How can I find the shape of an orbit under an inverse cube law of force?

In summary, the author found an equation for the explicit integration of the shape, r(\theta), of a one-body-problem (a particle rotating about a set point, O) for arbitrary \mathbf{f} = -f(r)\hat{\mathbf{r}}, and used it to find r(\theta) for an inverse square law f(r) = \mu / r^2. Where u = (1/r). They were able to get r = r(\theta(t)) => \dot{r} = {{dr} \over {d\theta}} {{d\theta} \over {dt}} = {{dr}
  • #1
bushdayroses
2
0

Homework Statement

I've found the a general form of equation for the explicit integration of the shape, [itex]r(\theta)[/itex], of a one-body-problem (a particle rotating about a set point, O) for arbitrary [itex]\mathbf{f} = -f(r)\hat{\mathbf{r}}[/itex], and used it to find [itex]r(\theta)[/itex] for an inverse square law [itex]f(r) = \mu / r^2[/itex]. Where [itex]u = (1/r)[/itex].

I was able to get [tex]r = r(\theta(t)) => \dot{r} = {{dr} \over {d\theta}} {{d\theta} \over {dt}} = {{dr} \over {d\theta}} \left({{h_0} \over {r^2}}\right)[/tex]

Where [itex]h_0 \neq 0[/itex] is the constant angular momentum.

Can anyone help me to figure out the shape under an inverse cube law of force, [itex]f(r) = {{\nu} / {r^3}}[/itex], and show that if [itex]\nu \le h^2[/itex], the orbit is unbounded?

I know that this solution will depend on the relative sizes of [itex]\nu[/itex] and [itex]h[/itex], but I can't seem to get this to work.EDIT:: Got LaTex to work
 
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  • #2
One way to approach this problem is to use the substitution

[tex]r=\frac{1}{u}\mbox{ and u =}\frac{1}{r}[/tex]

then differentiate r with respect to t giving

[tex]\dot{r}=-\frac{1}{u^2}\frac{du}{d\theta}\frac{d\theta}{dt}[/tex]

and

[tex]\dot{\theta}=\frac{L}{mr^2}[/tex]

This will give

[tex]\dot{r}=-\frac{L}{m}\frac{\mbox{d}u}{\mbox{d}\theta}[/tex]

Differentiate again with respect to t to find the second derivative of r in terms of u and theta. Write the general equation of motion for r in terms of F(r) and "centrigugal" force (L2/(mr3), and substitue the second derivative of r with respect to t. You will arrive at an equation of motion in terms of u and theta. This differential equation is easier to solve than straightforward methods. Once u is found substitue 1/r and solve for r.
 
  • #3
Got it figured out. Thanks
 

FAQ: How can I find the shape of an orbit under an inverse cube law of force?

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Orbital Dynamics is a branch of physics that studies the motion of objects in space under the influence of gravitational forces. It involves analyzing the orbits of planets, moons, satellites, and other celestial bodies and understanding how they are affected by various factors such as mass, velocity, and distance.

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