Theoretical Dynamics Homework 9: Kepler's Laws and Orbit Calculations, Assignments of Physics

Homework problems from a theoretical dynamics course, specifically problems 25, 26, and 27. Problem 25 asks students to apply kepler's laws to determine the mass of the sun. Problems 26 and 27 involve calculating the orbit of a particle under the influence of a gravitational potential and making plots of the orbit and position versus time. Students are expected to use newton's law of universal gravitation and euler-lagrange's equations.

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Pre 2010

Uploaded on 08/26/2009

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THEORETICAL DYNAMICS PHY–5246
HOMEWORK 9
(October 20, 2002)
Due on Monday, October 29, 2002
PROBLEM 25
Imagine yourself being Kepler around the year 1610 and having compiled information
on the motion of all the planets you decide to make a table that includes: a) the name
of the planet, b) the period of revolution of the planet around the Sun (in years), c)
the average distance (or semi-major axis) from the planet to the Sun (in A.U.), and
d) the ratio of the period square to the average distance cubed. After having found
this amazing correlation (Kepler’s third law) compute the mass of the Sun. Although
not yet discover at the time, you may use Newton’s Law of Universal gravitation with
G=6.673 ×1011 m3kg1s2.
PROBLEM 26
a) Starting from Euler-Lagrange’s equation of motion for the radial motion of a
particle of mass mmoving in a central potential, i.e., m¨r=V0
eff (r), obtain
the differential equation for the orbit:
d2u
2+u=m
l2
f(1/u)
u2,
where u1/r and f(r) = V0(r). The above equation suggests how to obtain
the orbit of the particle r=r(θ) if the force law f=f(r) is known. Conversely,
if the orbit is known, one can deduce the force law.
b) Consider the equation of the orbit in Cartesian coordinates:
x2
a2+y2
b2= 1 .
Obtain the force law f=f(r).
c) Consider the equation of the orbit in Cartesian coordinates:
(xc)2
a2+y2
b2= 1 ,
where c=a2b2. Obtain the force law f=f(r).
pf2

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THEORETICAL DYNAMICS — PHY–

HOMEWORK 9

(October 20, 2002) Due on Monday, October 29, 2002

PROBLEM 25

Imagine yourself being Kepler around the year 1610 and having compiled information on the motion of all the planets you decide to make a table that includes: a) the name of the planet, b) the period of revolution of the planet around the Sun (in years), c) the average distance (or semi-major axis) from the planet to the Sun (in A.U.), and d) the ratio of the period square to the average distance cubed. After having found this amazing correlation (Kepler’s third law) compute the mass of the Sun. Although not yet discover at the time, you may use Newton’s Law of Universal gravitation with G = 6. 673 × 10 −^11 m^3 kg−^1 s−^2.

PROBLEM 26

a) Starting from Euler-Lagrange’s equation of motion for the radial motion of a particle of mass m moving in a central potential, i.e., mr¨ = −V (^) eff′ (r), obtain the differential equation for the orbit:

d^2 u dθ^2

  • u = −

m l^2

f (1/u) u^2

where u ≡ 1 /r and f (r) = −V ′(r). The above equation suggests how to obtain the orbit of the particle r = r(θ) if the force law f = f (r) is known. Conversely, if the orbit is known, one can deduce the force law.

b) Consider the equation of the orbit in Cartesian coordinates:

x^2 a^2

y^2 b^2

Obtain the force law f = f (r).

c) Consider the equation of the orbit in Cartesian coordinates:

(x − c)^2 a^2

y^2 b^2

where c =

a^2 − b^2. Obtain the force law f = f (r).

PROBLEM 27

A particle of mass m = 1 moves under the influence of a gravitational (Kepler) potential of the form: V (r) = −k/r ; k > 0.

At time t = 0 the particle is located at a distance of r 0 = 1 and makes an angle of 45◦ relative to the horizontal. The initial velocity of the particle is equal v 0 =

2 and is directed at angle of 210◦^ (or 30◦) as indicated in the figure.

a) In terms of the initial conditions, compute the energy and angular momentum of the particle. What kind of orbit will the particle describe? Compute the classical turning point(s).

b) Make a plot of the orbit r = r(θ).

c) Make a plot of r and ˙r as a function of time for 0 ≤ t ≤ 1.

d) Make a plot of θ and θ˙ as a function of time for 0 ≤ t ≤ 1.

Hint: You may compute the above quantities any way you want. I obtained them by solving the Euler-Lagrange’s equations of motion for r(t) and θ(t) from t = 0 up to t = 1 using finite-difference equations. If you find yourself in trouble, come to see me!

v 0 r 0

x

y

45 deg

Sun

30 deg