AE 502
spring 2005
All Classes
Advanced Orbital Mechanics
Credit: 4 hours.
(A A E 406) 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 or equivalent.
- Section Status Closed
- Section Status Open
- Section Status Pending
- Section Status Open (Restricted)
- Section Status Unknown
Section Status updates every 10 minutes.
| Detail | Status | CRN | Type | Section | Time | Day | Location | Instructor |
|---|