I'm trying to derive the universal formulation of the time-of-flight equation that appears in the Kepler problem (following Bate Fundamentals of astrodynamics and Vallado Fundamentals of astrodynamics and applications), and I don't see a point about the hyperbolic case.
Starting from the energy equation:
$$ \dot{r}^2 = -\frac{\mu p}{r^2} + \frac{2\mu}{r} -\frac{\mu}{a} $$
after a Sundman transformation ($\dot{\chi} = \frac{\sqrt{\mu}}{r}$ ) and separating we have
$$ d\chi = \frac{dr}{\sqrt{-p + 2 r - \frac{r^2}{a}}}$$
Then both Bate and Vallado proceed and integrate assuming the elliptic case ($a > 0$), yielding
$$ \chi + c_0 = \sqrt{a} \arcsin{\frac{\frac{r}{a} - 1}{\sqrt{1 - \frac{p}{a}}}}$$
Later it is justified that this formulation is valid for elliptical, parabolic and hyperbolic orbits using the Stumpff functions, even though the integration was not performed for the case $a < 0$ ($a = 0$ is trivial). Furthermore, Vallado states "this case results in a hyperbolic sine solution, which we won't use" but after several trials I got a hyperbolic cosine solution instead:
$$ \chi + c_0 = \sqrt{-a} \cosh^{-1}{\frac{\frac{r}{-a} + 1}{\sqrt{1 - \frac{p}{a}}}}$$
I expected a sinh though, to keep simmetry with the other case.
My main question is: how come can you start from a certain case and then prove the formulation is valid for all of them? And as an aside: how would the hyperbolic derivation be?
Note: I know Battin An Introduction to the Mathematics and Methods of Astrodynamics has probably more detailed math but there's no way I can get one until the end of the holidays.
a) and then go backwards and show the formulation works for all cases, so in principle it's already tested. Thanks for linking your question but I don't think it's related to mine. – astrojuanlu Dec 30 '13 at 12:49