1. Attitude Dynamics and Control of a Spacecraft Using Shifting Mass Distribution Open Access Author: Ahn, Young Tae Title: Attitude Dynamics and Control of a Spacecraft Using Shifting Mass Distribution Graduate Program: Aerospace Engineering Keywords: spacecraft attitude dynamicsattitude controlcombinatorial optimization theory File: Download youngtaeahn_dissertation.pdf Committee Members: David Bradley Spencer, Dissertation Advisor/Co-AdvisorRobert Graham Melton, Committee MemberSven G Bilen, Committee MemberChristopher Rahn, Committee Member