case3 Element

Main element with specific settings for the determination of the take-off decision speed V1.

Namespace: Empty

Schema: Empty

Type
Parents
Children
NameOccurrencesDescription
Sequence Sequence
      Element maxTORunway

Maximum runway length. [m]

      Element vIASEngFail

Vector with different speeds VIAS in increas-ing order determining the speed of one engine failure. The vector determines the speed range where the assumed V1 is locat-ed. [m/s]

      Element vNGLimit

Maximum ground speed where nose gear steering is allowed. [m/s]

      Element maxBrake

Maximum brake efficiency: 1 = 100percent brake efficiency 0 = 0percent brake efficiency

      Element ctrl

Main element containing the setting for the PID controllers imitating the pilot inputs during the take-off run.

Attributes
NameTypeRequiredDescription
Attribute externalDataDirectorySimple Type string
Attribute externalDataNodePathSimple Type string
Attribute externalFileNameSimple Type string
See Also