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AE 502 - Advanced Orbital Mechanics

Spring 2021

Official Description

Circular-restricted three-body problem; surfaces of zero velocity, libration points, and halo orbits; perturbed two-body motion; Gauss and Lagrange planetary equations, Hamilton's principle, canonical equations and Delaunay variables; application to artificial Earth satellites; orbit determination. Course Information: Prerequisite: AE 402.

Related Faculty

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