Astrophysics - elliptical orbit proof help.

In summary, the equation for an ellipse with its origin at the center and its x-axis along the major axis is x^2/a^2 + y^2/b^2 =1, where a and b are the lengths of the semi-major and semi-minor axes. Using this equation, it can be proven that the area of an ellipse is given by A = πab. To find the area, one can solve for y and then integrate using trigonometric substitution.
  • #1
Kiwithepike
16
0
A.)
Assume a rectangular coord system has its origin at the center of an elliptical planetary orbit and that the coord system x-axis lies along the major axis of the ellipse. Show that the equation for the ellipse is given by x^2/a^2 + y^2/b^2 =1.
where a and b are the lengths if the semi-major axis and the semi-minor axis, respectively.

b.)
using the results from a, prove the area of an ellipse is given by A=(pi)ab.

Im am completely lost right now. Any ideas?
 
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  • #2
For starters, what facts do you know about an ellipse that you could use in the proof?
 
  • #3
(x-h)^2/a^2 + y-k)^2/b^2=1

c^2= a^2 -b^2

while a ≥b>0
 
  • #4
OK, well for part a, for the ellipse in question, what would h and k be?
 
  • #5
zero, so (x-h)^2 = x^2 and (y-k)^2= y^2 right?
 
  • #6
Right, so that part's done. (Although it seems really simple, are you sure you can use that equation as a starting point?)

Now what about part b? How could you find area?
 
  • #7
thats what the text tell you to use. That does seem really simple, maybe that's why I am so lost.

B) i know the area A=piab
so the way i was looking at it
solve for y? then integrate it, with trig sub get pi ab?
 
  • #8
Yep, sounds like you're on the right track with that. (Obviously make sure you actually do it to verify that you get the right answer)
 
  • #9
Thank you so much for your help
 

1. What is an elliptical orbit?

An elliptical orbit is a type of orbit where an object, such as a planet or satellite, follows a path that is shaped like an ellipse. This means that the distance between the object and the object it is orbiting around varies throughout the orbit, with the closest point being the perihelion and the farthest point being the aphelion.

2. How do we know that planets follow elliptical orbits?

In the 1600s, Johannes Kepler observed and studied the orbits of planets, particularly Mars, and discovered that they followed an elliptical path. Later, Isaac Newton developed his laws of motion and universal gravitation, which provided a mathematical explanation for why planets follow elliptical orbits.

3. What is the proof that an elliptical orbit is stable?

The stability of an elliptical orbit is based on the conservation of energy and angular momentum. As long as there are no external forces acting on the orbiting object, its energy and angular momentum will remain constant, keeping the object on its elliptical path.

4. How does an object's speed vary in an elliptical orbit?

In an elliptical orbit, an object's speed varies based on its distance from the object it is orbiting. When the object is closer, it will move faster due to the stronger gravitational pull, and when it is farther away, it will move slower due to the weaker gravitational pull.

5. Can objects in the universe have other types of orbits besides elliptical?

Yes, objects in the universe can have a variety of orbit types, including circular, parabolic, and hyperbolic orbits. The type of orbit depends on the object's initial velocity and the strength of the gravitational pull from other objects in the system.

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