| flightLoadCase Element |
flightLoadCaseType
Namespace: Empty
Schema: Empty
Type
ParentsChildren| Name | Occurrences | Description |
|---|---|---|
 All | ||
 aeroDataSetUID | [0, 1] | stringUIDBaseType |
| aircraftSettings | [0, 1] | loadCaseSettingsType |
| cutLoads | [0, 1] | cutLoadsType |
| description | [0, 1] | Load case description (String) |
| externalAmifFile | [0, 1] | stringBaseType |
| loadCondition | [0, 1] | flightLoadCaseType |
| mass | [0, 1] | loadCaseMassType |
| name | Load case name | |
| nodalLoads | [0, 1] | nodalLoadsType |
| state | loadCaseStateType |
Attributes| Name | Type | Required | Description |
|---|---|---|---|
 externalDataDirectory |  string | ||
| externalDataNodePath | string | ||
| externalFileName | string | ||
| uID | ID | Yes |
RemarksMain class
State
Includes general definition of aircraft attitude and the aircraft environment.
Aircraft Settings
Include definition of settings of the aircraft self. For example setting of a flap or landinggear.
MassCase
Include definition about the massCase and is linked by an UID to the massBreakdown, weightAndBalance or direct component link. ?!
References
Coordinate System(s)
- Earth Fix coord.sys. (EF) with planar surface (x-y-Ebene = Earth surface, x North, y East)
- refCoordUid (e.g. body fix and orientation to EF)
- refpointUid
Euler angles
- Attitude of body fix to earth fix coord.sys.
- ψ psi – heading
- θ theta – pitch angle
- Φ phi – bank angle
- Rotation order: ψ, θ, Φ
Reference of attitude values
- x,y,z (vector to ref point in EF)
- dx,dy,dz (vector in EF)
- u,v,w (vector in refCoord) (body fix)
- du,dv,dw (vector in refCoordUid) (body fix)
(dx,dy,dy --> Euler transformation (psi, theta, phi) --> u,v,w)
See Also