ESDU 67004 relates the vector components@ stability derivatives@ and inertia parameters in one set of axes to those in another. The axis systems in normal use in flight dynamics are Cartesian body axes with their xz-plane in the plane of symmetry of the aircraft. For this reason ESDU 67004 is restricted to translations of the origin in the xz-plane and rotation about the y-axis.
ESDU 67004 A-2004 history
2004ESDU 67004 A-2004 Conversion formulae for rotation and translation of body axes.