- #1
stephenklein
- 6
- 3
- 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 [itex]\vec{L}[/itex]:
[tex] \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) [/tex]
I permuted the double cross product:
[tex]\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) [/tex]
Here's where I'm running into trouble. In both Landau and my lecture notes, the next step is apparently to invoke
[tex] m\dot{\vec{v}} = \frac{\alpha \vec{r}}{r^{3}}, [/tex]
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, [itex] \dot{\phi} [/itex] is not constant and [itex] m\dot{\vec{v}} [/itex] 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.
[tex] \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) [/tex]
I permuted the double cross product:
[tex]\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) [/tex]
Here's where I'm running into trouble. In both Landau and my lecture notes, the next step is apparently to invoke
[tex] m\dot{\vec{v}} = \frac{\alpha \vec{r}}{r^{3}}, [/tex]
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, [itex] \dot{\phi} [/itex] is not constant and [itex] m\dot{\vec{v}} [/itex] 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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