Find force lawa from orbit equation

In summary: L^2}\left(\frac{1}{u^3}\left(\frac{du}{d\theta}\right)^2\right)Simplifying this, we get:\frac{d^2u}{d\theta^2} + u = -\frac{mF(r_0^{-1})}{L^2}\left(\frac{1}{u^3}\right)Since we know that the particle is moving in a circular orbit, the force must be balanced by the centripetal force, which is given by:F = \frac{mv^2}{r} = \frac{m}{r}\left(\frac{1}{u^3}\left(\frac{du}{d
  • #1
KBriggs
33
0

Homework Statement


The orbit of a particle moving on a central field is a circle passing through the origin, namely, [tex]r = r_0cos(\theta)[/tex]. Show that the force law is inverse fifth power.


Homework Equations



[tex]\frac{d^2u}{d\theta^2} + u = \frac{-mF(u^{-1})}{L^2u^2}[/tex]
[tex]u=r^{-1}[/tex]

The Attempt at a Solution



I keep getting that it is inverse third power...

[tex]u = \frac{1}{r_0cos(\theta)}[/tex]
then
[tex]\frac{d^2u}{d\theta^2} = u + \frac{tan^2(\theta)}{u}[/tex]

so

[tex]F(u^{-1}) = \frac{-1}{m}\left(L^2u^2\left(u + \frac{tan^2(\theta)}{u}\right) + L^2u^2\right)[/tex]

[tex]=\frac{-2L^2}{m}\left(u^3+utan(\theta)\right)[/tex]

so [tex]f(r) = \frac{-2L^2}{m}\left(\frac{1}{r^3}+\frac{tan(\theta)}{r}\right)[/tex]

Where am I going wrong?
 
Last edited:
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  • #2


Thank you for your post. In order to show that the force law is inverse fifth power, we need to find a relation between the force and the distance r. From your attempt, it seems that you have found a relation between the force and the angle \theta, which is not what we are looking for.

To show that the force is inverse fifth power, we can start from the equation of motion for a particle moving on a central field:

\frac{d^2r}{d\theta^2} + r = -\frac{mF(r)}{L^2}

where r is the distance from the origin, \theta is the angle, m is the mass of the particle, and L is the angular momentum. We can then substitute u = r^{-1} into this equation to get:

\frac{d^2u}{d\theta^2} + u = -\frac{mF(u^{-1})}{L^2u^2}

Now, since we know that the particle moves in a circular orbit, we can substitute the given relation r = r_0cos(\theta) into the equation of motion. This gives us:

\frac{d^2u}{d\theta^2} + u = -\frac{mF(r_0^{-1}cos(\theta)^{-1})}{L^2u^2}

Using the trigonometric identity cos(\theta)^{-1} = sec(\theta), we can simplify this to:

\frac{d^2u}{d\theta^2} + u = -\frac{mF(r_0^{-1}sec(\theta))}{L^2u^2}

Now, we know that the particle is moving in a circular orbit, so the acceleration is given by a = v^2/r, where v is the tangential velocity. We can express the tangential velocity in terms of u and \theta as:

v^2 = \frac{d}{d\theta}\left(\frac{1}{u}\right)^2 = \frac{1}{u^3}\left(\frac{du}{d\theta}\right)^2

Substituting this into the equation of motion, we get:

\frac{d^2u}{d\theta^2} + u = -\frac{mF(r_0^{-1}sec(\theta))}{
 
  • #3


Your mistake is in your substitution of u. u = r^-1 is not the correct substitution for this problem. The correct substitution is u = r_0cos(\theta). This will change your final result to be inverse fifth power.
 

What is the purpose of finding the force law from an orbit equation?

The purpose of finding the force law from an orbit equation is to understand the underlying physical principles and mathematical relationships that govern the motion of objects in orbit. This can help scientists make predictions and calculations for future space missions, as well as gain a deeper understanding of the dynamics of our solar system.

What is the process for finding the force law from an orbit equation?

The process for finding the force law from an orbit equation involves using known parameters such as the mass of the orbiting object, its velocity, and the radius of its orbit, to solve for the unknown force acting on the object. This can be done using mathematical equations such as Newton's law of gravitation or Kepler's laws of planetary motion.

What are some common assumptions made when finding the force law from an orbit equation?

Some common assumptions made when finding the force law from an orbit equation include assuming that the orbiting object is moving in a vacuum, that the force acting on the object is constant, and that the orbit is stable. These assumptions may vary depending on the specific situation and can affect the accuracy of the calculated force law.

What factors can affect the accuracy of the force law found from an orbit equation?

Several factors can affect the accuracy of the force law found from an orbit equation, such as the precision of the measured parameters, the accuracy of the mathematical models used, and the inclusion of potential external forces or perturbations. It is important to consider these factors and their potential impact on the calculated force law.

How can the force law found from an orbit equation be used in real-world applications?

The force law found from an orbit equation can be used in various real-world applications, such as space navigation, spacecraft trajectory planning, and understanding the motion of celestial bodies. It can also help scientists make predictions and calculations for future space missions, as well as aid in the development of new technologies related to space exploration.

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