Deriving equation 7.27 from the orbit equation

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Homework Statement


Diagram of an elliptical orbit with the auxiliary circle, marking center C, focus F, point N, planet P, angles psi and theta, and semi-major axis a with distance r; below is printed equation (1 - e cos psi)(1 + e cos theta) = b^2/a^2 (7.27) boxed in red.


Homework Equations


1/r = a/b2 * (1+e cosθ)

The Attempt at a Solution


How do you derive 7.27?
I tried to substitute r in the orbit equation by (acosψ - ae) / cosθ and got
(cos ψ - e)/cosθ*(1+e cosθ)=b^2/a^2 I don't know what to do next. Please help, thank you.
 
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  • Diagram of an elliptical orbit with the auxiliary circle, marking center C, focus F, point N, planet P, angles psi and theta, and semi-major axis a with distance r; below is printed equation (1 - e cos psi)(1 + e cos theta) = b^2/a^2 (7.27) boxed in red.
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Clara Chung said:
(cos ψ - e)/cosθ*(1+e cosθ)=b^2/a^2
I believe this is OK. You just need to manipulate it to get (7.27). I don't know the quickest way, but I found something that works. I don't want to give too much away.
Rearrange your equation as (cos ψ - e)*(1+e cosθ)=(b^2/a^2)*cosθ. Substitute for b^2/a^2 in terms of e. Multiply everything out and see if you can get to the result.
 
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I tried hard by substituting (b^2/a^2) but still can't figure out the equation... Then I changed my mind to substitute for e. Thank you so much.
(cos ψ - e)*(1+e cosθ)=(b^2/a^2)*cosθ

(ecos ψ - 1+b^2/a^2)*(1+e cosθ)=(b^2/a^2)*cosθ*e

-(1-ecosψ)(1+ecosθ)+(b^2/a^2)e cosθ+(b^2/a^2)=(b^2/a^2)*cosθ*e

(1-ecosψ)(1+ecosθ)=(b^2/a^2)
 
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