AERO 654 Astrodynamics and Mission Analysis
This course elaborates the fundamental concepts of spaceflight orbital mechanics and introduces trajectory design for planet-centered and interplanetary missions. It starts with a short review of the two-body problem and introduces the design and characterization of planet-centered orbits in the presence of perturbations and related orbit transfer maneuvers. It provides the link between mission requirements and orbit planning. Then, it focuses on interplanetary trajectory design and gravity assist maneuvers. Eventually, it introduces to concepts of dynamical system theory applied to missions to and around the libration points of the circular restricted three-body problem and to trajectory design with low-thrust propulsion.
Prerequisite
AERO650
Offered
Fall Spring