154
S. Palleboina and K. Pallela
circuits should be designed as per specifications and realize the same. Integrate all
the components of MAV and test the performance of the system as per specifications.
Insect wings consist of flexible membranes using chitinous fibrous material and
being supported by semielastic veins (see Chap. 4). According to XQ Bao et al. (2011,
Micromech Microeng 21, 125050) natural wings can will be mimicked in material
conception, weight, venation size, mass distribution and wings rigidity using hybrid
material for bio-mimicking MAVs.
References
1. Prime Faraday Technology Watch. (2002, January). An introduction to MEMS (Micro-
electromechanical Systems). Loughborough University.
2. Sáenz, J. P. (2005). An introduction to micro electro mechanical systems (MEMS). Rama de
Estudiantes del IEEE de Barcelona.
3. Ho, S., Nassef, H., Pornsinsirirak, N., Tai, Y. C., & Ho, C. M. (2003). Unsteady aerodynamics
and flow control for flapping wing flyers. Progress in Aerospace Sciences, 39(8), 635–681.
4. Maboudian, R. (1998). Surface processes in MEMS technology. Surface Science Reports, 30(6),
207–269.
5. Sibilski, K., ˙Zurek, J., & ˙Zyluk, A. (2010). Microelectromechanical flying insects—State of the
art. In 27th International Congress of the Aeronautical Sciences. ICAS, 2010. IEEE.
6. Chari. (2014). Bio-aerodynamics of avian flight. NDRF.