Conservation of the Laplace-Runge-Lenz vector in a Central Field

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Homework Help Overview

The discussion revolves around the conservation of the Laplace-Runge-Lenz vector in a central force field, specifically examining the implications of angular momentum conservation in orbital mechanics. Participants are exploring the relationship between radial and angular components of acceleration in the context of elliptical orbits.

Discussion Character

  • Conceptual clarification, Mathematical reasoning, Assumption checking

Approaches and Questions Raised

  • The original poster attempts to derive the relationship between angular momentum and acceleration components, questioning the assumption that acceleration is purely radial in elliptical orbits. Other participants discuss the implications of nonzero angular acceleration and its relation to the conservation of angular momentum.

Discussion Status

Participants are actively engaging with the problem, with some providing clarifications about the nature of acceleration in polar coordinates. There is a recognition of the need to reconcile the assumptions made in the derivation with the physical reality of elliptical motion.

Contextual Notes

There is an ongoing examination of the assumptions regarding the nature of motion in elliptical orbits, particularly concerning the constancy of angular velocity and the implications for acceleration components. The discussion reflects a mix of interpretations regarding the conditions under which the derivations are valid.

stephenklein
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Homework Statement
I'm tasked with showing the LRL vector is conserved in time when the potential is Newtonian. I.e. [itex]U(r) = -\frac{\alpha}{r},[/itex] with [itex]\alpha[/itex] constant.
Relevant Equations
[itex]\vec{L} = \vec{v} \times \vec{M} - \frac{\alpha \vec{r}}{r}, [/itex] where [itex]\vec{L}, \vec{M}[/itex] are the LRL vector and angular momentum, respectively
I actually have worked through the solution just fine by taking the derivative of \vec{L}:

\frac{d \vec{L}}{dt} = \dot{\vec{v}} \times \vec{M} - \alpha \left(\frac{\vec{v}}{r} - \frac{\left(\vec{v} \cdot \vec{r}\right)\vec{r}}{r^{3}}\right)
I permuted the double cross product:
\dot{\vec{v}} \times \vec{M} = \dot{\vec{v}} \times \left(m\vec{r} \times \vec{v}\right) = m\vec{r}\left(\dot{\vec{v}} \cdot \vec{v}\right) - m\vec{v}\left(\dot{\vec{v}} \cdot \vec{r}\right)
Here's where I'm running into trouble. In both Landau and my lecture notes, the next step is apparently to invoke
m\dot{\vec{v}} = \frac{\alpha \vec{r}}{r^{3}},
which comes from the fact that the force is Newtonian. But this implies the acceleration is only in the radial direction, which is only true for motions in circular orbit for which the angular velocity is constant. Obviously, for elliptical orbits, the condition that angular momentum is conserved implies that the angular velocity is at a maximum when r is at a minimum, and vice versa. Therefore, \dot{\phi} is not constant and m\dot{\vec{v}} will have an angular component as well. This can be seen as well from the equations of motion derived from the Lagrangian in polar coordinates.

Am I missing something? The derivation in Landau came under the section for Kepler's problem, so it doesn't seem obvious that I should assume the motion is perfectly circular, with no angular acceleration.
 
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stephenklein said:
Therefore, \dot{\phi} is not constant and m\dot{\vec{v}} will have an angular component as well.
In polar coordinates, the angular component of acceleration is given by ##a_{\phi} = 2\dot r \dot\phi + r \ddot \phi##. For reference see this document.

So, nonzero ##\ddot \phi## does not necessarily imply nonzero ##a_{\phi}##
 
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TSny said:
So, a nonzero ##\ddot \phi## does not necessarily imply nonzero ##a_{\phi}##
Wow, I feel like a dummy for not just looking up acceleration components in polar coordinates. That was immensely helpful, thank you.

So to flip the argument around, can we say that because ##m\dot{\vec{v}}## has only a radial component, that ##a_{\phi} = 0##, meaning ##2\dot{r} \dot{\phi} = -r\ddot{\phi}##? And physically, what would that refer to?
 
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stephenklein said:
So to flip the argument around, can we say that because ##m\dot{\vec{v}}## has only a radial component, that ##a_{\phi} = 0##, meaning ##2\dot{r} \dot{\phi} = -r\ddot{\phi}##?
Yes
stephenklein said:
And physically, what would that refer to?
I'm sorry, but I'm not sure what you are asking here.

You could say that it is a consequence of the conservation of angular momentum. The angular momentum is ##\vec M = mr^2\dot\phi \; \hat k## where ##\hat k## is a constant unit vector perpendicular to the plane of the orbit.

Since ##\dot {\vec M} = 0##, you have ##\frac {d }{dt}(mr^2 \dot \phi) = 0##. This implies ##2\dot{r} \dot{\phi} + r\ddot{\phi} = 0##.
 
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