| endCondition Element |
Condition terminating the segment
Namespace: Empty
Schema: Empty
| Name | Occurrences | Description |
|---|---|---|
| | [0, 1] | |
| | Calibrated air speed at the end of the segment | |
| | Mach number at the end of the segment | |
| | [0, 1] | |
| | Position at the end of the segment in geo coordinates | |
| | Position at the end of the segment in xyz coordinates | |
| | Runway reached at the end of the segment | |
| | [0, 1] | |
| | Fuel consumed | |
| | Fuel fraction at the end of the segment | |
| | Fuel remaining at the end of the segment | |
| | Mass fraction at the end of the segment | |
| | Stored energy consumed | |
| | Power fraction at the end of the segment | |
| | Stored energy remaining at the end of the segment | |
| | [0, 1] | |
| | Heading at the end of the segment | |
| | Turn angle covered | |
| | [0, 1] | Range covered |
| | ||
| | [0, 1] | Duration |
| | [0, 1] | UTC time at the end of the segment |
| | [0, 1] | Specific excess power at the end of the segment |
| | [0, 1] | Rate of climb at the end of the segment |
| | [0, 1] | Flight path angle at the end of the segment |
| | [0, 1] | List of stores released in the segment. The corresponding weightAndBalance vector for retrieving the new state as well as a potential change in aerodynamicPerformanceMap (if external stores are released) should be reflected within the configuration node at model level. |
| Name | Type | Required | Description |
|---|---|---|---|
Directory of the external data file | |||
Path of the node inside the external data file | |||
Name of the external data file |