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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
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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.
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.
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.
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).
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
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 − 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.