flightLoadCase Element |
flightLoadCaseType
Namespace: Empty
Schema: Empty
Name | Occurrences | Description |
---|---|---|
Sequence | ||
name | Load case name | |
description | [0, 1] | Load case description (String) |
aeroDataSetUID | [0, 1] | stringUIDBaseType |
loadCondition | [0, 1] | flightLoadCaseType |
state | loadCaseStateType | |
aircraftSettings | [0, 1] | loadCaseSettingsType |
mass | [0, 1] | loadCaseMassType |
nodalLoads | [0, 1] | nodalLoadsType |
cutLoads | [0, 1] | cutLoadsType |
externalAmifFile | [0, 1] | stringBaseType |
Name | Type | Required | Description |
---|---|---|---|
externalDataDirectory | string | ||
externalDataNodePath | string | ||
externalFileName | string | ||
uID | string | Yes |
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. ?!
Coordinate System(s)
Euler angles
Reference of attitude values
(dx,dy,dy --> Euler transformation (psi, theta, phi) --> u,v,w)