I Parabolic Motion from Hyperbolic Motion

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I thought this was nice. In what follows, ##c=1##.

For a particle undergoing constant proper acceleration ##\alpha## in the positive ##x##-direction, an inertial observer can use:

##x (\tau) = x_0 + \dfrac{\gamma(\tau) - \gamma_0}{\alpha}##,

where the Lorentz factor is:

##\gamma (\tau) = \cosh \phi (\tau)##

and the rapidity is:

##\phi (\tau) = \phi_0 + \alpha \tau##

(##\tau## is the particle's proper time, naught subscripts indicate values at ##\tau = 0##).

When ##\phi(\tau) \ll 1##, the Taylor series for the ##\cosh## function gives ##\cosh \phi(\tau) \approx 1 + \frac{1}{2}(\phi_0 + \alpha \tau)^2##:

##x (\tau) \approx x_0 + \dfrac{ \left[ 1 + \frac{1}{2} (\phi_0 + \alpha \tau)^2 \right] - \gamma_0}{\alpha} \\[20pt] \qquad = x_0 + \dfrac{ 1 + \frac{1}{2} \phi^2_0 - \gamma_0}{\alpha} + \phi_0 \tau + \dfrac{1}{2} \alpha \tau^2 .##

If also ##\phi_0 \ll 1##, then we can use ##\tau \approx t## (assume ##t_0=0##), ##\phi_0 \approx v_0##, ##\phi^2_0 \approx 0##, ##\gamma_0 \approx 1##, and ##\alpha \approx a##:

##x (\tau) \approx x_0 + v_0 t + \dfrac{1}{2} a t^2##.

Usually this reduction is done from a simplified version of the ##x(\tau)## function (##\phi_0 = 0##), so that the ##v_0 t## term isn't included.
 
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SiennaTheGr8 said:
##x (\tau) \approx x_0 + \dfrac{ \left[ 1 + \frac{1}{2} (\phi_0 + \alpha \tau)^2 \right] - \gamma_0}{\alpha} \\[20pt] \qquad = x_0 + \dfrac{ 1 + \frac{1}{2} \phi^2_0 - \gamma_0}{\alpha} + \phi_0 \tau + \dfrac{1}{2} \alpha \tau^2 .##

If also ##\phi_0 \ll 1##, then we can use ##\tau \approx t## (assume ##t_0=0##), ##\phi_0 \approx v_0##, ##\phi^2_0 \approx 0##, ##\gamma_0 \approx 1##, and ##\alpha \approx a##:

##x (\tau) \approx x_0 + v_0 t + \dfrac{1}{2} a t^2##.
Nice. Could you use ##\gamma_0\approx 1+\phi_0^2/2## to get directly from your penultimate expression to the final one without the extra approximations?
 
Yes, that's good. So that would give (for ##\phi(\tau) \ll 1## and ##\phi_0 \ll 1##):

##x(\tau) \approx x_0 + \phi_0 \tau + \dfrac{1}{2} \alpha \tau^2##,

though you'd still need further substitutions to "convert" to coordinate time/velocity/acceleration if you want to recover the Newtonian approximation.
 
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