Optimizing Orbital Maneuvers Based on Time and Fuel Constraints

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Isaac Poplin Emily Farmer Steven Levasseur Cedrick Kwuimy


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.

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PM Poster Session -- Great Hall -- D: New Frontiers