Preliminary design of a small-sized flapping UAV: II. Kinematic and structural aspects

Author:

Negrello F.,Silvestri P.,Lucifredi A.,Guerrero J. E.,Bottaro A.

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Reference22 articles.

1. Madangopal R, Khan ZA, Agrawal SK (2005) Biologically inspired design of small flapping wing air vehicles using four-bar mechanisms and quasi-steady aerodynamics. J Mech Des 127:809–816

2. Malik AM, Khalid MSU, Barlas F (2010) Modeling and simulation of kinematics for an active flapping and pitching mechanism. In: Proceedings of the World Congress on Engineering 2010 vol II WCE 2010, June 30–July 2, 2010, London, UK

3. Zbikowski R, Galinski C, Pedersen CB (2005) Four-bar linkage mechanism for insectlike flapping wings in hover: concept and an outline of its realization. J Mech Des 127(4):817–824

4. Kempf A (1999) Patent nFR2776937, France

5. Larijani RF, DeLaurier JD (2001) nonlinear aeroelastic model for the study of flapping wing flight, fixed and flapping wing aerodynamics for micro air vehicle applications. In: Mueller TJ (ed) Progress in astronautics and aeronautics, vol 195. AIAA, Reston, pp 399–420

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