The course covers the natural dynamics of objects under gravity, including orbits in the two-body problem and the three-body problem. Fundamental topics for astrodynamics cover Lagrange functions, Lambert’s theorem, and patched conics. Application in trajectory design includes orbital maneuvers/transfers and interplanetary orbits. Mission design software will be used to model orbit and trajectory. Students cannot receive credit for this course if they have taken AE 5093 “Special Topics: Orbital Mechanics”.
Recommended Background
Strong knowledge of dynamics and control, differential equations, and linear algebra (AE 2310, ES 2503, MA 2051, MA 2071, or equivalent). Strong MATLAB programming skills.