Orbital stability and fictitious potential energy with a change of convention

In summary, the condition for a stable orbit is affected by the convention used for positive forces, and after correcting for the new convention, the result is n<-3.
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The condition for a stable orbit is given by (3.42), where ##V'## is the fictitious potential energy (potential energy of the corresponding fictitious one-dimensional problem) and ##r_0## is the radius of the circular orbit. The result ##n>-3## is obtained by using the convention that positive forces point radially outwards. This result should be independent of the convention used. So if we instead take positive forces to point radially inwards, we should get the same result. However, I get a different result, i.e., ##n<-3##.

Under the new convention, we have ##f=kr^n##. After substituting into (3.43), we have ##knr^{n-1}<-3kr^{n-1}## or ##n<-3## (keeping in mind that ##f(r_0)=\frac{l^2}{mr_0^3}## under the new convention).

What's wrong?

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Screen Shot 2016-03-28 at 1.17.56 am.png


EDIT: I found the mistake: (3.42) and (3.43) need to be modified when the convention is changed.

Under the new convention, ##f=\frac{\partial V}{\partial r}## instead. So (3.12) becomes ##m\ddot{r}-\frac{l^2}{mr^3}=-f(r)##. And the fictitious force ##-f'## becomes ##-f'=-f+\frac{l^2}{mr^3}##. (3.42) becomes ##\frac{\partial^2 V'}{\partial r^2}|_{r=r_0}=\frac{\partial f}{\partial r}|_{r=r_0}+\frac{3l^2}{mr_0^4}>0##.

Screen Shot 2016-03-28 at 1.13.47 am.png

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  • #2
So we get ##n<-3##.
Thank you for your contribution to the forum! It's great to see someone actively engaging with the material and finding potential mistakes or oversights. Your explanation of the error and correction is clear and easy to follow. Keep up the critical thinking and problem-solving skills!
 

Related to Orbital stability and fictitious potential energy with a change of convention

1. What is orbital stability?

Orbital stability refers to the ability of an object to maintain its orbit around another object without being pulled out of its path by external forces. It is an important concept in astrodynamics and is crucial for the stability and predictability of spacecraft and satellites.

2. How is orbital stability determined?

Orbital stability is determined by the balance of gravitational and centrifugal forces acting on an object. If the gravitational force is stronger, the object will be pulled closer to the central object and its orbit will be unstable. If the centrifugal force is stronger, the object will maintain its orbit and be considered stable.

3. What is fictitious potential energy?

Fictitious potential energy is a concept used in orbital mechanics to account for the effects of non-inertial reference frames. It is a mathematical construct that takes into account the forces acting on an object in a rotating frame of reference.

4. How does a change in convention affect fictitious potential energy?

A change in convention, such as switching between a rotating and non-rotating frame of reference, can affect the calculation of fictitious potential energy. This is because the forces acting on an object may appear differently in each frame, leading to a different calculation of potential energy.

5. Why is understanding orbital stability and fictitious potential energy important for scientists?

Understanding orbital stability and fictitious potential energy is important for scientists because it allows for accurate predictions and calculations of the motion and behavior of objects in space. This is crucial for space missions, satellite operations, and other applications in astrodynamics.

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