I am trying to go from body-referenced aircraft velocities u, v, w, to angle of attack a, sideslip b, and total speed V. This is a standard problem for beginning aeronautics, I'm just wondering the best was to solve it with maple. Spefically, I would like to use the following relations to get short expressions for the derivatives of u, v, and w.
Given that
u = V * cos(a) * cos(b)
v = V*sin(b)
w = V*sin(a)*cos(b)
and all variables above...