if entered are in Connect distance units / second. |
ConvertAxes | "<FromAxesSpec>" "<ToAxesSpec>" {TimeInstant} <x> <y> <z> [<xv> <yv> <zv>] | Convert a position/velocity from one axes to another at the specified time instant. <x>, <y>, and <z> values are entered in Connect distance units. <xv>, <yv>, and <zv> values are optional and if entered are in Connect distance units / second. |
For information on "<ComponentSpec>" formats see Component Specification.
For valid {TimeInstant} values see Time Options.
Determine if the specified Axes exists:
VectorTool_R * Exists "Satellite/Satellite1 J2000 Axes"
Determine if the specified template Axes exists:
VectorTool_R * Exists Template "Satellite Body Axes"
Return information about the specified Position Vector:
VectorTool_R * Details "Satellite/ESP Position Vector"
Vector Type: Displacement
Vector Name: Position
Vector Parent: ESP
Origin Point: Earth Center
Destination Point: ESP Center
Apparent: False
Convert the specified Position from Earth Inertial System to Earth Fixed System:
VECTORTOOL_R * ConvertSystem "CentralBody/Earth Inertial" "CentralBody/Earth Fixed" "29 Sep 2013 16:00:00.000" -4844418.113 632169.241 4086605.212
1216469.934078 -4736121.718381 4081386.888024
Convert the specified Position and Velocity from Satellite Body Axes to Satellite LVLH:
VectorTool_R * ConvertAxes "Satellite/Satellite1 Body" "Satellite/Satellite1 LVLH" "5 Apr 2013 16:02:00.000" 2429147.990 -6402503.478 644947.940 4410.004618 2210.635488 5335.388073
-701493.175561 2378921.472598 6415404.004448 2639.445311 572.556440 76.298556
This command belongs to the following group(s):
10.1
STK Programming Interface 11.0.1