Precision formation flying and spacecraft pointing for swarm mission concepts requires micropropulsion technologies and robust control solutions. Plasmonic force propulsion can provide nanonewton levels of thrust with which some spacecraft control can be realized. This study considers the feasibility of providing precision pointing and orbit control using an array of plasmonic force thruster configurations within the constraints of system level design requirements of the CubeSat platform (with applicability to micro/nano/pico-satellites in general). Results show that pointing and relative position can be maintained for a range of swarm precision formation flight missions.