- #1
thalesofmiletus
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- TL;DR Summary
- Circular orbits are solution of Euler-Lagrange's equation for lagrangian in Kepler problem. But this is only necessary condition, not sufficient. Another condition is that second variation of lagrangian needs to be positive definite. And if my calculations are correct, it is not. But otherwise in Gelfands and Fomin's "Calculus of variations" there is footnote indicating that it should be (with all other theorems).
My point of view is bases on CALCULUS OF VARIATIONS by I. M. GELFANDS. and V. FOMIN. I would assume that you are familiar with the topic. I've found this book online, If needed I can provide link, but for now I don't know if it's legal in this site, so I won't.
(by the way, I'm new on this site, so if latex isn't working I will try to repair it, but I'd appreciate help in such case)
So basically junctional for Kepler problem is defigned as such
[tex]\int\left(\frac{1}{2} m(\dot r^2+r^2 \dot \varphi^2) +\frac{GMm}{r} \right)dt [/tex]
From which using E-L equations you can derive solution
[tex]r=\frac{p}{1+\varepsilon \cos{(\varphi-\varphi_0)}}[/tex]
where [tex]p=\frac{L^2}{GMm^2}[/tex] , [tex]\varepsilon=\sqrt{1+\frac{2EL^2}{G^2M^2m^3}}[/tex] , E is total energy [tex]E=\frac{1}{2} m\dot r^2+\frac{L^2}{2mr^2} -\frac{GMm}{r}[/tex] and L is angular momentum [tex]L=mr^2 \dot \varphi[/tex]. (I can provide my full solution if you need)
Before we consider special solution of circular orbits, let's derive formula for second variation in general case. Formula is given as
[tex] \delta^2J[h]=\frac{1}{2} \int_a^b \left( \sum_{i,k=1}^n F_{y_iy_k}h_ih_k + 2\sum_{i,k=1}^n F_{y_iy'_k}h_ih'_k + \sum_{i,k=1}^n F_{y'_iy'_k}h'_ih'_k\right) dx [/tex]
(Note that you cannot use (Ph',h')+(Qh,h) is this case, becouse that require [tex]F_{yy'}[/tex] to be simetrical, which IS NOT for this example)
where for junctional in Kepler problem partial derivatives are
[tex]F_{rr}=m \dot \varphi^2+\frac{2GMm}{r^3}[/tex]
[tex]F_{r\varphi}=F_{\varphi r}=F_{\varphi\varphi}=0[/tex]
[tex]F_{r \dot r}=0[/tex]
[tex]F_{r\dot\varphi}=2mr\dot\varphi[/tex]
[tex]F_{\varphi \dot r}=F_{\varphi \dot \varphi}=0[/tex]
[tex]F_{\dot r\dot r}=m[/tex]
[tex]F_{\dot r \dot \varphi}=0[/tex]
[tex]F_{\dot \varphi\dot \varphi }=mr^2[/tex]
Now let's asume that [tex]\varepsilon=0[/tex] (the solution is circle). Let [tex]r\equiv R[/tex], using angular momemtum formula and E-L equation with respect to r we can derive [tex]$L=\sqrt{GMm^2R}[/tex]. Substituting that to partials we get (ignoring ones that equal 0)
[tex]F_{rr}=m \dot \varphi^2+\frac{2GMm}{R^3}=\frac{3GMm}{R^3}[/tex]
[tex]F_{r\dot\varphi}=2mR\dot\varphi=2\sqrt{\frac{GMm^2}{R}}=2\sqrt{\frac{GMm}{R^3}\cdot mR^2}[/tex]
[tex]F_{\dot r\dot r}=m[/tex]
[tex]F_{\dot \varphi\dot \varphi }=mR^2[/tex]
So under integral we get
[tex] \frac{3GMm}{R^3}h_1^2+4\sqrt{\frac{GMm}{R^3}\cdot mR^2}h_1\dot h_2+mR^2\dot h_2^2+m\dot h_1^2[/tex]
which can be rearanged to
[tex]\left(\sqrt{\frac{3GMm}{R^3}}h_1+\sqrt{mR^2}\dot h_2\right)^2+\left(4-2\sqrt{3}\right)\sqrt{\frac{GMm^2}{R}}h_1\dot h_2+m\dot h_1^2[/tex]
what can be negative, for example if we take [tex]\dot h_2=-\sqrt{\frac{3GM}{R^4}}h_1[/tex] then the squared bracket is 0 and you can easily come on up h_1 that makes second variation negative.
So to conclude, there are (h_1,h_2) for which [tex]\delta^2J[h][/tex] are negative, so it cannot be positive definite. What means that circular orbits are not minimas of lagrangian. What means that they should not be present in world when we assume least-action principle. Well clearly there is something wrong in here. I hope some one might help me.One last remark. In Gelfands and Fomin's book there is footnote (page 119) that theorems regarding Jacobi equations are true even when [tex]F_{yy'}[/tex] is not simetrical. As far as I understand the book, from those theorems we deduce sifficient conditions for minimas of juntional. And if we ignore that [tex]F_{yy'}[/tex] is not simetrical and check Legendre and Jacobi conditions as it were simetrical, we get that both holds, even in strengthened versions. So we conclude that circular orbits are minimas of lagrangian in kepler problem? The footnote refers to (H. Niemeyer, private communication), how can I tell if this is valid?
(by the way, I'm new on this site, so if latex isn't working I will try to repair it, but I'd appreciate help in such case)
So basically junctional for Kepler problem is defigned as such
[tex]\int\left(\frac{1}{2} m(\dot r^2+r^2 \dot \varphi^2) +\frac{GMm}{r} \right)dt [/tex]
From which using E-L equations you can derive solution
[tex]r=\frac{p}{1+\varepsilon \cos{(\varphi-\varphi_0)}}[/tex]
where [tex]p=\frac{L^2}{GMm^2}[/tex] , [tex]\varepsilon=\sqrt{1+\frac{2EL^2}{G^2M^2m^3}}[/tex] , E is total energy [tex]E=\frac{1}{2} m\dot r^2+\frac{L^2}{2mr^2} -\frac{GMm}{r}[/tex] and L is angular momentum [tex]L=mr^2 \dot \varphi[/tex]. (I can provide my full solution if you need)
Before we consider special solution of circular orbits, let's derive formula for second variation in general case. Formula is given as
[tex] \delta^2J[h]=\frac{1}{2} \int_a^b \left( \sum_{i,k=1}^n F_{y_iy_k}h_ih_k + 2\sum_{i,k=1}^n F_{y_iy'_k}h_ih'_k + \sum_{i,k=1}^n F_{y'_iy'_k}h'_ih'_k\right) dx [/tex]
(Note that you cannot use (Ph',h')+(Qh,h) is this case, becouse that require [tex]F_{yy'}[/tex] to be simetrical, which IS NOT for this example)
where for junctional in Kepler problem partial derivatives are
[tex]F_{rr}=m \dot \varphi^2+\frac{2GMm}{r^3}[/tex]
[tex]F_{r\varphi}=F_{\varphi r}=F_{\varphi\varphi}=0[/tex]
[tex]F_{r \dot r}=0[/tex]
[tex]F_{r\dot\varphi}=2mr\dot\varphi[/tex]
[tex]F_{\varphi \dot r}=F_{\varphi \dot \varphi}=0[/tex]
[tex]F_{\dot r\dot r}=m[/tex]
[tex]F_{\dot r \dot \varphi}=0[/tex]
[tex]F_{\dot \varphi\dot \varphi }=mr^2[/tex]
Now let's asume that [tex]\varepsilon=0[/tex] (the solution is circle). Let [tex]r\equiv R[/tex], using angular momemtum formula and E-L equation with respect to r we can derive [tex]$L=\sqrt{GMm^2R}[/tex]. Substituting that to partials we get (ignoring ones that equal 0)
[tex]F_{rr}=m \dot \varphi^2+\frac{2GMm}{R^3}=\frac{3GMm}{R^3}[/tex]
[tex]F_{r\dot\varphi}=2mR\dot\varphi=2\sqrt{\frac{GMm^2}{R}}=2\sqrt{\frac{GMm}{R^3}\cdot mR^2}[/tex]
[tex]F_{\dot r\dot r}=m[/tex]
[tex]F_{\dot \varphi\dot \varphi }=mR^2[/tex]
So under integral we get
[tex] \frac{3GMm}{R^3}h_1^2+4\sqrt{\frac{GMm}{R^3}\cdot mR^2}h_1\dot h_2+mR^2\dot h_2^2+m\dot h_1^2[/tex]
which can be rearanged to
[tex]\left(\sqrt{\frac{3GMm}{R^3}}h_1+\sqrt{mR^2}\dot h_2\right)^2+\left(4-2\sqrt{3}\right)\sqrt{\frac{GMm^2}{R}}h_1\dot h_2+m\dot h_1^2[/tex]
what can be negative, for example if we take [tex]\dot h_2=-\sqrt{\frac{3GM}{R^4}}h_1[/tex] then the squared bracket is 0 and you can easily come on up h_1 that makes second variation negative.
So to conclude, there are (h_1,h_2) for which [tex]\delta^2J[h][/tex] are negative, so it cannot be positive definite. What means that circular orbits are not minimas of lagrangian. What means that they should not be present in world when we assume least-action principle. Well clearly there is something wrong in here. I hope some one might help me.One last remark. In Gelfands and Fomin's book there is footnote (page 119) that theorems regarding Jacobi equations are true even when [tex]F_{yy'}[/tex] is not simetrical. As far as I understand the book, from those theorems we deduce sifficient conditions for minimas of juntional. And if we ignore that [tex]F_{yy'}[/tex] is not simetrical and check Legendre and Jacobi conditions as it were simetrical, we get that both holds, even in strengthened versions. So we conclude that circular orbits are minimas of lagrangian in kepler problem? The footnote refers to (H. Niemeyer, private communication), how can I tell if this is valid?