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Aerospace Engineering
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Orbital Mechanics
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Lambert's Problem
Lambert's Problem
Determines the unique conic section connecting two points in space (
r
⃗
1
,
r
⃗
2
\vec{r}_1, \vec{r}_2
r
1
,
r
2
) over a specified time of flight (
Δ
t
\Delta t
Δ
t
), given the central body's gravity.