I am trying to calculate the orientation of a wing, expressed as roll, pitch and yaw angle based on the three unit vectors, that form the kite reference frame. All coordinates are in ENU (East, North, Up) reference frame The orientation shall be calculated with respect to the NED (North, East, Dow…

Just as a follow up: The main problem was not yet mentioned in this discussion yet. The main problem was that the vectors of the kite reference frame are defined in in the ENU reference frame, but I need the orientation in the NED reference frame. The solution is simple: Convert the vectors of the …

[image] ufechner7: For unknown reasons the function dcm_to_angle did not work for me, I use now the following functions: What was the error?

How to calculate roll, pitch and yaw?

General Usage

Ronis_BR October 21, 2024, 4:41pm 21

What was the error?

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How to calculate roll, pitch and yaw?

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