missionSegmentEndConditionType

complexType · extension complexBaseType · sequence

End condition

Specifies the end conditions for a segment or segment block (e.g.: an altitude or velocity). If a phase has no endCondition, it will base its endCondition on the segmentBlock settings (e.g.: it is the cruise segment, retrieving its total length based on the length of the segmentBlock minus all other segment lengths available within the segmentBlock).

Attributes

NameTypeConstraintsUseDefaultDescription
@externalDataDirectoryxsd:stringoptionalDirectory of the external data file
@externalDataNodePathxsd:stringoptionalPath of the node inside the external data file
@externalFileNamexsd:stringoptionalName of the external data file

Child elements

NameTypeConstraintsOccurrenceHow often the element may appear at this place. The schema writes it as minOccurs and maxOccurs on the declaration.DefaultDescription
sequenceThe children below must appear in exactly this order. Each may repeat as often as its own occurrence allows.
choiceExactly one of the alternatives below may appear, unless the occurrence next to this line says otherwise.· [0..1] optional
calibratedAirSpeeddoubleConstraintBaseType[1..1] requiredCalibrated air speed at the end of the segment
machNumberdoubleConstraintBaseType[1..1] requiredMach number at the end of the segment
choiceExactly one of the alternatives below may appear, unless the occurrence next to this line says otherwise.· [0..1] optional
positionXYZpointConstraintType[1..1] requiredPosition at the end of the segment in xyz coordinates
positionGeogeographicPointConstraintType[1..1] requiredPosition at the end of the segment in geo coordinates
runwaymissionEndRunwayType[1..1] requiredRunway reached at the end of the segment
choiceExactly one of the alternatives below may appear, unless the occurrence next to this line says otherwise.· [0..1] optional
massFractiondoubleConstraintBaseType[1..1] requiredMass fraction at the end of the segment
fuelFractiondoubleConstraintBaseType[1..1] requiredFuel fraction at the end of the segment
fuelRemainingdoubleConstraintBaseType[1..1] requiredFuel remaining at the end of the segment
fuelConsumeddoubleConstraintBaseType[1..1] requiredFuel consumed
powerFractiondoubleConstraintBaseType[1..1] requiredPower fraction at the end of the segment
powerRemainingdoubleConstraintBaseType[1..1] requiredStored energy remaining at the end of the segment
powerConsumeddoubleConstraintBaseType[1..1] requiredStored energy consumed
choiceExactly one of the alternatives below may appear, unless the occurrence next to this line says otherwise.· [0..1] optional
headingdoubleConstraintBaseType[1..1] requiredHeading at the end of the segment
turnAngledoubleConstraintBaseType[1..1] requiredTurn angle covered
rangedoubleConstraintBaseType[0..1] optionalRange covered
choiceExactly one of the alternatives below may appear, unless the occurrence next to this line says otherwise.
durationtimeConstraintBaseType[0..1] optionalDuration
endTimeUTCtimeConstraintBaseType[0..1] optionalUTC time at the end of the segment
specificExcessPowerdoubleConstraintBaseType[0..1] optionalSpecific excess power at the end of the segment
rateOfClimbdoubleConstraintBaseType[0..1] optionalRate of climb at the end of the segment
flightPathAngledoubleConstraintBaseType[0..1] optionalFlight path angle at the end of the segment
releasedStoresreleasedStoresType[0..1] optionalList of stores released in the segment. The corresponding weightAndBalance vector for retrieving the new state as well as a potential change in aerodynamicPerformanceMap (if external stores are released) should be reflected within the configuration node at model level.

Used by

In a dataset · 2 paths

In the schema · 2 declarations

TypeName
missionSegmentBlockConstraintsTypeendCondition
missionSegmentTypeendCondition