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Design and Testing of a Low-Cost Flight Control and Data Acquisition System for Unstable Subscale Aircraft
Linköping University, Department of Management and Engineering, Fluid and Mechatronic Systems. Linköping University, Faculty of Science & Engineering.ORCID iD: 0000-0002-8932-9210
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: 0000-0002-7797-4239
Linköping University, Department of Management and Engineering, Fluid and Mechatronic Systems. Linköping University, Faculty of Science & Engineering.ORCID iD: 0000-0002-2315-0680
2016 (English)In: Proceedings of the 30th Congress of The International Council of the Aeronautical Sciences (ICAS), September 25-30, Daejeon, South Korea., Bonn: The International Council of the Aeronautical Sciences , 2016Conference paper, Published paper (Refereed)
Abstract [en]

Current research on subscale flight testing methodologies at Linköping University is performed by using various platforms, some of them with advanced configurations. These have been previously flown in open-loop under direct commands from the pilot. However, the interest in flying some of these platforms with relaxed stability and the investigation of multi-surface control allocation techniques motivated the implementation of a simple low-cost flight control system based on commercial-off-the-shelf components. The work described in this paper evaluates the simplest available solutions that provide control augmentation for small, longitudinally unstable, free-flying models. This work also tries to define a reliable, fail-safe system architecture that can be implemented in more advanced platforms. Moreover, data acquisition and analysis are evaluated with the aim of applying system identification techniques.

Place, publisher, year, edition, pages
Bonn: The International Council of the Aeronautical Sciences , 2016.
Keyword [en]
subscale, flight testing, flight control, data acquisition, relaxed stability
National Category
Aerospace Engineering
Identifiers
URN: urn:nbn:se:liu:diva-142393ISBN: 978-3-932182-85-3 (print)OAI: oai:DiVA.org:liu-142393DiVA: diva2:1153436
Conference
30th Congress of The International Council of the Aeronautical Sciences (ICAS), Daejeon, Korea, September 25-30, Daejeon, South Korea.
Projects
MSDEMO
Available from: 2017-10-30 Created: 2017-10-30 Last updated: 2017-11-16

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CiteExportLink to record
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Citation style
  • apa
  • harvard1
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Language
  • de-DE
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More languages
Output format
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