Ground tests play a key role in verifying many critical aspects of a spacecraft mission, even within the current trend of high fidelity simulation tools. In fact numerical runs of complex maneuvers still need some realistic indications of the expected system’s behaviour to better define model assumptions. To this aim different test-beds have been recently built at the Guidance and Navigation Laboratory of Sapienza - Università di Roma. They share, for reasons of costs and complexity, the limitation of a bi-dimensional representation of the space gravity-less environment. Nevertheless, they allowed to better investigate complex dynamics’ phenomena typical to space activities, and a number of interesting indications have been provided by these experimental tests. Among the different realizations there are robotic arms equipped with different endeffectors, a self-standing floating platform representing a spacecraft bus (also able to perform rendezvous or re-orientation manoeuvres) and a scaled simulator for image-based navigated and controlled formation-flying. The paper is intended to present the main characteristics of these test-beds and to discuss their performance and the related research activities.

A testbed for small satellites technologies / Sabatini, Marco; Gasbarri, Paolo; Palmerini, Giovanni Battista. - STAMPA. - Vol.2 N.4:(2016), pp. 637-652. (Intervento presentato al convegno 3rd IAA conference on University Satellite Missions and Cubesat Workshop tenutosi a Rome nel November 30th- December 5th, 2015).

A testbed for small satellites technologies

SABATINI, MARCO;GASBARRI, Paolo;PALMERINI, Giovanni Battista
2016

Abstract

Ground tests play a key role in verifying many critical aspects of a spacecraft mission, even within the current trend of high fidelity simulation tools. In fact numerical runs of complex maneuvers still need some realistic indications of the expected system’s behaviour to better define model assumptions. To this aim different test-beds have been recently built at the Guidance and Navigation Laboratory of Sapienza - Università di Roma. They share, for reasons of costs and complexity, the limitation of a bi-dimensional representation of the space gravity-less environment. Nevertheless, they allowed to better investigate complex dynamics’ phenomena typical to space activities, and a number of interesting indications have been provided by these experimental tests. Among the different realizations there are robotic arms equipped with different endeffectors, a self-standing floating platform representing a spacecraft bus (also able to perform rendezvous or re-orientation manoeuvres) and a scaled simulator for image-based navigated and controlled formation-flying. The paper is intended to present the main characteristics of these test-beds and to discuss their performance and the related research activities.
2016
3rd IAA conference on University Satellite Missions and Cubesat Workshop
Floating platform, air bearing, robotic arm, visual navigation, control
04 Pubblicazione in atti di convegno::04b Atto di convegno in volume
A testbed for small satellites technologies / Sabatini, Marco; Gasbarri, Paolo; Palmerini, Giovanni Battista. - STAMPA. - Vol.2 N.4:(2016), pp. 637-652. (Intervento presentato al convegno 3rd IAA conference on University Satellite Missions and Cubesat Workshop tenutosi a Rome nel November 30th- December 5th, 2015).
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11573/953433
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