constraintSettings Element |
constraintSettingsType
Namespace: Empty
Schema: Empty
Name | Occurrences | Description |
---|---|---|
All | ||
acceleration | [0, 1] | Rate of velocity within the segment |
altitude | [0, 1] | Constant altitude for the segment. |
CAS | [0, 1] | Calibrated airspeed within the segment |
climbAngle | [0, 1] | Climb angle within the segment |
deltaTemperatureISA | [0, 1] | Delta in temperature compared to standard ISA conditions |
descentAngle | [0, 1] | Descent angle within the segment |
loadFactor | [0, 1] | Load factor experienced during segment |
machNumber | [0, 1] | Mach number within the segment |
prioritySetting | [0, 1] | priority setting indicating which constraint is preferred within the segment |
rateOfClimb | [0, 1] | Climb angle within the segment |
rateOfDescent | [0, 1] | Rate of descent within the segment |
rateOfTurn | [0, 1] | Rate of turn within the segment |
stepClimbAltitudeDifference | [0, 1] | Altitude difference of each step climb. |
stepClimbSpecificExcessPower | [0, 1] | Specific excess power within the segment (e.g.: for defining minimum SEP to remain after step climbs have been performed). |
thrustSetting | [0, 1] | Thrust setting for derated engine as fraction of max. Thrust (e.g.: for powered descents, deceleration not at IDLE, manoevres). |
Name | Type | Required | Description |
---|---|---|---|
externalDataDirectory | string | ||
externalDataNodePath | string | ||
externalFileName | string |