ECE 5810 - Astrodynamics

A course in celestial dynamics as applied to space travel. Students will learn the basics of satellite orbit definition, determination, and navigation. While the general n- body problem will be taken up, the emphasis will be placed on the calculation of geocentric and heliocentric orbits. The primary application will be satellite systems as applied to the Global Positioning System. This course is cross-listed with ME 5810.

Prerequisites & Corequisites: Prerequisite: CENM, EENM, or ELCD admission.

Credits: 3 hours
Lab Hours: (3 to 0)