constraintSettings Element

constraintSettingsType

Namespace: Empty

Schema: Empty

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

Rate of velocity within the segment

      Element altitude[0, 1]

Constant altitude for the segment.

      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 loadFactor[0, 1]

Load factor experienced during segment

      Element machNumber[0, 1]

Mach number within the segment

      Element prioritySetting[0, 1]

priority setting indicating which constraint is preferred 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 stepClimbAltitudeDifference[0, 1]

Altitude difference of each step climb.

      Element stepClimbSpecificExcessPower[0, 1]

Specific excess power within the segment (e.g.: for defining minimum SEP to remain after step climbs have been performed).

      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 segment
See Also