Prerequisite: ENAE404; or permission of ENGR-Aerospace Engineering department. Mathematics and applications of orbit theory, building upon the foundations developed in ENAE 404 and ENAE 441. Topics include two body orbits, solutions of Kepler's equation, the two-point boundary value problem, rendezvous techniques, and Encke's method.
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Average GPA: 3.26 between 136 students
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