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constraints Element

Constraints

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
Attribute externalDataNodePathSimple Type string
Attribute externalFileNameSimple Type string
Remarks
Constraint settings for the point performance definition
See Also