AE 502
spring 2007
All Classes
Advanced Orbital Mechanics
Credit: 4 hours.
Circular restricted three body problem; surfaces of zero velocity, libration points, halo orbits; perturbed two body motion; Gauss and Lagrange planetary equations, Hamilton's principle, canonical equations and the Delaunay variables, application to artificial Earth satellites; orbit determination. Prerequisite: AE 402.
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