The 6DoF ECEF (Quaternion) dialog accepts the Initial Euler Orientation as a parameter. The documentaion for this block does not mention whether these Initial Euler angles are associated with the Direct Cosine Matrix that represents a coordinate transformation of a vector in Earth axes into a vector in body axes, or whether it represents a coordinate transformation of a vector in inertial axes into a vector in body axes.
MATLAB: Does the documentation for the 6DoF ECEF (Quaternion) block in the Aerospace Blockset 2.0.1(R14SP3) not mention about how the Initial Euler angles are to be specified
6dofaerospaceAerospace Blocksetangleeulerinitialquaternion
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