On the design of UAS horizontal separation maneuvers
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hdl:2117/18419
Tipus de documentText en actes de congrés
Data publicació2013
Condicions d'accésAccés obert
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Abstract
This paper studies the separation maneuvers that
an Unmanned Air System (UAS) may execute to avoid breaching
the separation safety margins imposed in each type of airspace,
namely 3 NM, 5 NM, and 10 NM. The UAS was assumed
under the control of its Pilot in Command, with available
information about its surrounding traffic through ADS-B or
ADS-C, and most likely under the supervision of an ATCo.
A number of UAS separation maneuvers have been identified
that may guarantee the desired levels of separation if executed
with the right parameters and enough anticipation. This paper
focuses on identification of the most suitable maneuver for
any separation conflict geometry and performance envelop. The
conflict geometry is modeled to take into account the speed of
both vehicles (the UAS and the intruder), the conflict angle, the
turning limitations of the UAS, the reaction time of the pilot, and
the communication latency.
CitacióPastor, E. [et al.]. On the design of UAS horizontal separation maneuvers. A: SESAR Innovation Days. "Proceedings of the 2nd SESAR innovation days.". Brauhschweig: 2013, p. 1-11.
Versió de l'editorhttp://sesarinnovationdays.eu/files/SIDs/2012/SID%202012-23.pdf
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pastor_SID_12.pdf | 6,338Mb | Visualitza/Obre |