AAE 63200 - Advanced Orbital Dynamics

Credit Hours: 3.00. Discussion of more advanced concepts in astrodynamics. Includes fundamental theories from celestial mechanics, as well as trajectory determination and perturbation analysis with application to the motion of Earth-orbiting and interplanetary spacecraft. Assumes experience with the two-body problem. Offered in alternate years. Prerequisite: AAE 50700, AAE 53200. Credits: 3.00