Gravity Assist-Elliptical Trajectories

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The discussion focuses on the mathematical relationship in the JPL technical report regarding gravity assists and elliptical trajectories. A critical error in the equation is identified, specifically the omission of the term (r2)² within the square root. This missing term is essential for accurately applying the triangular inequality, which states that r1' and r2' must exceed the distance between points P1 and P2, calculable through r1, r2, and the angle θ using the law of cosines.

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rpthomps
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Good evening,

I am working my way through a JPL technical report I found online at

link

Specifically, I am at page 17 which looks like

1tM3dJ0.png


and I am trying to understand the relation

G7cVWTH.png


I basically, don't understand where this relationship comes from and why it is necessary.

Any help would be appreciated.

Ryan
 
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Well, there is a mistake in that equation. There should be another term inside the square root. The missing term is (r2)2. That triangular inequality simply expresses that r1' and r2' must add to something larger than the distance between P1 and P2 which can be found from r1, r2, and θ by use of the law of cosines.
 
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Thanks Dauto
 

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