Orbital Mechanics
Texas A & M University-College Station
CourseAERO 423
Two-body problem, restricted three-body problem, orbital perturbations, orbital maneuvers, interplanetary trajectories, orbit determination and other selected topics.
Credits
3 credits
Course Code
AERO 423
Related Courses
Prerequisites, corequisites, and courses that build on this one
Required For
Courses that require this course as a prerequisite