This paper presents the Hardware-In-The-Loop testing of a multi-sensor relative navigation module enabling close-proximity operations toward passively cooperative space targets in the frame of On-Orbit Servicing missions. The module, which is designed according to the CubeSat standard to occupy two CubeSat units, consists of a monocular camera and a wide-field-of-view laser range finder, and exploits a sensor fusion logic to provide relative position and attitude (pose) estimates. A laboratory setup is conceived and realized to characterize the pose estimation performance of the module by providing a highly accurate benchmark. Experimental tests show that the module is able to measure its relative position and attitude with respect to a target at operative distances below 2 meters with millimeter and tenths-of-degree level accuracy, respectively. Further tests on a larger-scale trajectory in an uncontrolled environment (in terms of illumination conditions and reference pose solution) demonstrate the capability to perform pose estimation up to operative distances of about 9 meters from the target, keeping reprojection errors at sub-centimeter level, and collecting reliable range finder measurements up to 30 m.
Experimental Assessment of a Visual-Laser Relative Navigation Module for CubeSats / Napolano, Giuseppe; Vela, Claudio; Nocerino, Alessia; Opromolla, Roberto; Grassi, Michele; Amoruso, Salvatore; Di Donfrancesco, Guido. - (2023), pp. 464-469. (Intervento presentato al convegno 2023 IEEE 10th International Workshop on Metrology for AeroSpace (MetroAeroSpace) tenutosi a Milan, Italy nel 19-21 June 2023) [10.1109/MetroAeroSpace57412.2023.10189939].
Experimental Assessment of a Visual-Laser Relative Navigation Module for CubeSats
Giuseppe Napolano;Claudio Vela;Alessia Nocerino;Roberto Opromolla;Michele Grassi;Salvatore Amoruso;
2023
Abstract
This paper presents the Hardware-In-The-Loop testing of a multi-sensor relative navigation module enabling close-proximity operations toward passively cooperative space targets in the frame of On-Orbit Servicing missions. The module, which is designed according to the CubeSat standard to occupy two CubeSat units, consists of a monocular camera and a wide-field-of-view laser range finder, and exploits a sensor fusion logic to provide relative position and attitude (pose) estimates. A laboratory setup is conceived and realized to characterize the pose estimation performance of the module by providing a highly accurate benchmark. Experimental tests show that the module is able to measure its relative position and attitude with respect to a target at operative distances below 2 meters with millimeter and tenths-of-degree level accuracy, respectively. Further tests on a larger-scale trajectory in an uncontrolled environment (in terms of illumination conditions and reference pose solution) demonstrate the capability to perform pose estimation up to operative distances of about 9 meters from the target, keeping reprojection errors at sub-centimeter level, and collecting reliable range finder measurements up to 30 m.I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.