AE 4700 - Orbital Mechanics

Introduction to astrodynamics, including the two-body problem and restricted three-body problem, orbital trajectories, transfers and targeting, and orbit determination. Computer modeling and simulation of orbital trajectories.

Prerequisites & Corequisites: Prerequisite: ME 2580, with a grade of “C” or better.

Credits: 3 hours

Restrictions: Restricted to majors in aerospace engineering.