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Foundations of Circulation Control Based Small-Scale Unmanned Aircraft pp 79–97Cite as

UC\(^2\)AV: Unmanned Circulation Control Aerial Vehicle

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Part of the book series: Intelligent Systems, Control and Automation: Science and Engineering ((ISCA,volume 91))

Abstract

This chapter reviews circulation control wing implementation and integration with the RMRC Anaconda platform. It describes the key elements of the platform and the parameters of the aircraft and goes through a detailed Finite Elements Analysis (FEA) of the CCW.

Just because there are flaws in aircraft design that doesn’t mean flying carpets exist

— Ben Goldacre

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Authors and Affiliations

  1. Department of Electrical and Computer Engineering, D. F. Ritchie School of Engineering and Computer Science, DU Unmanned Systems Research Institute, University of Denver, Denver, CO, USA

    Konstantinos Kanistras & Kimon P. Valavanis

  2. Department of Computer Science, D. F. Ritchie School of Engineering and Computer Science, DU Unmanned Systems Research Institute, University of Denver, Denver, CO, USA

    Matthew J. Rutherford

Authors
  1. Konstantinos Kanistras
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  2. Kimon P. Valavanis
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  3. Matthew J. Rutherford
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Corresponding author

Correspondence to Konstantinos Kanistras .

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Kanistras, K., Valavanis, K.P., Rutherford, M.J. (2018). UC\(^2\)AV: Unmanned Circulation Control Aerial Vehicle. In: Foundations of Circulation Control Based Small-Scale Unmanned Aircraft. Intelligent Systems, Control and Automation: Science and Engineering, vol 91. Springer, Cham. https://doi.org/10.1007/978-3-319-67852-8_9

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  • DOI: https://doi.org/10.1007/978-3-319-67852-8_9

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  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-319-67851-1

  • Online ISBN: 978-3-319-67852-8

  • eBook Packages: EngineeringEngineering (R0)

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