| Automatic mass balancing of a spacecraft three-axis simulator: Analysis and experimentation S Chesi, Q Gong, V Pellegrini, R Cristi, M Romano Journal of Guidance, Control, and Dynamics 37 (1), 197-206, 2014 | 81 | 2014 |
| A dynamic, hardware-in-the-loop, three-axis simulator of spacecraft attitude maneuvering with nanosatellite dimensions S Chesi, O Perez, M Romano Journal of Small Satellites 4 (1), 315-328, 2015 | 56 | 2015 |
| Aerodynamic three-axis attitude stabilization of a spacecraft by center-of-mass shifting S Chesi, Q Gong, M Romano Journal of guidance, control, and dynamics 40 (7), 1613-1626, 2017 | 45 | 2017 |
| CubeSat three axis simulator (CubeTAS) H Woo, O Rico, S Chesi, M Romano AIAA Modeling and Simulation Technologies Conference, 6271, 2011 | 24 | 2011 |
| PICASSO: a state of the art CubeSat B Mero, KA Quillien, M McRobb, S Chesi, R Marshall, A Gow, C Clark, ... | 17 | 2015 |
| Adcs at scale: Calibrating and monitoring the dove constellation L Leung, V Beukelaers, S Chesi, H Yoon, D Walker, J Egbert | 15 | 2018 |
| Attitude control of nanosatellites using shifting masses S Chesi University of California, Santa Cruz, 2015 | 12 | 2015 |
| Satellite attitude control by center-of-mass shifting S Chesi, Q Gong, M Romano Advances in the Astronautical Sciences 150, 2575-2594, 2014 | 5 | 2014 |
| Angularly unbounded three-axis spacecraft simulator S Chesi, M Romano US Patent 10,621,883, 2020 | 2 | 2020 |
| Automatic Mass Balancing for Small Three-Axis Spacecraft Simulator Using Sliding Masses S Chesi, V Pellegrini, Q Gong, R Cristi, M Romano Advances in the Astronautical Sciences, 142, 2547-2562, 2012 | 1 | 2012 |
| A 4-PI steradians dynamic three-axis simulator for satellite hardware-in-the-loop experiments M Romano, S Chesi | | 2013 |
