The Kepler Problem Part 1-Classical and Relativistic Mechanics-Lecture Handout, Exercises of Classical and Relativistic Mechanics

This lecture handout is part of Advanced Classical and Relativistic Mechanics course. Prof. Manasi Singh provided this handout at Punjab Engineering College. It includes: Kepler, Problem, Newtonian, Mechanics, Gravity, Position, Function, Conservation, Angular, Momentum

Typology: Exercises

2011/2012

Uploaded on 07/19/2012

davdas900
davdas900 🇮🇳

4.6

(5)

110 documents

1 / 2

Toggle sidebar

This page cannot be seen from the preview

Don't miss anything!

bg1
Thus the energy looks just like the energy of a particle of mass min a potential Veff on the half-line
{0< r < ∞}. We have reduced the problem to a 1-dimensional problem! Veff is called the effective
potential. Note that the second term creates the effect of a repulsive force equal to j2/mr3, called
the centrifugal force.
3. Show that
˙r=r2
m(EVeff (r)).(4)
We could solve this differential equation to find ras a function of t, but it’s nicer to find ras a
function of θ, since this allows us to see the shape of the particles’ orbits. In fact it turns out to be
easier to first find θas a function of rand then solve for rin terms of θ so that’s what we’ll do.
4. Using equations (3) and (4) show that
dr =j/mr2
q2
m(EVeff (r))
.
Conclude that
θ=θ0+Z(j/mr2)dr
q2
m(EVeff (r))
(5)
Now let’s specialize to the case of gravity, where f(r) = k/r2and thus V(r) = k /r
for some constant k.
5. Sketch a graph of the effective potential Veff (r) in this case, and say what a particle moving
in this potential would do, depending on its energy E.
6. Show using equation (5) that
θ=θ0+ arccos
j
mr k
j
q2E
m+k2
j2
.
This is the only part of this homework where you really need to sweat. However, some ways to do
it are easier than others, so think a bit before you plunge into an enormous masochistic calculation
if you do it intelligently, you will only need a medium-sized masochistic calculation! For example,
you may want to derive a general formula for
Zdx
ax2+bx +c
and then use it to do the integral in equation (5).
7. Reduce the clutter a bit more by defining
p=j2/km, e =r1 + 2Ej2
mk2.
Show that in terms of these variables we have
θ=θ0+ arccos p/r 1
e
2
docsity.com
pf2

Partial preview of the text

Download The Kepler Problem Part 1-Classical and Relativistic Mechanics-Lecture Handout and more Exercises Classical and Relativistic Mechanics in PDF only on Docsity!

Thus the energy looks just like the energy of a particle of mass m in a potential Veff on the half-line { 0 < r < ∞}. We have reduced the problem to a 1-dimensional problem! Veff is called the effective potential. Note that the second term creates the effect of a repulsive force equal to j^2 /mr^3 , called the centrifugal force.

  1. Show that r˙ =

m

(E − Veff (r)). (4)

We could solve this differential equation to find r as a function of t, but it’s nicer to find r as a function of θ, since this allows us to see the shape of the particles’ orbits. In fact it turns out to be easier to first find θ as a function of r and then solve for r in terms of θ — so that’s what we’ll do.

  1. Using equations (3) and (4) show that

dθ dr

j/mr^2 √ 2 m (E^ −^ Veff^ (r))

Conclude that

θ = θ 0 +

(j/mr^2 ) dr √ 2 m (E^ −^ Veff^ (r))

Now let’s specialize to the case of gravity, where f (r) = −k/r^2 and thus V (r) = −k/r for some constant k.

  1. Sketch a graph of the effective potential Veff (r) in this case, and say what a particle moving in this potential would do, depending on its energy E.
  2. Show using equation (5) that

θ = θ 0 + arccos

j mr −^

k √ j 2 E m +^

k^2 j^2

This is the only part of this homework where you really need to sweat. However, some ways to do it are easier than others, so think a bit before you plunge into an enormous masochistic calculation — if you do it intelligently, you will only need a medium-sized masochistic calculation! For example, you may want to derive a general formula for ∫ dx √ ax^2 + bx + c

and then use it to do the integral in equation (5).

  1. Reduce the clutter a bit more by defining

p = j^2 /km, e =

2 Ej^2 mk^2

Show that in terms of these variables we have

θ = θ 0 + arccos

p/r − 1 e

docsity.com

and thus r =

p 1 + e cos(θ − θ 0 )

Note that when θ = θ 0 the denominator is maximized, so r is minimized. We call this point the perihelion of the orbit, since in Newton’s original application to the earth going around this sun, this is the point on the earth’s orbit where its distance to the sun is minimized.

  1. Show that equation (6) describes an ellipse, parabola or hyperbola in polar coordinates, depending on the value of the parameter e, which we call the eccentricity. To do this, first simplify things by rotating the coordinate system so that θ 0 = 0. Then express the variables r, θ in terms of x, y and show that equation (6) becomes the equation

(1 − e^2 )x^2 + 2epx + y^2 = p^2.

Show that for e = 0 this describes a circle of radius p. Show also that for 0 < e < 1 it describes an ellipse, for e = 1 it describes a parabola, and for e > 1 it describes a hyperbola. Newton used the elliptic case to predict when the comet discovered by Edmund Halley would return! However, he didn’t give Halley much credit for obtaining the necessary data.

  1. How are the three kinds of orbits — ellipse, parabola or hyperbola — related to the energy E?

docsity.com