TWingInstantaneousCalculationData |
The TWingInstantaneousCalculationData contains information about the instantaneous state of a wing. This information is available for wing angle external functions.
typedef struct {
} TWingInstantaneousCalculationData;
Specifies the size, in bytes, of this data structure.
The global axes X,Y,Z coordinates of the position of the wing origin relative to the global origin.
A matrix containing the orientation of the wing, relative to global axes. The matrix is in row-major order, so the first 3 elements are the first row, the next 3 the second row and the last 3 the third row. These rows contain the global axes components of the unit vectors in the wing local x-, y- and z-axes directions: the first 3 elements of the matrix (first row) are the global axes components of the wing local x-direction, the next 3 elements (second row) are the global axes components of the wing local y-direction, and the last 3 (third row) are the global axes components of the wing local z-direction.
The X,Y,Z components in the global axes directions, of the velocity of the wing origin relative to global.
The x,y,z components in the wing axes directions, of the angular velocity of the wing relative to global.
Note: | This vector is given in wing axes components, not global axes components. |