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Course: |
EA362 |
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Title: |
ASTRODYNAMICS I |
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Credits: |
3-0-3 |
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Description: |
Introduction to the principles of planetary and satellite motion. Topics include the classical two-body problem, orbital parameters, orbit determination and maneuvers, remote sensing geometry, types of orbits and their uses, constellation design, orbit changes, perturbations and atmospheric drag effects, rendezvous, ballistic missile trajectories, and lunar and interplanetary travel.
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Offered: |
Spring 2012-2013 |
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Requisites: |
Prereq: EA204.
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