Time average of potential energy in Keplerian orbit

AI Thread Summary
The discussion focuses on calculating the time average of potential energy in a two-body Keplerian orbit, specifically showing that this average equals the instantaneous potential energy when the bodies are separated by the semi-major axis. The user attempts to derive the average potential energy using the formula for gravitational potential energy and the definition of time average, but encounters an issue with an extra factor of (1-e^2) in the denominator. Suggestions include correcting the conversion of period P and utilizing conservation of angular momentum to properly evaluate the integral. The user is encouraged to substitute for dt using angular momentum, but remains confused about correctly expressing the period in terms of angular measure. The conversation emphasizes the need for clarity in integrating over the orbital path.
acr
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Hello,

I'm trying to show that the time average of the potential energy of a 2-body system is equal to the instantaneous potential energy of that system when the two bodies are separated by a distance equal to the semi-major axis, a.

So I know that

U = \frac{-Gm_{1}m_{2}}{r}

and the time average of a function f(t) over a time interval \tau is defined to be

<f(t)>=\frac{1}{\tau}\int_0^{\tau} f(t) dt

and

r = \frac{a(1-e^{2})}{1+ecos \theta}

Can anyone tell me what's wrong with my attempt? Here it is:

&lt;U&gt;=\frac{1}{P} \int_0^P \frac{-Gm_1m_2}{r} dt = \frac{-Gm_{1}m_{2}}{2\pi a(1-e^2)}\int_0^{2\pi}(1+ecos\theta) d\theta<br /> =\frac{-Gm_1m_2}{a(1-e^2)}<br />,

but I'm supposed to be verifying that

&lt;U&gt;=\frac{-Gm_1m_2}{a}

I can't seem to figure out how to get rid of that factor of (1-e^2) in the denominator. I suppose this can be simplified by just asking why/how

&lt;\frac{1}{r}&gt;=\frac{1}{a}

and not

\frac{1}{a(1-e^2)}}

Thank you for your time
 
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Welcome to PF!

Hello acr! Welcome to PF! :smile:

(nice LaTeX, btw :biggrin:)
acr said:
Can anyone tell me what's wrong with my attempt? Here it is:

&lt;U&gt;=\frac{1}{P} \int_0^P \frac{-Gm_1m_2}{r} dt = \frac{-Gm_{1}m_{2}}{2\pi a(1-e^2)}\int_0^{2\pi}(1+ecos\theta) d\theta<br /> =\frac{-Gm_1m_2}{a(1-e^2)}<br />

ah, you haven't converted 1/P properly (t = P when θ = 2π doesn't mean P = 2π, does it? :wink:), or dt.

Hint: use conservation of angular momentum. :wink:
 
Thanks tiny-tim,

I'm trying to make sense of how to incorporate the conservation of angular momentum. Would it be correct to assume that

<br /> \textbf{v} \times \textbf{r} = r^2 \frac{d\theta}{dt}=const=\frac{L}{m}<br />

is a valid statement? This would indicate that

<br /> dt=\frac{mr^2 }{L} d \theta<br />

but that doesn't seem to help much when I evaluate the new integral (or if it does, it's eluding me!)... I'm still not getting something. Any suggestions?
 
acr said:
<br /> dt=\frac{mr^2 }{L} d \theta<br />

That's right. :smile:

And now use that into the original integral, to substitute for dt. :wink:
 
Thanks again. Because r is the separation between m1 and m2, L would be m2r2 d theta/dt (choosing to let r represent the position of m2 relative to m1). When I use the result above for dt, the new integral ends up coming out as

<br /> <br /> \frac{-Gm_1 m_2^2 a (1-e^2)^{1/2}}{L}<br /> <br />

Which would indicate that I want L to be equal to

<br /> <br /> m_2 a^2 \sqrt{1-e^2} =m_2 a b<br /> <br />

I don't see how it could be, though. I am still using 2pi in place of P. I'm not sure how I should go about writing P in terms of angular measure, if this isn't correct. Any insights?

Thank you
 
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