How Do You Calculate the Area of an Ellipse from Pericenter to Pi/2?

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SUMMARY

The discussion focuses on calculating the area of an ellipse from the pericenter to π/2 using orbital mechanics principles. The relevant orbit equation is r = p/(1 + e*cos(θ), where p is the semi-latus rectum and e is the eccentricity. The area is determined through the integral A = 1/2 * ∫(r^2 dθ) from 0 to π/2. The solution involves converting to Cartesian coordinates and applying the ellipse equation x²/a² + y²/b² = 1, along with the derived semi-major and semi-minor axes.

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Homework Statement



I have an orbital mechanics problem, in which I need to find the area of the ellipse from pericenter to pi/2 (semi-latus rectum location).


Homework Equations



So I have the orbit equation
r = p/(1+e*cos(theta)) where the origin is at the focus. So I know that A = integral( 1/2 * r^2 * d_theta) from 0-> pi/2.


The Attempt at a Solution



The problem is when plugging in r I can't integrate it. I need to account for the fact that 0=<e=<1 also. I have read many many other posts and searched on this topic but haven't found a concise answer.


Thanks for the help!
 
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I know it may sound unintuitive, by you might want to try performing the integration in a Cartesian form.

Given a semi-latus rectum p and eccentricity e, the semi major and minor axes are:

a = p/(1 - e2) and b = sqrt(ap)

The distance from the center of the ellipse to the focus is sqrt(a2 - b2).

The equation of the ellipse in Cartesian form is x2/a2 + y2/b2 = 1 .

Then follow the example shown http://math.ucsd.edu/~wgarner/math10b/area_ellipse.htm" with the appropriate domain for x.
 
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