here's my question:
I have position and velocity vectors of a body in the inertial frame. Now i need to switch the reference system to body frame.
So i have
$\bar{x}_b = \hat{R}\bar{x}_I$
where
$\hat{R}=\hat{R}( \phi(t),\theta(t),\psi(t)) = \left[ \begin{matrix}\cos{(\theta)}\cos{(\psi)} & \cos{(\theta)}\sin{(\psi)} & -\sin{(\theta)}\\ \sin{(\phi)}\sin{(\theta)}\cos{(\psi)}-\cos{(\phi)}\sin{(\psi)} & \sin{(\phi)}\sin{(\theta)}\sin{(\psi)}+\cos{(\phi)}\cos{(\psi)} & \sin(\phi)\cos(\theta) \\ \cos{(\phi)}\sin{(\theta)}\cos{(\psi)}+\sin{(\phi)}\cos{(\psi)} & \sin{(\phi)}\sin{(\theta)}\sin{(\psi)}-\sin{(\phi)}\cos{(\psi)} & \cos(\phi)\sin(\theta) \end{matrix} \right]$
so now I should do:
$$\bar{v}_b = \dot{\bar{x}}_b = \frac{\partial{\hat{R}}}{\partial{t}}\cdot \bar{x}_I +\hat{R} \cdot\frac{\partial{\bar{x}_I}}{\partial{t}} $$
Is this correct? My doubt is about rotational matrix, should it be derived? Or am i missing something?
Thanks in advance!
I can say quite surely that the right answer is that:
$$ V_\text{b} = \hat{R}_{\text{i} \rightarrow \text{b}} \cdot V_\text{i}$$
where $V_\text{b}$ is $\dot{x}_\text{b}$ (velocity in body frame) and $V_\text{i}$ the velocity in inertial frame.