Rewriting Central Force Problem of Black Hole Potential

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SUMMARY

The discussion focuses on deriving a second-order differential equation for the function \( u(\phi) \) that describes the motion of an object orbiting a non-rotating black hole, based on the radial equation from General Relativity. The equation is transformed using the substitution \( u = \frac{1}{r} \) and involves angular momentum \( l \) and potential \( V_o = GM_o \). The final form of the equation is \( u'' + u - \frac{V_o}{l^2} - 3V_ou^2 = 0 \), demonstrating the relationship between radial and angular motion in the context of black hole physics.

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  • Understanding of General Relativity concepts
  • Familiarity with differential equations
  • Knowledge of orbital dynamics and angular momentum
  • Proficiency in mathematical substitutions and transformations
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  • Study the derivation of the effective potential in General Relativity
  • Learn about the Schwarzschild metric and its implications for black hole orbits
  • Explore the mathematical techniques for solving second-order differential equations
  • Investigate the physical significance of the parameters \( V_o \) and \( l \) in orbital mechanics
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Students and researchers in theoretical physics, particularly those focusing on General Relativity, black hole dynamics, and orbital mechanics. This discussion is beneficial for anyone looking to deepen their understanding of the mathematical framework governing black hole orbits.

Digital Honeycomb
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Homework Statement


From the homework:
In General Relativity it is found that the radial equation of an object orbiting a non-rotating black hole has the form $$\dot r^2 + (1 - 2 \frac {V_o} {r} ) (\frac {l^2} {r^2} + 1) = E^2$$ where ##r## is the radial coordinate, ##l## is the angular momentum, and ##E## is the total energy; the potential ##V_o = GM_o##, where ##M_o## is the mass of the black hole. Show, using the standard substitution ##u = \frac {1} {r}##, and rewriting ##\dot r## in terms of ##\dot \phi## and ##u' = \frac {du} {d\phi}##, that we can write a differential equation for ##u(\phi)## of form $$u'' + u - \frac {V_o} {l^2} - 3V_ou^2 = E^2$$​

Homework Equations


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The Attempt at a Solution


First off I'm not entirely sure how to rewrite ##\dot r## in terms of ##\dot \phi##. In the notes it is described that the angular momentum ##l = mr^2\dot\phi##, so therefore this equation could be written in the form $$\dot r = \sqrt{E^2 - (1 - 2V_o u)(m\dot\phi +1)}$$ but it is not exactly like I can plug this back into the original equation. I can also try taking that since ##u = \frac {1} {r}##, that ##\frac {du} {dt} = \frac {-1} {r^2} \frac {dr} {dt} = \frac {du} {d\phi} \frac {d\phi} {dt}## and so ##\dot r = \frac {-1} {u^2} u' \dot \phi## but putting this into the first equation, I'm not exactly sure where the ##u''## is supposed to come from. Am I coming at this from the wrong direction entirely? Thank you!
 
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I'm not sure about the motivation for going from the equation in terms of \dot{r} to the second-order equation in terms of u, but here's how it could be done:

First take a time derivative of your equation for \dot{r}. The right side of the equation is a constant, so that gives:

2 \dot{r} \ddot{r} - F(r) \dot{r} = 0

where - F(r) is the derivative of that potential-like expression on the left side. Dividing through by \dot{r} and rearranging gives you a second-order equation for r:

\ddot{r} = \frac{1}{2} F(r)

Now, at this point, you can use a trick from nonrelativistic orbital dynamics. You do a simultaneous change of dependent variable from r to u = \frac{1}{r} and a change of independent variable from t to \phi.
 
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Hmm, okay... so doing that I end up with the equation, $$\ddot r = \frac {l^2} {r ^3} - 3 \frac {V_o l^2} {r^4} - 2 \frac {V_0} {r^2},$$ substituting ##u = \frac {1} {r}## is simple enough for the RHS of the equation, but not for understanding exactly how to change ##\ddot r## into an equation of ##u(t)##. I know that ##\frac {d^2u} {dr^2} = \frac {2} {r^3}##, but I'm afraid I don't understand how to turn this into an equation in respect to time. I suppose I can take that ##\dot u = \frac {-1} {r^2} \dot r## and then ##\ddot u = \frac {2} {r^3} \dot r - \frac {1}{r^2}\ddot r##, but beyond that I'm not sure how to turn this purely into some ##u(t)## (beyond that, I realize I can take ##d\phi = \frac {L}{m}u^2 dt##, however).
 
As I said, you have to simultaneously change r to u and t to \phi.

\frac{dr}{dt} = \frac{dr}{du} \frac{du}{d\phi} \frac{d\phi}{dt}

\frac{dr}{du} = -\frac{1}{u^2}
\frac{d\phi}{dt} = \frac{\mathcal{l}}{mr^2} = \frac{\mathcal{l}}{m} u^2

So \frac{dr}{dt} = -\frac{\mathcal{l}}{m} \frac{du}{d\phi}

Then operate again by \frac{d}{dt} = \frac{d\phi}{dt} \frac{d}{d\phi} to get:

So \frac{d^2 r}{dt^2} = -(\frac{\mathcal{l}}{m})^2 u^2 \frac{d^2 u}{d\phi^2}
 
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Oh! That makes sense! And then plugging that into the equation gives $$- \frac {l^2} {m^2}u^2 u'' = l^2 u^3 - 3V_o l^2 u^4 - V_o u^2$$ and that turns into $$u'' + u - \frac {V_o} {l^2} - 3V_o u^2 = 0$$ if you take ##m = 1##! Thank you so much!
 

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