controlSurfacePerformanceMapOldType

complexType · extension complexBaseType · sequence

Control surface performance map (legacy)

Delta performance map with aerodynamic data for a control surface. Array order is: relativeDeflection min->max then angleOfAttack then angleOfSideslip then altitude then machNumber. AngleOfAttack, angleOfSideslip, altitude and machNumber are taken from the basic performance map one level above.

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.
controlSurfaceUIDstringUIDBaseType[1..1] requiredReference to the control surface
relDeflectionstringVectorBaseType[1..1] requiredRelative deflection
dcdstringArrayBaseType[0..1] optionalIncrement of the drag coefficient due to the control surface deflection
dcsstringArrayBaseType[0..1] optionalIncrement of the side force coefficient due to the control surface deflection
dclstringArrayBaseType[0..1] optionalIncrement of the lift coefficient due to the control surface deflection
dcmdstringArrayBaseType[0..1] optionalIncrement of the moment coefficient around the d-axis due to the control surface deflection
dcmsstringArrayBaseType[0..1] optionalIncrement of the moment coefficient around the s-axis due to the control surface deflection
dcmlstringArrayBaseType[0..1] optionalIncrement of the moment coefficient around the l-axis due to the control surface deflection

Used by

In a dataset · 1 path

In the schema · 1 declaration

TypeName
controlSurfacePerformanceMapsOldTypecontrolSurface