aeroMapType

Aerodynamic coefficients and derivatives of the aircraft for one set of boundary conditions. The atmospheric model and the configuration the map is valid for are given in <boundaryConditions>, the coefficients over altitude, Mach number, sideslip angle and angle of attack in <aeroPerformanceMap>, and the permitted range of the angle of attack, optionally, in <aeroLimitsMap>.

The configuration can set several control devices at the same time. Their settings are then superposed by summing them up, in the order described in section 9 of cpacsType.

Attributes

Name	Type	Use	Description
`@externalDataDirectory`	`xsd:string`	optional	Directory of the external file the element was read from, as URI
`@externalDataNodePath`	`xsd:string`	optional	Path of the parent element in the merged dataset, at which the element was inserted from an external file
`@externalFileName`	`xsd:string`	optional	Name of the external file the element was read from
`@uID`	`xsd:ID`	optional	UID

Child elements

Name	Type	OccurrenceHow often the element may appear at this place. The schema writes it as minOccurs and maxOccurs on the declaration.	Description
allThe children below may appear in any order. Each may appear at most once.
`name`	`stringBaseType`	[1..1] required	Name
`description`	`stringBaseType`	[0..1] optional	Description
`boundaryConditions`	`aeroPerformanceBoundaryConditionsType`	[1..1] required	Boundary conditions the aerodynamic map is valid for
`aeroPerformanceMap`	`aeroPerformanceMapType`	[1..1] required	Aerodynamic coefficients and derivatives
`aeroLimitsMap`	`aeroLimitsMapType`	[0..1] optional	Aerodynamic limitations

aeroMapType

Attributes

Child elements

Used by

In a dataset · 2 paths

In the schema · 1 declaration