Autonomous station keeping for LEO missions with a hybrid continuous-impulsive electric propulsion system A. Garulli, A. Giannitrapani, M. Leomanni, F. Scortecci Sep 1, 2011 PDF Cite Aerospace applications Related Comparison of EKF and UKF for spacecraft localization via angle measurements Autonomous Low-Earth-Orbit station-keeping with electric propulsion An MPC-based attitude control system for all-electric spacecraft with on/off actuators Precise attitude control of all-electric GEO spacecraft using Xenon microthrusters Minimum switching limit cycle oscillations for systems of coupled double integrators