Geoff Schwindt
Footnot 18 Project
2:40 MWF
Kepler's Laws of Planetary Motion
In 1605, Johannes Kepler who had been studying the precise observations of the planets as calculated by Tycho Brahe discovered that the orbits of the planets followed three mathematic rules. Though he was unable to show why these rules behaved as they did, he was able to extrapolate them from Brahe's data. When Isaac Newton invented calculus, he was able to derive the formulas regulating the motion of the planets from his own laws of motion and gravitation.
Kepler's three laws are:
The orbit of every planet is an ellipse with the sun at one foci;
A line joining a planet and the sun sweeps out in equal areas in equal times;
The ratio of the squares of the revolutionary periods for two planets is equal to the ratio of the cubes of their semimajor axes.
Proof 2:
The
angular momentum equation is: ![]()
so ![]()
![]()
![]()
A vector crossed with itself is 0, and the book establishes that rXa is also equal to 0
![]()
Therefore, by integrating, L is equal to a constant.
The
change in area of the triangular area between two vectors r (radius)
and v (angular momentum) region is:
where
r goes from time t=t1 to t=t2
However,
![]()
Substituting
into the area function, we find that ![]()
Since we
have established that L is a constant and m is also a constant,
is constant, so with an equal change in time the area swept out by
the position vector of the planet will be constant, proving Kepler's
second law.
Kepler's Third Law
Following
from Kepler's Second Law, multiplying both sides by dt gives us ![]()
Integrating
both sides with respect to their variables gives us ![]()
Squaring
both sides we find that ![]()
Solving
for t^2 we find that ![]()
The area
of an ellipse is equal to
where
a is the length of the semimajor axis and b is the length of the
semiminor axis
So ![]()
And
where
c is the distance between a foci and the center of the ellipse
So ![]()
where
is
the eccentricity of the ellipse.
So ![]()
So ![]()
The
equation for the angular momentum can be rewritten as
![]()
From
the book we know that
,
a constant vector. So
Solving
for m and squaring both sides we find that
![]()
Substituting
this in we find that

This
reduces to
![]()
Using
a property of ellipses we can say that
where
p is the directrix
![]()
So

so
![]()
From
the book we know that
where
G is the universal gravitational constant and M is the mass of the
sun.
So
![]()
Canceling the h's and solving for c leaves us with
![]()
Substituting
that into the equation gives us

Simplifying
gives us
![]()
Since G and M are constants, this proves Kepler's third law that the square of the period of revolution is proportional to the cube of its major axis.
Using Kepler's 3rd Law and inputting the given data we get that
![]()
Using Maple's solve command for a, we find that that a is equal to ![]()
To find this, the satellite must have a period of revolution equal to one day, therefore
![]()
Solving for a in Maple gives us
but
we must subtract the radius of the Earth,
This
leaves us with a final altitude of
above
the earth.
Reference - MAT294, Calculus III, Fall 2006 - Henry Braun, "Kepler's Laws"