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Flight test design for remotely-piloted aircraft in confined airspace
Linköping University, Department of Management and Engineering, Fluid and Mechatronic Systems. Linköping University, Faculty of Science & Engineering.
Linköping University, Department of Management and Engineering, Fluid and Mechatronic Systems. Linköping University, Faculty of Science & Engineering.
Linköping University, Department of Management and Engineering, Fluid and Mechatronic Systems. Linköping University, Faculty of Science & Engineering.ORCID iD: 0000-0002-2315-0680
Linköping University, Department of Management and Engineering, Fluid and Mechatronic Systems. Linköping University, Faculty of Science & Engineering.
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2017 (English)In: 6th CEAS Air and Space Conference, Aerospace Europe, 16-20 October, 2017, Bucharest, Romania. / [ed] The Council of European Aerospace Societies, Brussels, 2017Conference paper, Published paper (Refereed)
Abstract [en]

Thispaper presents various techniques and procedures that aim to simplify flighttesting of fixed-wing, remotely-piloted aircraft with the purposes ofperformance evaluation and system identification. These methods have beenspecifically developed for flight within visual line-of-sight, a type ofoperation that limits the available airspace severely but offers major costadvantages considering the current regulations for unmanned flight in mostWestern countries.

Place, publisher, year, edition, pages
Brussels, 2017.
Keywords [en]
flight testing, visual line-of-sight, UAS, data acquisition, flight dynamics
National Category
Aerospace Engineering
Identifiers
URN: urn:nbn:se:liu:diva-155054OAI: oai:DiVA.org:liu-155054DiVA, id: diva2:1295444
Conference
6th CEAS Air and Space Conference, Aerospace Europe, 16-20 October, 2017, Bucharest, Romania.
Projects
MSDEMOAvailable from: 2019-03-11 Created: 2019-03-11 Last updated: 2019-03-22Bibliographically approved

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Sobron, AlejandroLundström, DavidKrus, PetterJouannet, Christopher

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