This paper presents a fully Automatic Collision Avoidance System (ACAS) for unmanned aerial vehicles. This system has been developed by the Italian Aerospace Research Center (CIRA) in collaboration with the department of Aerospace Engineering of the University of Naples “Federico II”, in the framework of the national funded research project TECVOL (Technologies for the Autonomous Flight). The proposed system is comprised of the two subsystems: the Obstacle Detection and Tracking subsystem, which permits to reveal flying intruders in a selected field of regard and to estimate their motion; the Collision Avoidance subsystem, which provides conflict detection and resolution capabilities, addressed in a 3D environment using information about current position and instantaneous speed vectors. Even if the sense and avoid system here proposed has been mainly developed for Unmanned Aerial Systems (UAS), where high automation levels are required, it can be also successfully applied in manned commercial aircraft, as an aid to pilots. The effectiveness of the system has been demonstrated during a flight test campaign, where proper conflict scenarios have been considered. In fact, the proposed ACAS setup was installed onboard a very light aircraft named FLARE (Flight Laboratory for Aeronautical Research), which has been customized with automatic flight capabilities. In the paper first the system and the developed algorithms are described, then some relevant results obtained from the flight test campaign, demonstrating the reliability and the efficiency of the developed system, are presented and discussed.

Automatic Collision Avoidance System: Design, Development and Flight tests / Luongo, Salvatore; V., Di Vito; Fasano, Giancarmine; Accardo, Domenico; Forlenza, Lidia; Moccia, Antonio. - ELETTRONICO. - (2011), pp. 5C1-1-5C1-10. (Intervento presentato al convegno 30th DASC - Digital Avionics Systems Conference - AIAA - IEEE tenutosi a Seattle, WA, USA nel 16-20 October 2011) [10.1109/DASC.2011.6096080].

Automatic Collision Avoidance System: Design, Development and Flight tests

LUONGO, SALVATORE;FASANO, GIANCARMINE;ACCARDO, DOMENICO;FORLENZA, LIDIA;MOCCIA, ANTONIO
2011

Abstract

This paper presents a fully Automatic Collision Avoidance System (ACAS) for unmanned aerial vehicles. This system has been developed by the Italian Aerospace Research Center (CIRA) in collaboration with the department of Aerospace Engineering of the University of Naples “Federico II”, in the framework of the national funded research project TECVOL (Technologies for the Autonomous Flight). The proposed system is comprised of the two subsystems: the Obstacle Detection and Tracking subsystem, which permits to reveal flying intruders in a selected field of regard and to estimate their motion; the Collision Avoidance subsystem, which provides conflict detection and resolution capabilities, addressed in a 3D environment using information about current position and instantaneous speed vectors. Even if the sense and avoid system here proposed has been mainly developed for Unmanned Aerial Systems (UAS), where high automation levels are required, it can be also successfully applied in manned commercial aircraft, as an aid to pilots. The effectiveness of the system has been demonstrated during a flight test campaign, where proper conflict scenarios have been considered. In fact, the proposed ACAS setup was installed onboard a very light aircraft named FLARE (Flight Laboratory for Aeronautical Research), which has been customized with automatic flight capabilities. In the paper first the system and the developed algorithms are described, then some relevant results obtained from the flight test campaign, demonstrating the reliability and the efficiency of the developed system, are presented and discussed.
2011
9781612847979
Automatic Collision Avoidance System: Design, Development and Flight tests / Luongo, Salvatore; V., Di Vito; Fasano, Giancarmine; Accardo, Domenico; Forlenza, Lidia; Moccia, Antonio. - ELETTRONICO. - (2011), pp. 5C1-1-5C1-10. (Intervento presentato al convegno 30th DASC - Digital Avionics Systems Conference - AIAA - IEEE tenutosi a Seattle, WA, USA nel 16-20 October 2011) [10.1109/DASC.2011.6096080].
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11588/396210
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