An MPC-based attitude control system for all-electric spacecraft with on/off actuators M. Leomanni, A. Garulli, A. Giannitrapani, F. Scortecci Dec 1, 2013 PDF Cite Aerospace applications Related Precise attitude control of all-electric GEO spacecraft using Xenon microthrusters Minimum switching limit cycle oscillations for systems of coupled double integrators SSCAM: Micro-satellite platform for Earth observation Minimum switching control for spacecraft precision pointing with on/off actuators Propulsion options for station-keeping of small LEO satellites