Are Geodesics and Projectile Trajectories Equivalent in Curved Space-Time?

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SUMMARY

The discussion centers on the equivalence of geodesics and projectile trajectories in curved space-time, specifically using the Schwarzschild metric. The participants analyze the Christoffel symbols derived from the metric and their implications for the geodesic equation. They explore approximations such as σ = 1 - 2gr and the Taylor series expansion of 1/(1-x) to relate general relativity to Newtonian mechanics. The conversation emphasizes the need for a deeper understanding of weak field theory to derive classical mechanics from general relativity.

PREREQUISITES
  • Understanding of Schwarzschild metric in general relativity
  • Familiarity with Christoffel symbols and geodesic equations
  • Knowledge of Taylor series expansions and their applications
  • Basic principles of Newtonian mechanics and gravitational laws
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  • Research weak field theory in the context of general relativity
  • Study the Euler-Lagrange equation and its relationship to geodesics
  • Explore the derivation of Newton's law of gravitation from general relativity
  • Examine the implications of kinematic equations in curved space-time
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Physicists, students of general relativity, and anyone interested in the mathematical foundations of gravitational theory and its connection to classical mechanics.

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Yes, I want to make sure that geodesics of a particle moving in curved space time is the same thing of projectile trajectories.
I start from assuming that 1-\frac{2GM}{r}\approx1-2gr and then calculate the schwarzschild metric in this form
\Sigma_{\mu\nu}=\begin{bmatrix}\sigma & 0\\ 0 & -\sigma^{-1}\end{bmatrix} where \sigma = 1-2gr

and I calculated for the Christoffel symbols for this metric:
\Gamma^0_{\mu\nu}=-\sigma g\begin{bmatrix}0 & 1\\ 1 & 0\end{bmatrix}
\Gamma^1_{\mu\nu}=-\frac{g}{\sigma^2}\Sigma_{\mu\nu}

I plugged them to a geodesics equation

\partial^2_\tau x^\mu = -\Gamma^\mu_{\alpha\beta}\partial_\tau x^\alpha\partial_\tau x^\beta
where d\tau^2 = dx^\mu dx^\nu\Sigma_{\mu\nu}

and I got these ugly conditions:
\partial^2_\tau t = \sigma\partial_\tau t\partial_\tau \sigma
\partial^2_\tau \sigma = \frac{2g^2}{\sigma^2}

what I expect is just something like
x=-\frac{g}{2}t^2

I havn't finished these differential equations yet. But I want to know that I'm going through the right track, right? Any suggestion?
 
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In the level of approximation you're using, you might as well make your life easier and approximate \sigma^{-1} as 1+2gr. I would also define a new coordinate \rho=gr to avoid having to write all the factors of g.
 
I can't see why we can assume that \sigma^{-1} = 1+2gr, they're not quitely equal.(at least at the Earth's surface)

But i think i can apporximate σ to be -2gr because 1 is very small comparing with -2gr. But I still can't find a way to prove this.

Please, any can help me?
 
Black Integra said:
I can't see why we can assume that \sigma^{-1} = 1+2gr, they're not quitely equal.(at least at the Earth's surface)

It IS an approximation. The taylor series expansion of 1/(1-x) is 1+x+x^2 + o(x^3), basically. So if x is small, it's a good approximation.
 
I don't think this approach can give the Newtonian result because you are using kinematic equations. The full equation for r is

<br /> \ddot{r}=-\frac{\left( m\,{r}^{2}-4\,{m}^{2}\,r+4\,{m}^{3}\right) \,{\dot{t}}^{2}-m\,{r}^{2}\,{\dot{r}}^{2}}{{r}^{4}-2\,m\,{r}^{3}}<br />
setting \dot{t}=1 and doing a Maclaurin-Taylor expansion of the RHS in m
<br /> \ddot{r}=-\frac{\left( 1-{\dot{r}}^{2}\right) \,m}{{r}^{2}}+\frac{2\,\left(1+{\dot{r}}^{2}\right) \,{m}^{2}}{{r}^{3}}+\frac{4\,{\dot{r}}^{2}\,{m}^{3}}{{r}^{4}}+ ...<br />
assuming m << r we get
<br /> \ddot{r}=-\frac{\left( 1-{\dot{r}}^{2}\right) \,m}{{r}^{2}}<br />
which does not have a closed form solution. In this m=GM/c2.

However it is possible to deduce Newton's law of gravitation from GR by another approach.
 
Last edited:
pervect said:
It IS an approximation. The taylor series expansion of 1/(1-x) is 1+x+x^2 + o(x^3), basically. So if x is small, it's a good approximation.

That's the point. I use 1-2GM/r = 1-2gr because I calculate in case where g=9.8 and r is around the Earth's radius (not small, is it?)


Mentz114 said:
I don't think this approach can give the Newtonian result because you are using kinematic equations.
Oh. I have never heard something like this before, it's new for me. What's the name of the other way, other than kinematic equation?

Mentz114 said:
However it is possible to deduce Newton's law of gravitation from GR by another approach.
What is the other approach to deduce the classical mechanics? Mainly, I just want to find out that Euler-Lagrange Equation and Geodesics Equation are the same concept.
 
The geodesic equation is found by extremizing the action for a free particle which is
<br /> \int_{\lambda_1}^{\lambda_2}\frac{ds}{d\lambda}d \lambda = \int_{\lambda_1}^{\lambda_2}\sqrt{g_{\mu\nu}\frac{dx^\mu}{d\lambda}\frac{dx^\nu}{d\lambda}}d\lambda<br />
where s is the proper length.

Look up 'weak field theory' in the context of GR to see how Newton's law can be inferred from GR. It's too involved for me to reproduce here.
 
After some reading I found the correct procedure. From my post #5
<br /> \ddot{r}=-\frac{\left( 1-{\dot{r}}^{2}\right) \,m}{{r}^{2}}+\frac{2\,\left(1+{\dot{r}}^{2}\right ) \,{m}^{2}}{{r}^{3}}+\frac{4\,{\dot{r}}^{2}\,{m}^{3 }}{{r}^{4}}+ ...<br />
Now for static rest particle \dot{r}=0 so the leading term gives the Newtonian value.
<br /> \ddot{r}=-\frac{m}{{r}^{2}}=-\frac{GM}{{r}^{2}}<br />

A longer way is to start with
<br /> g_{\mu\nu}=\eta_{\mu\nu}+f_{\mu\nu}<br />
and
<br /> \frac{d^2 x^a}{d\tau^2}= -\Gamma^a_{bc}\frac{dx^b}{d\tau}\frac{dx^c}{d\tau}<br />
throwing away lots of stuff and setting the 4-velocities to (1,0,0,0) getting
<br /> \frac{d^2 x^a}{dt^2}= -\Gamma^a_{00}= \frac{1}{2}\eta^{ab}g_{00,b}= \frac{1}{2}\eta^{ab}f_{00,b}<br />
which works for f_{00}=2m/r
 
Last edited:
thx, that's clear :)
 

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