1. Halo Orbit Design In The Circular Restricted Three-Body Problem Using Differential Evolution Open Access Author: Small, Jeffrey Title: Halo Orbit Design In The Circular Restricted Three-Body Problem Using Differential Evolution Graduate Program: Aerospace Engineering Keywords: Halo OrbitsCR3BPDifferential Evolution File: Download JeffreySmall_MsThesis.pdf Committee Members: Robert Graham Melton, Thesis Advisor/Co-Advisor
