Set vehicle temperature parameters.
SEET <VehiclePath> VehTemperature {TempOptions}
This command is valid for Satellite, Missile & Launch Vehicle.
| {TempOptions} | Description |
|---|---|
| EarthAlbedo <Value> | A measure of the reflectance of sunlight from the Earth's surface. <Value> should be between 0.0 and 1.0. |
| MaterialEmissivity <Value> | A measure of the IR emission of the spacecraft. <Value> should be between 0.0 and 1.0. |
| MaterialAbsorptivity <Value> | A measure of the absorptivity of the spacecraft. <Value> should be between 0.0 and 1.0. |
| Dissipation <Value> | Value (in Watts) of internal heat consumption of the spacecraft. <Value> should be between 0.0 and 1.0e9 watts. |
| CrossSectionalArea <Value> | Cross sectional area (in m^2) of the spacecraft. For the spherical model, pi*r^2; for the plate model, the area of the plate. |
| ShapeModel {Sphere | Plate} | Specify the type of thermal model for the spacecraft. |
| NormalVector "<TruncObjPath> <VectorName>" | Specify the VGT vector that defines the normal direction to the plate when using the plate model. |
To set the vehicle temperature parameters:
SEET */Satellite/Satellite1 VehTemperature MaterialEmissivity 0.5 ShapeModel Plate NormalVector "Satellite/Satellite1 Sun"
If activated, Connect returns an acknowledgement message.
This command belongs to the following group(s):
9.1
STK Programming Interface 11.0.1