| aeroLimitsMap Element |
Aerodynamic limitations
Namespace: Empty
Schema: Empty
Type
ParentsChildren| Name | Occurrences | Description |
|---|---|---|
 All | ||
 altitude | Altitude [m] | |
| incrementMaps | [0, 1] | Increment maps for limitation values due to movable device deflections |
| machNumber | Mach number | |
| operationLimit | [0, 1] | Vehicle operation limit |
Attributes| Name | Type | Required | Description |
|---|---|---|---|
 externalDataDirectory |  string | ||
| externalDataNodePath | string | ||
| externalFileName | string |
RemarksThis map explicitly specifies limitations of a vehicle in terms of angles of attack and sideslip angles.
All vectors, i.e. altitude, machNumber,
angleOfSideslip and angleOfAttack, must have the
same length. To avoid redundancy with the aeroPerformanceMap, this type does not contain
any aerodynamic coefficients.
See Also