Optimizing Orbital Maneuvers Based on Time and Fuel Constraints

By Isaac Poplin, Aerospace Engineering; Emily Farmer, Aerospace Engineering; Steven Levasseur, Computer Engineering Advisor: Cedrick Kwuimy Presentation ID: PM_D28 Abstract: Currently, it requires many complicated math calculations to determine the most efficient orbital transfer maneuvers. We would like to design a program that autonomously concludes the optimal route for spacecraft from Earth to various destinations in the solar system at any given time based upon time, fuel consumption, and safety considerations.