A comet revolves around the sun

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Homework Help Overview

The problem involves a comet's motion in a closed elliptical trajectory around the sun, specifically examining the relationship between the position vector and the velocity vector at the perihelion and aphelion. The goal is to demonstrate that these vectors are perpendicular at those points, under the influence of gravity alone.

Discussion Character

  • Conceptual clarification, Mathematical reasoning, Assumption checking

Approaches and Questions Raised

  • The original poster attempts to analyze the motion equations for an elliptical orbit and considers the implications of position and velocity at extreme points of the orbit. They question the validity of their reasoning regarding the relationship between the derivatives of the position vector and the velocity vector.
  • Some participants question the distinction between scalar and vector quantities in the original poster's reasoning, suggesting a need for clarity in the mathematical expressions used.
  • Another participant shares their experience of discovering a theorem related to ellipses and how it contributed to their understanding of the problem.
  • There is a discussion about the assumptions made regarding the derivatives of the position vector and the implications for the velocity vector.

Discussion Status

The discussion is ongoing, with participants exploring different interpretations of the original poster's reasoning. Some guidance has been offered regarding the mathematical relationships involved, and there is a recognition of the need for clarity in the use of vector notation. The original poster appears to be reconsidering their assumptions based on feedback.

Contextual Notes

Participants are navigating the complexities of vector calculus and the geometry of ellipses, with some expressing uncertainty about the mathematical notation and concepts involved. There is an acknowledgment of the original poster's struggle with the assumptions related to the motion of the comet.

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Homework Statement



A comet revolves around the sun in a closed elliptical trajectory. Ignore any force acting upon it besides gravity. Prove that the angle between the position vector (sun in the origin) and the velocity vector of the comet at its perihelion and aphelion is 90º.

The Attempt at a Solution



I tried to approach this problem by writing down the motion equations for a body on an elliptical orbit under the action of gravity. But it is a second order differential equation, that I later found out has no analytic solution.

So I just thought: when the comet is nearest and furthest from the sun, position r(t) must have a maximum/minimum, hence dr(t)/dt = 0, at those points. That also works for the r(t)^2, so dr(t)^2/dt = 0 <=> r(t)\cdotv(t) = 0 and this happens (since none of them is zero) only when they are both perpendicular.

However, by assuming dr(t)/dt = 0, I'm assuming that v(t) = 0 for some time t. But as we know that is never true, has the comet never stops moving. Is my solution valid? If so, why? If not, could you give me an hint? Does this all come down to the geomtry of the elipse ( because I never studied the equations that describe ellipses)?
 
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I think you're getting mixed up between scalars and vectors. If ##\vec r(t)## is the position vector, what is its magnitude? What do you get when that is at an extreme value?
 
After a few unsuccessful efforts to try to prove it by means of pure geometry, I learned a very useful theorem about ellipses, that the tangent of a point bissects the exterior angle. I just had to prove that. Then I found the answer where I least expected. I learned about Fermat's principle of least time, and with a little bit of thinking I had my proof.

I was really pleased with that, because those are the kind of answers I'm the most attracted to in physics.
 
Glad you got there, but it's not clear to me whether you now understand what you did wrong here:
Calabi_Yau said:
when the comet is nearest and furthest from the sun, position r(t) must have a maximum/minimum, hence dr(t)/dt = 0, at those points. That also works for the r(t)^2, so dr(t)^2/dt = 0 <=> r(t)\cdotv(t) = 0 and this happens (since none of them is zero) only when they are both perpendicular.

However, by assuming dr(t)/dt = 0, I'm assuming that v(t) = 0 for some time t
The first paragraph works if what you mean is:
when the comet is nearest and furthest from the sun, position ##r(t) = |\vec r(t)|## must have a maximum/minimum, hence dr(t)/dt = 0, at those points. That also works for the ##r(t)^2 = \vec r \cdot \vec r##, so dr(t)^2/dt = 0 <=> ##\vec r(t) \cdot \dot {\vec r}(t) = 0## and this happens (since none of them is zero) only when they are perpendicular.​
But what are you saying in the second paragraph? dr(t)/dt = 0 does not imply ##\vec v(t) = 0 ## nor ##|\vec v(t)| = 0 ##. ##\frac {d\vec r(t)}{dt} = 0## would imply that, but that's not what you assumed.
 
Right, I see. I assumed \frac{dr.r}{dt} = 0 does not imply dr(t)/dt = 0.

(Sorry for not writing with the proper symbols, but I am not very used to using those features)
 
Calabi_Yau said:
Right, I see. I assumed \frac{dr.r}{dt} = 0 does not imply dr(t)/dt = 0.

(Sorry for not writing with the proper symbols, but I am not very used to using those features)
If you don't want to be bothered with LaTex for vectors, you can just put the vector variables in bold.
 

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