| thrustSetting Element |
Thrust setting for derated engine as fraction of max. Thrust (e.g.: for powered descents, deceleration not at IDLE, manoevres). If a vector is provided, a constraint profile is defined with respect to the <referenceEndCondition> using the <endConditionRatio> vector.
Namespace: Empty
Schema: Empty
Type
Content Type| Item | Facet Value | Description |
|---|---|---|
 string | ||
 Pattern | ((\s+)?[-+]?(\d+)?(\.)?(\d+)?(([eE][-+]?)?\d+)?(\s+)?|(\s+)?(NaN)(\s+)?)(;(((\s+)?[-+]?(\d+)?(\.)?(\d+)?(([eE][-+]?)?\d+)?(\s+)?)|(\s+)?(NaN)(\s+)?))* |
Parents
Attributes| Name | Type | Required | Description |
|---|---|---|---|
 a |  string | ||
| b | string | ||
| c | string | ||
| delta | string | ||
| externalDataDirectory | string | ||
| externalDataNodePath | string | ||
| externalFileName | string | ||
| mapType | string | ||
| mu | string | ||
| relationalOperator | string | Yes | |
| uncertaintyFunctionName | uncertaintyFunctionType | ||
| v | string | ||
| w | string |
See Also