I’m reading “Fundamentals of Astrodynamics” by Roger Bate and in the first chapter he states “in general
$ \vec{a }\cdot\dot{\vec{a}}= a\dot{a}. $
My intuition tells me that the dot product of the position and velocity of something in a circular orbit for example should in fact be zero.
Just to check it for myself I tried to prove it and got the following:
$\frac{d}{dt} (\vec{r}\cdot\vec{r})=\dot{\vec{r}}\cdot\vec{r}+\vec{r}\cdot\dot{\vec{r}}\\ \frac{d}{dt}r^{2}= 2(\vec{r}\cdot\dot{\vec{r}})\\ \vec{r }\cdot\dot{\vec{r}}= r\dot{r}$
This is the result that I don’t intuitively believe since the two vectors aren’t always parallel. Where did I go wrong with my logic?
Note that $\dot a$ is not the length of $\dot{\vec a}$, it is the time derivative of $|\vec a|$. So for instance, for an object moving at constant speed in a circular orbit, where $\vec a$ and $\dot{\vec a}$ are perpendicular, as you say, then we have $\dot a=0$.