Case studies to illustrate the rotorcraft certification by simulation process; CS 29/27 low-speed controllability

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dc.contributor.authorvan’t Hoff, Stefan
dc.contributor.authorWhite, Mark
dc.contributor.authorDadswell, Christopher
dc.contributor.authorLu, Linghai
dc.contributor.authorPadfield, Gareth
dc.contributor.authorQuaranta, Giuseppe
dc.contributor.authorPodzus, Philipp
dc.date.accessioned2023-10-05T14:07:19Z
dc.date.available2023-10-05T14:07:19Z
dc.date.issued2023-09-07
dc.description© The Authorsen_UK
dc.description.abstractThis paper is one of a set presented at the 49th European Rotorcraft Forum discussing results from the EU Clean Sky 2 project, Rotorcraft Certification by Simulation (RoCS). The process developed by the RoCS team provides guidance on the use of flight simulation in certification and features four case studies that illustrate aspects of the process using flight simulation models and flight test data provided by Leonardo Helicopters. This paper presents the case study for the low-speed controllability requirements from the relevant certification paragraphs in the EASA Certification Specifications CS-27 and CS-29. Following an introduction of the related specifications, and the motivation behind seeking compliance supported by simulation, the various phases of the RCbS process are explored in more detail. The intent is to exercise aspects of the RoCS guidance in a practical application to investigate the implementation, and the strengths and limitations, given real-world constraints. Emphasis is placed on the Validation & Verification as well as the Credibility Assessment, taking into account test and simulation uncertainties. Results from piloted simulation trials are included to illustrate possible flight simulator fidelity assessment methods.en_UK
dc.identifier.citationvan't Hoff S, White M, Padfield G, et al (2023) Case studies to illustrate the rotorcraft certification by simulation process; CS 29/27 low-speed controllability. In: 49th European Rotorcraft Forum (ERF49 2023), 5-7 September 2023, Bückeburg, Germanyen_UK
dc.identifier.isbn978-3-932182-92-1
dc.identifier.issn0178-6326
dc.identifier.urihttps://publikationen.dglr.de/?id=620&tx_dglrpublications_pi1[document_id]=54801057
dc.identifier.urihttps://publikationen.dglr.de/?id=620&tx_dglrpublications_pi1[document_id]=54801000
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/20335
dc.language.isoenen_UK
dc.publisherGerman Society for Aeronautics and Astronautics (DGLR: Deutsche Gesellschaft für Luft- und Raumfahrt)en_UK
dc.rightsAttribution 4.0 International*
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/*
dc.titleCase studies to illustrate the rotorcraft certification by simulation process; CS 29/27 low-speed controllabilityen_UK
dc.typeConference paperen_UK

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