For reliable verification of attitude determination and control systems, ground-based hardware-in-the-loop simulations are strongly desirable. To this end, a Three-Degrees of Freedom Dynamic Testbed for CubeSats has been developed at the University of Bologna. In this paper, the development of a platform for 1U CubeSats testing is described. Within the facility, disturbance-free environment is guaranteed and a magnetic field is generated by a Helmholtz cage to enable experimental verification of magnetic attitude control systems. A COTS CubeSat mockup is integrated and employed to test detumbling, spin-axis pointing and three-axis attitude control laws relying on magnetorquers only. The experimental results show the facility capabilities in highly demanding magnetic attitude control scenarios.
On-ground experimental verification of magnetic attitude control for nanosatellites / Bahu, Anton; Modenini, Dario. - ELETTRONICO. - (2021), pp. 568-573. (Intervento presentato al convegno 2021 IEEE 8th International Workshop on Metrology for AeroSpace (MetroAeroSpace) tenutosi a Naples, Italy nel 23-25 June 2021) [10.1109/MetroAeroSpace51421.2021.9511720].
On-ground experimental verification of magnetic attitude control for nanosatellites
Bahu, Anton
;Modenini, Dario
2021
Abstract
For reliable verification of attitude determination and control systems, ground-based hardware-in-the-loop simulations are strongly desirable. To this end, a Three-Degrees of Freedom Dynamic Testbed for CubeSats has been developed at the University of Bologna. In this paper, the development of a platform for 1U CubeSats testing is described. Within the facility, disturbance-free environment is guaranteed and a magnetic field is generated by a Helmholtz cage to enable experimental verification of magnetic attitude control systems. A COTS CubeSat mockup is integrated and employed to test detumbling, spin-axis pointing and three-axis attitude control laws relying on magnetorquers only. The experimental results show the facility capabilities in highly demanding magnetic attitude control scenarios.I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.