AE 502

Spring 2012 Part of Term 1

Part of Term 1
Jan 17-May 2

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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AE 502 class schedule data for spring 2012
CRN Type Section Time Day Location Instructor Section Details
39827
Lecture-Discussion
A
9:00AM -9:50AM
MWF
Talbot Laboratory
Conway, B
Part of Term:
1
Date Range:
01/17/12-05/02/12
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