What is the proof for Bertrand's theorem in celestial mechanics?

In summary, the conversation discusses using Lagrangian mechanics to solve for the trajectory of a particle in a central potential. The Lagrangian is written in terms of the kinetic and potential energy, and the conserved angular momentum term is used to simplify the equations. The substitution of variables and integral is used to solve for the trajectory, and the final result is given in terms of the energy and angular momentum. The conversation also mentions a specific case where the potential is a power law.
  • #1
cristianbahena
16
1
Homework Statement
I don't know how I can find the equation (2.78) and the next equations. It is from Classical Dynamics: A Contemporary Approach: Jorge V.
Relevant Equations
integral equation of energy (central problem)
Screenshot at 2019-10-06 10-13-25.png
 
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  • #2
Usually you will start from ##\mathcal{L} = \frac{1}{2}\mu v^2 - V## and then write\begin{align*}
\frac{1}{2}\mu v^2 + V &= E \\

\frac{1}{2} \mu (\dot{r}^2 + r^2\dot{\varphi}^2) + V(r) &= E
\end{align*}Also ##\varphi## doesn't appear in the Lagrangian so ##\partial \mathcal{L} / \partial \dot{\varphi} = \mu r^2 \dot{\varphi} := L## is conserved, so you can replace ##\tilde{V}(r) := \frac{1}{2} \mu r^2 \dot{\varphi}^2 + V(r) = \dfrac{L^2}{2\mu r^2} + V(r)##. Further, write ##\dot{r} = \dfrac{dr}{d\varphi} \dot{\varphi} = \dfrac{dr}{d\varphi} \dfrac{L}{\mu r^2}## so that\begin{align*}
\frac{L^2}{2\mu^2 r^4} \left( \dfrac{dr}{d\varphi} \right)^2 + \tilde{V}(r) = E
\end{align*}which is simple to invert to the integral\begin{align*}

\varphi(r) = \sqrt{\frac{L^2}{2\mu}} \int^r \frac{dr}{r^2\sqrt{E - \tilde{V}(r)}}

\end{align*}The classic substitution is now ##u=1/r##, which transforms this into\begin{align*}

\tilde{\varphi}(u) = -\sqrt{\frac{L^2}{2\mu}} \int^{u} \frac{du}{\sqrt{E - \tilde{W}(u)}}

\end{align*}Of course we can also take the integral between the minimum and maximum ##u## of the orbit, and using the scaling ##u = yu_{\mathrm{max}}## given in the image the integral becomes\begin{align*}

\Theta := \varphi(r_{\mathrm{max}}) - \varphi(r_{\mathrm{min}}) = \sqrt{\frac{L^2}{2\mu}} \int_{v_{\mathrm{min}}}^1 \frac{u_{\mathrm{max}} dy}{\sqrt{E - \tilde{U}(y)}}

\end{align*}You should notice that since ##\tilde{V}(r) = \dfrac{L^2}{2\mu r^2} + V(r)##, that ##\tilde{W}(u) = \dfrac{L^2 u^2}{2\mu } + V\left(\dfrac{1}{u} \right)##. If we let ##V(r) = \alpha r^k## then ##\tilde{W}(u) = \dfrac{L^2 u^2}{2\mu } + \alpha u^{-k}##. Finally when we substitute for ##y## we see that\begin{align*}
\tilde{U}(y) = \dfrac{L^2 y^2 u_{\mathrm{max}}^2}{2\mu } + \alpha u_{\mathrm{max}}^{-k} y^{-k} = y^2 u_{\mathrm{max}}^2 \left( \dfrac{L^2 }{2\mu } + \alpha (yu_{\mathrm{max}})^{-(k+2)}\right) = u_{\mathrm{max}}^2 \mathcal{Y}(y)
\end{align*}Furthermore ##u_{\mathrm{max}}^2 \mathcal{Y}(1) = \dfrac{L^2 u_{\mathrm{max}}^2}{2\mu} + \alpha (u_{\mathrm{max}})^{-k} = E## is just the energy evaluated at the minimum radius, hence\begin{align*}
\Theta = \sqrt{\frac{L^2}{2\mu}} \int_{v_{\mathrm{min}}}^1 \frac{dy}{\sqrt{\mathcal{Y}(1) - \mathcal{Y}(y)}}
\end{align*}Although I can't comment on the line at the very end of the proof without seeing "equation (2.77)", hope it's somewhat helpful.
 
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FAQ: What is the proof for Bertrand's theorem in celestial mechanics?

What is Bertrand's theorem in celestial mechanics?

Bertrand's theorem is a mathematical theorem that states that in a central force field, there are only two types of closed orbits - circles and ellipses. This theorem is important in celestial mechanics as it helps us understand the behavior of objects in orbit around a central body, such as planets orbiting the sun.

What is the significance of Bertrand's theorem?

Bertrand's theorem is significant because it provides insight into the stability of orbits in a central force field. It also helps us understand the conditions under which a planet or other celestial body can maintain a stable orbit around a central body.

What is the proof for Bertrand's theorem?

The proof for Bertrand's theorem involves using mathematical equations and principles, such as conservation of angular momentum and the inverse square law of gravity. It can be quite complex and involves advanced mathematical concepts, but it essentially shows that only circular and elliptical orbits are possible in a central force field.

Are there any real-world applications of Bertrand's theorem?

Yes, there are many real-world applications of Bertrand's theorem. For example, it helps us understand the stability of planetary orbits in our solar system and other planetary systems. It also has applications in satellite and spacecraft orbits, as well as in understanding the behavior of comets and other celestial objects.

Are there any exceptions to Bertrand's theorem?

Yes, there are a few exceptions to Bertrand's theorem. One exception is in the case of a central force field with a potential that is not spherically symmetric, such as a rotating central body. In this case, there can be other types of closed orbits, such as Lissajous orbits. Additionally, in the presence of external forces, such as tidal forces, there can be non-closed orbits as well.

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