Classical mechanics: Central potential, trajectory

In summary, the particle trajectories into the central potential are possible if r<r_0 and r>r_0. If r=r_0, then there is no movement.
  • #1
fluidistic
Gold Member
3,923
261

Homework Statement


Determine the possible trajectories of a particle into the following central potential: [itex]U(r)=U_0[/itex] for [itex]r< r_0[/itex] and [itex]U(r)=0[/itex] for [itex]r>r_0[/itex].

Homework Equations


Not sure. What I used: Lagrangian+Euler/Lagrange equations.

The Attempt at a Solution


I used polar coordinates but I'm not sure it's well justified. Since we're dealing with a central potential problem, isn't the motion restricted to a 2 dimensional plane? If so, then I think it's safe to use polar coordinates.
Ok so my Lagrangian is [itex]L=T-V=\frac{m(\dot \theta r^2 + \dot r ^2 )}{2}-U(r)[/itex]. I notice that [itex]\theta[/itex] is cyclic, thus the angular momentum is conserved.
Using Lagrange's equations for [itex]\theta[/itex], I reached the differential equation [itex]\dot r r = cte[/itex]. For [itex]r[/itex], I reach [itex]\ddot r - \dot \theta r =0[/itex].
I know I made an error, I reach the same motion equation regardless what U(r) thus r is.
Hmm... Since [itex]\theta[/itex] is cyclic, does this imply that [itex]\dot \theta =0[/itex]?
If so, then [itex]\ddot r =0[/itex]. But this is senseless since it would imply that [itex]\dot r[/itex] is also a constant, and thus that r is also a constant from my first use of Lagrange equations...
It might be a little too late to do physics for me now, but I'm willing to put the effort.
Any help will be appreciated. Thanks a lot!

Edit: I notice an error for the 1st Euler/Lagrange equation conclusion. I do reach that r is constant instead of [itex]r \dot r[/itex], which still doesn't make sense to me.
 
Last edited:
Physics news on Phys.org
  • #2
There is a silly mistake at T (kinetic energy). Check that :smile:
(by the way, [itex]d\theta/dt=0[/itex] is meaningless. That would mean the particle's motion, including the initial state, is restricted to radial direction)
 
  • #3
hikaru1221 said:
There is a silly mistake at T (kinetic energy). Check that :smile:
(by the way, [itex]d\theta/dt=0[/itex] is meaningless. That would mean the particle's motion, including the initial state, is restricted to radial direction)
Thanks for pointing this out. Indeed.
T is in fact [itex]\frac{m(\dot \theta ^2 r^2 + \dot r ^2 )}{2}[/itex].
The equations of motion I reach are now [itex]2r \dot r \dot \theta + \ddot \theta r^2=0[/itex] and [itex]\ddot r - \dot \theta ^2 r =0[/itex].
I also know that [itex]r^2 \theta = constant[/itex].
I don't know if I can divide any of these equations by r. As far as I know, r could be worth 0 and thus I can't divide by r.
I don't know how to proceed in order to reach the trajectories; or in other words, how to solve the motion equations.
Also I notice that there's no difference at all for r>r_0 or r<r_0 in my equations. It seems wrong to me.
 
  • #4
The [itex]\partial L / \partial r[/itex] term involves [itex]\partial U / \partial r = d U / dr[/itex]. What is [itex]d U / dr?[/itex] It isn't zero everywhere.
 
  • #5
George Jones said:
The [itex]\partial L / \partial r[/itex] term involves [itex]\partial U / \partial r = d U / dr[/itex]. What is [itex]d U / dr?[/itex] It isn't zero everywhere.

Ah yes you're right. It's worth 0 everywhere except in [itex]r=r_0[/itex] where it's worth [itex]\pm \infty[/itex] depending upon if [itex]U_0[/itex] is greater or lesser than 0.
So U(r) isn't analytic. How do I deal with this problem?!
 
  • #6
Are you familiar with the Dirac delta "function"?
 
  • #7
George Jones said:
Are you familiar with the Dirac delta "function"?

A bit. I've seen some relations and the formal definition of it (if I remember well it was the limit of a sequence) but I'm not so comfortable with it.
Out my memory, I remember that [itex]\int g(x) \delta (x-a) dx=g(a)[/itex] where the integral bounds cover of course an interval containing x=a.
I didn't check in wikipedia so my memory might fail. Also a friend of mine once told me it was a double abuse of notation to write the integral I just wrote, but I didn't really understood why.
So in my example, [itex]a=r_0[/itex]. And [itex]g(x)[/itex] would be [itex]U(r)[/itex]. So basically... err no that can't be... Hmm.
 
  • #8
Have you seen the connection between the Heavisde step function and the Dirac delta function?

With experience, it is actually possible to see the answer to the original problem without doing any calculations (somewhat similar to billiard ball collision problems). We should go through the calculations, though.
 
  • #9
George Jones said:
Have you seen the connection between the Heavisde step function and the Dirac delta function?

With experience, it is actually possible to see the answer to the original problem without doing any calculations (somewhat similar to billiard ball collision problems). We should go through the calculations, though.

About the Heaviside function: Heard of it before but never checked it in details. I just did in wikipedia and its connection to the Dirac Delta function seems to be that [itex]H(x)=\int _{-\infty} ^x \delta (t)dt[/itex]. So in my case it'd be worth 0 for [itex]x<r_0[/itex] and 1 for [itex]x>r_0[/itex]. But I don't see how this can help. I've checked in Golstein's book (1st edition) on Classical dynamics and to my surprise there's a short comment on Dirac's Delta and nothing on Heaviside function.
So the problem seems simple but it requires the use of Dirac's delta due to the singularity of the potential function. I'll help for further help here as I'm in unknown territory (I'll still try to figure out things if I can). And thank you so far.
 
  • #10
fluidistic said:
[itex]H(x)=\int _{-\infty} ^x \delta (t)dt[/itex]

Can you invert this?
fluidistic said:
So in my case it'd be worth 0 for [itex]x<r_0[/itex] and 1 for [itex]x>r_0[/itex].

Consequently, [itex]U \left( r \right) = U_0 H \left( r_0 - r \right)[/itex]. What does this give for [itex]dU / dr[/itex]?

fluidistic said:
But I don't see how this can help. I've checked in Golstein's book (1st edition) on Classical dynamics and to my surprise there's a short comment on Dirac's Delta and nothing on Heaviside function.
So the problem seems simple but it requires the use of Dirac's delta due to the singularity of the potential function. I'll help for further help here as I'm in unknown territory (I'll still try to figure out things if I can). And thank you so far.

Look up "impulsive force" in Goldstein or your text or ...
 
  • #11
George Jones said:
Can you invert this?
Do you mean that I find the inverse of the Heaviside function?


Consequently, [itex]U \left( r \right) = U_0 H \left( r_0 - r \right)[/itex]. What does this give for [itex]dU / dr[/itex]?



Look up "impulsive force" in Goldstein or your text or ...
The first edition of Golstein as only 1 exercise about impulsive forces. It seems rather tough to me and doesn't seem to involve any special function.
Ok back to your expression. Now I understand that [itex]U(r)=U_0 H(r_0-r)[/itex]. :smile:
I also understand I must find [itex]\frac{d U}{dr}[/itex]. If I'm not wrong, I think this is simply worth [itex]U_0 \delta (r_0 -r)[/itex].
So as I had, [itex]\frac{d U}{dr}=0[/itex] for [itex]r\neq r_0[/itex] which makes sense.
Now in [itex]r=r_0[/itex] it's worth [itex]\infty[/itex] as it should I guess.
How would I continue? I'm not seeing where we're going.
 
  • #12
That expression [itex]U(r)=U_0H(r_0-r)[/itex] along with one ODE and the expression [itex]r^2\dot{\theta}=C=const[/itex] will give you an ODE of r. As you want to stay cautious with dividing by r, you may simply consider ODE at [itex]r \neq 0[/itex]. You will get something like this:
[itex]f(\ddot{r},\dot{r},r)=\delta(r-r_0)[/itex]

Here's the trick: observe that the change only happens at [itex]r=r_0[/itex] (this is what George meant by impulsive force: an immediate change without change in position). So deal with the ODE within the interval: [itex](r_0^-;r_0^+)[/itex]. Notice that: [itex]\int^{0^+}_{0^-}\delta(x)dx=1[/itex]
 
  • #13
Thanks guys for all the help so far.
To hikaru, could you be a little more specific about the ODE's I should get? I've redone all the algebra. I do reach [itex]\dot \theta r^2 = constant[/itex]. I do reach [itex]\ddot \theta r ^2 + 2 \dot \theta \dot r r =0[/itex]. Is this the first ODE you talk about?
I don't see how I can "mix them" along with [itex]U(r)=U_0H(r_0-r)[/itex] in order to get a single ODE depending on r.
And ok for your trick, I'll use it.

Edit: If [itex]\frac{dU}{dr}=U_0 \delta (r-r_0 )[/itex] then I reach the ODE [itex]\dot \theta ^2 r + U_0 \delta (r-r_0)-\ddot r =0[/itex]. I have no idea if this is right.
 
  • #14
fluidistic said:
[itex]\dot \theta ^2 r + U_0 \delta (r-r_0)-\ddot r =0[/itex]. I have no idea i this is right.

Good! Are there some missing m's?

Now use your other equation to eliminate [itex]\dot \theta[/itex].
 
  • #15
George Jones said:
Good! Are there some missing m's?

Now use your other equation to eliminate [itex]\dot \theta[/itex].

Thanks for helping me. :)
Yes I miss one m (my draft hasn't this error so I suppose it's a typo error). Edit: OH actually 2 I see.
This should be [itex]m \dot \theta ^2 r + U_0 \delta (r-r_0)-m \ddot r =0[/itex](*).
Now I'm not sure what equation to use. I assume you mean [itex]\dot \theta r^2=K_1[/itex] but I don't see how I can use it in order to give rid of [itex]\dot \theta[/itex] in (*).

Edit2: My bad nevermind, I think I know how!
 
  • #16
I get [itex]\frac{mK_1 ^2}{r^3}+U_0 \delta (r-r_0)-m \ddot r =0[/itex]. This is true for [itex]r\neq 0[/itex].
I need to solve this equation for r... Ok I'll think about how to do but I'm not that confident.
Edit: Ok it doesn't look that bad. I still have a doubt about the limits of some integrals (funnily I've helped someone on this forum yesterday night about the limits of an integral...); let me show you.
(*) is equivalent to [itex]\ddot r = \frac{K_1 ^2}{r^3} + \frac{U_0 \delta (r-r_0)}{m}[/itex].
I integrate with respect to time in order to get [itex]\dot r[/itex] (with the idea of doing it again to get r).
So I have [itex]\dot r=K_1 ^2 \int \frac{dt}{r^3} + \frac{U_0}{m} \int \delta (r-r_0)dt[/itex]. My guess is that the limits of the integrals are [itex]-\infty[/itex] and [itex]+\infty[/itex].
I'd like a confirmation if I'm on the right track and the limits are correct.
 
Last edited:
  • #17
Maybe I shouldn't give this hint, but ... reduction of order.
 
  • #18
George Jones said:
Maybe I shouldn't give this hint, but ... reduction of order.
Oops I didn't see this message. I edited my above post and was looking for a different approach. Could this work too?

Edit: If reduction of order is the only "easy" way to go then I'm already lost on what is the characteristic polynomial.
 
Last edited:
  • #19
fluidistic said:
So I have [itex]\dot r=K_1 ^2 \int \frac{dt}{r^3} + \frac{U_0}{m} \int \delta (r-r_0)dt[/itex]. My guess is that the limits of the integrals are [itex]-\infty[/itex] and [itex]+\infty[/itex].
I'd like a confirmation if I'm on the right track and the limits are correct.

This equation is correct, but since [itex]r \left( t \right)[/itex] is to be determined, we don't know how to do the integrals.
fluidistic said:
If reduction of order is the only "easy" way to go then I'm already lost on what is the characteristic polynomial.

See Type 2 (example almost halfway down the page) from

http://www.cliffsnotes.com/study_guide/Reduction-of-Order.topicArticleId-19736,articleId-19724.html .
 
Last edited by a moderator:

1. What is classical mechanics?

Classical mechanics is a branch of physics that describes the motion of objects under the influence of forces. It is based on the laws of motion and gravitation developed by Isaac Newton in the 17th century.

2. What is a central potential?

A central potential is a type of force that acts on an object towards a single point or center. It is mathematically described as a function of the distance between the object and the center, and it is often used to model the gravitational or electrostatic force between two objects.

3. How is the trajectory of an object determined in classical mechanics?

The trajectory of an object in classical mechanics is determined by solving the equations of motion, which describe how the position, velocity, and acceleration of the object change over time. These equations are derived from Newton's laws of motion.

4. Can central potential be used to describe all types of motion?

No, central potential can only be used to describe motion in which the force acts towards a single point or center. It cannot be used to model forces that act in different directions or vary in magnitude with distance.

5. What are some real-world applications of classical mechanics?

Classical mechanics has numerous applications in everyday life, such as in the design of vehicles, buildings, and other structures. It is also used in fields like astronomy, engineering, and sports to understand and predict the motion of objects.

Similar threads

  • Advanced Physics Homework Help
Replies
11
Views
1K
  • Advanced Physics Homework Help
Replies
16
Views
914
  • Advanced Physics Homework Help
Replies
4
Views
2K
  • Advanced Physics Homework Help
Replies
2
Views
825
  • Advanced Physics Homework Help
Replies
5
Views
1K
  • Advanced Physics Homework Help
Replies
25
Views
2K
  • Advanced Physics Homework Help
Replies
5
Views
2K
Replies
8
Views
236
  • Advanced Physics Homework Help
Replies
2
Views
2K
  • Advanced Physics Homework Help
Replies
2
Views
6K
Back
Top