Precise attitude control of all-electric GEO spacecraft using Xenon microthrusters M. Leomanni, A. Garulli, A. Giannitrapani, F. Scortecci Oct 1, 2013 PDF Cite Aerospace applications Related 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 Nonlinear orbit control with longitude tracking