“…The UAV with the world coordinate systems can be transformed into the proposed model [
27] as
where Δ X and Δ Y define the x and y ‐axis random displacement, which is caused by the UAV linear oscillation, where the fixed coordinate system can be defined as x ′ y ′ z ′. By substituting the values of the roll angle, pitch angle, and yaw angle, which are mentioned in Equations (), (), and (), Equation () is derived from these equations, which is the transformation matrix of Equation ().…”