The paper focuses on guidance and relative navigation aspects in the framework of an Active Debris Removal mission. Specifically, an original multi-step strategy, inspired by the one designed for the OSAM-1 mission, is proposed to perform rendezvous toward an uncooperative target reaching a relative distance suitable for monitoring using Electro-Optical sensors. At each step, passive safety is guaranteed by setting pre-defined regions of interest that cannot be breached by the chaser until the mission control on ground provides an Authority-to-Proceed command. As regards the navigation aspects, particular attention is paid to the problem of obtaining highly accurate relative state estimates in close-proximity conditions using a LIDAR. Finally, an ad-hoc reconfiguration strategy is proposed to keep the chaser within a limited along-track distance from the target. The reconfiguration manoeuvre is commanded on the basis of the LIDAR-based relative state estimates. Performance assessment is carried out by means of numerical simulations.
Analysis of manoeuvring strategies and relative navigation for multi-step rendezvous toward uncooperative target / Nocerino, Alessia; Cimmino, Nicola; Opromolla, Roberto; Fasano, Giancarmine; Grassi, Michele. - (2020). (Intervento presentato al convegno 71st International Astronautical Congress, IAC 2020 tenutosi a Virtuale nel 12 - 14 Ottobre 2020).
Analysis of manoeuvring strategies and relative navigation for multi-step rendezvous toward uncooperative target
Alessia Nocerino;Nicola Cimmino;Roberto Opromolla;Giancarmine Fasano;Michele Grassi
2020
Abstract
The paper focuses on guidance and relative navigation aspects in the framework of an Active Debris Removal mission. Specifically, an original multi-step strategy, inspired by the one designed for the OSAM-1 mission, is proposed to perform rendezvous toward an uncooperative target reaching a relative distance suitable for monitoring using Electro-Optical sensors. At each step, passive safety is guaranteed by setting pre-defined regions of interest that cannot be breached by the chaser until the mission control on ground provides an Authority-to-Proceed command. As regards the navigation aspects, particular attention is paid to the problem of obtaining highly accurate relative state estimates in close-proximity conditions using a LIDAR. Finally, an ad-hoc reconfiguration strategy is proposed to keep the chaser within a limited along-track distance from the target. The reconfiguration manoeuvre is commanded on the basis of the LIDAR-based relative state estimates. Performance assessment is carried out by means of numerical simulations.I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.