AE 502
spring 2021
All Classes
Advanced Orbital Mechanics
Credit: 4 hours.
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.
Prerequisite: AE 402.
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