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constraints Element

Constraints applying to the point performance

Namespace: Empty

Schema: Empty

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

Rate of velocity [m/s^2]

      Element altitude[0, 1]

Constant altitude [m]

      Element angleOfAttack[0, 1]

Angle of attack [deg]

      Element calibratedAirSpeed[0, 1]

Calibrated airspeed [m/s]

      Element climbAngle[0, 1]

Climb angle [deg]

      Element duration[0, 1]

Duration [s]

      Element machNumber[0, 1]

Mach number [-]

      Element rateOfClimb[0, 1]

Rate of climb [m/s]

      Element rateOfTurn[0, 1]

Rate of turn [deg/s]

      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

Directory of the external data file

Attribute externalDataNodePathSimple Type string

Path of the node inside the external data file

Attribute externalFileNameSimple Type string

Name of the external data file

See Also