constraintSettings Element

constraintSettingsPointPerformanceType

Namespace: Empty

Schema: Empty

Type
Parents
Children
NameOccurrencesDescription
All All
      Element acceleration[0, 1]

Rate of velocity within the segment

      Element angleOfAttack[0, 1]

Angle of attack [for pointPerformance constraints]

      Element CAS[0, 1]

Calibrated airspeed within the segment

      Element climbAngle[0, 1]

Climb angle within the segment

      Element deltaTemperatureISA[0, 1]

Delta in temperature compared to standard ISA conditions

      Element descentAngle[0, 1]

Descent angle within the segment

      Element duration[0, 1]

Duration of the condition. [for pointPerformance constraints]

      Element loadFactor[0, 1]

Load factor experienced during segment

      Element machNumber[0, 1]

Mach number within the segment

      Element rateOfClimb[0, 1]

Climb angle within the segment

      Element rateOfDescent[0, 1]

Rate of descent within the segment

      Element rateOfTurn[0, 1]

Rate of turn within the segment

      Element thrustSetting[0, 1]

Thrust setting for derated engine as fraction of max. Thrust (e.g.: for powered descents, deceleration not at IDLE, manoevres).

Attributes
NameTypeRequiredDescription
Attribute externalDataDirectorySimple Type string
Attribute externalDataNodePathSimple Type string
Attribute externalFileNameSimple Type string
Remarks
specific performance settings for the point performance
See Also