Research interests include leveraging dynamical systems techniques to explore multi-body systems, thereby enabling rapid and well-informed trajectory design and optimization for both large spacecraft and small satellites, as well as the analysis of natural celestial bodies.
keywords
Spacecraft Trajectory Design and Optimization, Dynamical Systems Theory, Mission Design, CubeSats
ASEN 3200 - Orbital Mechanics/Attitude Dynamics and Control
Primary Instructor
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Spring 2018 / Spring 2019
Presents the fundamentals of orbital mechanics, 3D rigid body dynamics and satellite attitude dynamics and controls. Offered spring only.
ASEN 5050 - Space Flight Dynamics
Primary Instructor
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Fall 2018 / Fall 2019
Includes celestial mechanics, space navigation, and orbit determination; trajectory design and mission analysis trajectory requirements; and orbital transfer and rendezvous. Recommended prerequisite: ASEN 3200 or equivalent or instructor consent required.
