Theoretical Design of Coaxial Rotor Micro Air Vehicle

Mr. Manoj J Watane, Dr. Sau Kamaltai Gawai, Prof. Dushyant B. Pawar
Volume 1: Issue 3, July 2014, pp 196-198

Author's Information
Mr. Manoj J Watane1 
Corresponding Author
1Department of Mechanical Engineering, Institute of Engineering & Technology Darapur, Dist. Amravati, India.
manoj.watane25@gmail.com

 Dr. Sau Kamaltai Gawai, Prof. Dushyant B. Pawar2
2Department of Mechanical Engineering, Institute of Engineering & Technology Darapur, Dist. Amravati, India.

Research Article -- Peer Reviewed
Published online – 30 July 2014

Open Access article under Creative Commons License

Cite this article – Mr. Manoj J Watane, Dr. Sau Kamaltai Gawai, Prof. Dushyant B. Pawar “Theoretical Design of Coaxial Rotor Micro Air Vehicle”, International Journal of Analytical, Experimental and Finite Element Analysis, RAME Publishers, vol. 1, issue 3, pp. 196-198, July 2014.
ark:/13960/t6455m58v

Abstract:-
In recent years, there has been rapid development of autonomous unmanned aircraft equipped with autonomous control devices called unmanned aerial vehicles (UAVs) and micro aerial vehicles (MAVs). These have become known as “robotic aircraft,” and their use has become wide spread. They can be classified according to their application for military or civil use. There has been remarkable development of UAVs and MAVs for military use. However, it can be said that the infinite possibilities of utilizing their outstanding characteristics for civil applications remain hidden. In this paper detailed design procedure for designing a micro air vehicle weighing from 20 gram to 500 gram is presented. Using such design procedure for pay load capacity of 10 grams is design. Different parameters like rotor blade length, length of stabilizer bar, length of fuselage, total length of body, totalpower required is find out. To check feasibility of vehicle in hover condition checking parameters like thrust force, lift force, centrifugal force are find out..
Index Terms:-
Micro air vehicle, coaxial rotor, small weight.,
REFERENCES
  1. McMichael, J. M., Francis, M. S.: “Micro Air Vehicles – Towards a New Dimension in Flight”, DARPA PRESS RELEASE 7th August 1997

  2. Tousley, B.: “Micro Air Vehicle (MAV) Advanced Concept Technology Demonstration (ACTD)”, DARPA PRESS RELEASE 29th June 2005

  3. Bohorquez, F., Samuel, P., Sirohi, J., Rudd, L., Pines, D., Perel, R.: “Design and Analysis and Performance of a Rotary Wing MAV”, Journal of the American Helicopter Society, Vol. 48, No. 2, April 2003, pp. 80-90

  4. Bohorquez, F., Pines, D.: “Rotor and Airfoil Design for Efficient Rotary Wing Micro Air Vehicles”, Proceeding of the 61st Annual Forum of the American Helicopter Society, Grapevine, Texas, June 2004.

  5. Vladimir Khromov and Omri Rand “Design Trends For Rotary-Wing Unmanned Air Vehicles” 25th International Congress Of The Aeronautical Sciences-2006

  6. Michael Inglin “From Kamov's first design to Micro Aerial Vehicles” a survey on coaxial helicopters- 2009

  7. Ron Perel “Design, Analysis and Performance of a Rotary Wing MAV”.

  8. KenzoNonami “Autonomous Flying Robots”-2010

  9. Julián D. Colorado M. “Towards Miniature MAV Autonomous Flight A Modeling & Control Approach”-2009

  10. Alexander P. K. Hall “Coaxial Rotary-Wing Mini Aerial Vehicle Aeromechanics”-March-2009

To view full paper, Download here .

To View Full Paper

For authors

Author's guidelines Publication Ethics Publication Policies Artical Processing Charges Call for paper Frequently Asked Questions(FAQS)

Publishing with