Rotating-frame derivative formula
= Rotating-frame derivative formula
If a frame rotates with <angular velocity> $\boldsymbol\Omega$ relative to an inertial frame, the derivatives of any vector $\mathbf a(t)$ satisfy
$$
\left(\frac{d\mathbf a}{dt}\right)_{\rm inertial}
=\left(\frac{d\mathbf a}{dt}\right)_{\rm rotating}
+\boldsymbol\Omega\times\mathbf a.
$$
Applying this formula twice to a <position> gives the <Coriolis acceleration>, <Euler acceleration>, and <centrifugal acceleration> terms.