Propulsion options for very low Earth orbit microsatellites M. Leomanni, A. Garulli, A. Giannitrapani, F. Scortecci Jan 1, 2017 PDF Cite DOI Aerospace applications Related Minimum switching thruster control for spacecraft precision pointing A class of globally stabilizing feedback controllers for the orbital rendezvous problem State feedback control in equinoctial variables for orbit phasing applications Sum-of-Norms model predictive control for spacecraft maneuvering An adaptive groundtrack maintenance scheme for spacecraft with electric propulsion