1. Effective Use of an Analytical Approximation for the Relative Motion of Spacecraft on Hyperbolic Trajectories Open Access Author: Stueck, Clifford Title: Effective Use of an Analytical Approximation for the Relative Motion of Spacecraft on Hyperbolic Trajectories Graduate Program: Aerospace Engineering Keywords: Hyperbolic OrbitsRelative MotionLagrange ExpansionAnalytical Model File: Download Clifford_Stueck_Master_s_Thesis.pdf Committee Members: Robert G. Melton, Thesis Advisor/Co-AdvisorPuneet Singla, Committee MemberAmy Pritchett, Program Head/ChairDaning Huang, Committee Member
