Solving for Central Force in $r = c\theta^2$ Orbit

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SUMMARY

This discussion focuses on deriving the central force function \( f(r) \) for a particle moving in the orbit defined by \( r = c\theta^2 \). The key equation derived is \( f(r) = -h^2\left(\frac{6c}{r^4} + \frac{1}{r^3}\right) \), where \( r^2\dot{\theta} = h \) is a constant representing angular momentum. Participants discuss the application of the radial equation \( \ddot{r} - r\dot{\theta}^2 = -f(r) \) and the substitution \( u(\theta) = \frac{1}{r(\theta)} \) to simplify calculations. The challenge lies in correctly differentiating \( r \) and substituting variables to eliminate \( \theta \).

PREREQUISITES
  • Understanding of polar coordinates and basis vectors, specifically \( (r, \theta) \) and \( (e_r, e_\theta) \).
  • Familiarity with central force motion and conservation of angular momentum in conservative fields.
  • Knowledge of differential equations, particularly in the context of motion dynamics.
  • Experience with substitutions in calculus, such as \( u(\theta) = \frac{1}{r(\theta)} \).
NEXT STEPS
  • Study the derivation of central force equations in polar coordinates.
  • Learn about the conservation of angular momentum and its implications in orbital mechanics.
  • Explore techniques for solving second-order differential equations in physics.
  • Investigate the use of substitutions in differential equations to simplify complex problems.
USEFUL FOR

Students and professionals in physics, particularly those focusing on classical mechanics, orbital dynamics, and mathematical methods in physics. This discussion is beneficial for anyone looking to deepen their understanding of central force problems and their mathematical formulations.

Carla1985
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Could someone please explain how I work with $-mf(r)e_r$ in this question. Usually we get given an equation (like the one for f(r)) and have to work out the orbit by getting a differential equation etc. I'm not too sure how to work it this way around.

"A particle of mass m moves under the influence of a central force $\textbf{F}(\textbf{r}) =−mf(r)e_r$, in the orbit

$r = c\theta^2$, (1)


where c > 0 and (r, θ) and er , eθ are the polar co-ordinates and corresponding basis vectors in the plane of motion of the particle. Show that:
\[
f(r)=-h^2(\frac{6c}{r^4}+\frac{1}{r^3})
\]
where $r^2\dot{\theta}=h$ is constant



[Hint: Use the substitution $u(\theta)=\frac{1}{r(\theta}$ to write the radial equation $\ddot{r}-r\dot{\theta}^2=-f(r)$ in terms of u(θ), and then determine f using this equation and (1).]"
 
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Carla1985 said:
Could someone please explain how I work with $-mf(r)e_r$ in this question. Usually we get given an equation (like the one for f(r)) and have to work out the orbit by getting a differential equation etc. I'm not too sure how to work it this way around.

"A particle of mass m moves under the influence of a central force $\textbf{F}(\textbf{r}) =−mf(r)e_r$, in the orbit

$r = c\theta^2$, (1)

where c > 0 and (r, θ) and er , eθ are the polar co-ordinates and corresponding basis vectors in the plane of motion of the particle. Show that:
\[
f(r)=-h^2(\frac{6c}{r^4}+\frac{1}{r^3})
\]
where $r^2\dot{\theta}=h$ is constant


[Hint: Use the substitution $u(\theta)=\frac{1}{r(\theta}$ to write the radial equation $\ddot{r}-r\dot{\theta}^2=-f(r)$ in terms of u(θ), and then determine f using this equation and (1).]"

Hi Carla!

Your equations are:

$$\ddot r - r \dot \theta^2=-f(r) \qquad$$ central acceleration
$$r^2\dot \theta = h \qquad\qquad\qquad$$ preservation of angular momentum in a conservative central field
$$r=c\theta^2 \qquad\qquad\qquad$$ the given orbit

Can you solve $f(r)$ from these, expressing it using only $r$?
 
I'm not sure how to do the $\ddot{r}$ part. I rearranged $r=c\dot{\theta}^2$ for theta and subbed that into get
$f(r)=-(\ddot{r}-\frac{h^2}{r^3})$

I differentiated r and got $\dot{r}=2c\theta\dot{\theta}$
and then subbed in theta again: $\frac{2ch\theta}{r^2}$ and then did the same thing again to get $\ddot{r}=\frac{2ch}{r^2}\theta\dot{\theta}=\frac{2ch^2}{r^2}\theta$ which doesn't add up at all.

I think the hint is confusing me too, it says to do a substitution u=1/r which we always do our other questions but I'm not sure where that applies here.
 
The substitution simply makes some of the problem easier to work. But it is not necessary. See if you can finish it the way I like Serena is helping you with. It will help if you if you then want to go back and use the hint.

-Dan
 
Thanks, I am still working on it thought I think I am going to take a break and get some sleep. its past midnight and the kids will have me up at 7am lol. I am so close its frustrating though.
I have $\ddot{r}=\frac{2ch^2\theta}{r^4}$ instead of $\frac{6ch^2}{r^4}$ and I cannot for the life of me see how I get rid of theta and get a 3 instead.

Maybe a fresh look in the morning will tell me where I've gone wrong though hehe.
 
Carla1985 said:
Maybe a fresh look in the morning will tell me where I've gone wrong though hehe.

Well... the morning has passed.
Any new insights? ;)
 

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