Output : Différence entre versions
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| Ligne 14 : | Ligne 14 : | ||
|Unit | |Unit | ||
|- | |- | ||
| − | |DATE | + | | DATE |
| − | |Date TAI | + | | Date (TAI) |
| − | | style= | + | | style=text-align:center; | - |
| + | |- | ||
| + | | TIME | ||
| + | | Duration since initial conditions | ||
| + | | style=text-align:center; | sec | ||
| + | |- | ||
| + | | TMASS | ||
| + | | Total mass | ||
| + | | style=text-align:center; | kg | ||
| + | |- | ||
| + | | PMASS | ||
| + | | Propellant mass | ||
| + | | style=text-align:center; | kg | ||
| + | |- | ||
| + | | XIN | ||
| + | | Inertial x coordinates | ||
| + | | style=text-align:center; | m | ||
| + | |- | ||
| + | | YIN | ||
| + | | Inertial y coordinates | ||
| + | | style=text-align:center; | m | ||
| + | |- | ||
| + | | ZIN | ||
| + | | Inertial z coordinates | ||
| + | | style=text-align:center; | m | ||
| + | |- | ||
| + | | VXIN | ||
| + | | Velocity in inertial x coordinates | ||
| + | | style=text-align:center; | m/s | ||
| + | |- | ||
| + | | VYIN | ||
| + | | Velocity in inertial y coordinates | ||
| + | | style=text-align:center; | m/s | ||
| + | |- | ||
| + | | VZIN | ||
| + | | Velocity in inertial z coordinates | ||
| + | | style=text-align:center; | m/s | ||
| + | |- | ||
| + | | POSIN | ||
| + | | Position norm in inertial frame | ||
| + | | style=text-align:center; | m | ||
| + | |- | ||
| + | | VIN | ||
| + | | Velocity norm in inertial frame | ||
| + | | style=text-align:center; | m/s | ||
| + | |- | ||
| + | | XREL | ||
| + | | X component of the relative position in rotating frame | ||
| + | | style=text-align:center; | m/s | ||
| + | |- | ||
| + | | YREL | ||
| + | | Y component of the relative position in rotating frame | ||
| + | | style=text-align:center; | m/s | ||
| + | |- | ||
| + | | ZREL | ||
| + | | Z component of the relative position in rotating frame | ||
| + | | style=text-align:center; | m/s | ||
| + | |- | ||
| + | | VXREL | ||
| + | | X component of the relative velocity in rotating frame | ||
| + | | style=text-align:center; | m/s | ||
| + | |- | ||
| + | | VYREL | ||
| + | | Y component of the relative velocity in rotating frame | ||
| + | | style=text-align:center; | m/s | ||
| + | |- | ||
| + | | VZREL | ||
| + | | Z component of the relative velocity in rotating frame | ||
| + | | style=text-align:center; | m/s | ||
| + | |- | ||
| + | | VREL | ||
| + | | Relative velocity in rotating frame | ||
| + | | style=text-align:center; | m/s | ||
|- | |- | ||
| − | |||
| − | |||
| − | |||
|} | |} | ||
Version du 11 juillet 2017 à 08:08
This tab allows to the user to specify how output data will be stored with the frequency, the inertial frame used for output data (could be different of the propagation frame) as well as local frame.
But, in the same tab, the user will have access to a graphical display (only available after propagation has occurred).
| Acronym | Description | Unit |
| DATE | Date (TAI) | - |
| TIME | Duration since initial conditions | sec |
| TMASS | Total mass | kg |
| PMASS | Propellant mass | kg |
| XIN | Inertial x coordinates | m |
| YIN | Inertial y coordinates | m |
| ZIN | Inertial z coordinates | m |
| VXIN | Velocity in inertial x coordinates | m/s |
| VYIN | Velocity in inertial y coordinates | m/s |
| VZIN | Velocity in inertial z coordinates | m/s |
| POSIN | Position norm in inertial frame | m |
| VIN | Velocity norm in inertial frame | m/s |
| XREL | X component of the relative position in rotating frame | m/s |
| YREL | Y component of the relative position in rotating frame | m/s |
| ZREL | Z component of the relative position in rotating frame | m/s |
| VXREL | X component of the relative velocity in rotating frame | m/s |
| VYREL | Y component of the relative velocity in rotating frame | m/s |
| VZREL | Z component of the relative velocity in rotating frame | m/s |
| VREL | Relative velocity in rotating frame | m/s |
