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Design Constraints of a Minimally Actuated Four Bar Linkage Flapping-Wing Micro Air Vehicle

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Robot Intelligence Technology and Applications 2

Part of the book series: Advances in Intelligent Systems and Computing ((AISC,volume 274))

Abstract

This paper documents and discusses the design of a low-cost Flapping-Wing Micro Air Vehicle (FW-MAV) designed to be easy to fabricate using readily available materials and equipment. Basic theory of operation as well as the rationale underlying various design decisions will be provided. Using this paper, it should be possible for readers to construct their own devices quickly and at little expense.

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References

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Correspondence to Benjamin M. Perseghetti .

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© 2014 Springer International Publishing Switzerland

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Perseghetti, B.M., Roll, J.A., Gallagher, J.C. (2014). Design Constraints of a Minimally Actuated Four Bar Linkage Flapping-Wing Micro Air Vehicle. In: Kim, JH., Matson, E., Myung, H., Xu, P., Karray, F. (eds) Robot Intelligence Technology and Applications 2. Advances in Intelligent Systems and Computing, vol 274. Springer, Cham. https://doi.org/10.1007/978-3-319-05582-4_47

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  • DOI: https://doi.org/10.1007/978-3-319-05582-4_47

  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-319-05581-7

  • Online ISBN: 978-3-319-05582-4

  • eBook Packages: EngineeringEngineering (R0)

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