Abstract
At the moment, multi-rotor MAV is being proposed for many critical applications so the engineer must provide an MAV, which have good specifications such as the high lifetime, high operational speed, more secure on-flight, and low maintenance cost in order to survive at critical applications. This work deals with the conceptual design and its optimization of the hybrid multi-rotor MAV for high-speed applications by using FSI simulation. The proposed MAV has characterized by the use of two counter-rotating propellers for vertical operation, and two propellers are located in the rear part of the MAV for forward force and yawing control. The airframe and propellers of the MAV are preferred to be of Kevlar composite, which allows for propeller flexibility without sacrificing durability. High lifetime and low probability of failures in terms of FSI analysis are to be achieved by the implementation of Kevlar composite, which has good impact load withstanding capability. The present work aims at performing a numerical simulation to be used for investigating the design behavior of the MAV by simulating the displacement and principal stress in order to withstand at high-speed operation. The design process entailed the overall system design, component selection, and placement in CATIA. FSI simulation of stress and displacement throughout the Kevlar MAV has been analyzed by Ansys 16.2, and thereby, the design optimization has been carried out in the MAV.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Vijayanandh, R., et al.: Numerical study on structural health monitoring for unmanned aerial vehicle, special issue on trends and future in engineering. J. Adv. Res. Dyn. Control Syst. 9(Sp–6), 1937–1958 (2017)
Raj Kumar, G., et al.: Conceptual design and structural analysis of integrated composite micro aerial vehicle, special issue on special issue on environment, engineering & energy. J. Adv. Res. Dyn. Control Syst. 9(Sp–14), 857–881 (2017)
Vijayanandh, R., et al.: Design, fabrication and simulation of hexacopter for forest surveillance. ARPN J. Eng. Appl. Sci, 12(12), 3879–3884 (2017). ISSN 1819-6608
Michelson, R.C., et al.: Overview of Micro Air Vehicle System Design and Integration Issues, pp. 1–12. Georgia Tech Research Institute, Georgia Institute of Technology, Atlanta, GA, USA
Mishra, S., et al.: Design and analysis of composite structure for development of a flapping wing micro air vehicle. J. Basic. Appl. Eng. Res. 1(4), 90–92 (2014) Print ISSN: 2350-0077; Online ISSN: 2350-0255
Shkarayev, S.: Aerodynamic Design of VTOL Micro Air Vehicles. In: 3rd US-European Competition and Workshop on Micro Air Vehicle Systems (MAV07) & European Micro Air Vehicle Conference and Flight Competition (EMAV2007), pp. 4–18, 17–21 Sep 2007, Toulouse, France
Sai Kumar, A., et al.: Design and fabrication of 150 mm fixed wing micro aerial vehicle. Int. J. Sci. Technol. 3(3), 4–9 (2013). ISSN (online): 2250-141X, www.ijst.co.in
Perel, R., et al.: Design, Analysis and Performance of a Rotary Wing MAV. Johns Hopkins University/Applied Physics Laboratory Laurel, MD 20725, pp. 3–17
Hossain, M.A., et al: Development of Design and Manufacturing of a Fixed Wing Radio Controlled Micro Air Vehicle (MAV). MIST Journal: GALAXY (DHAKA) 3, 4–12 (2011). ISSN 2073-6444Â
Kumar, V., et al.: Opportunities and Challenges with Autonomous Micro Aerial Vehicles, pp. 4–16. GRASP Laboratory, University of Pennsylvania, Philadelphia, PA
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2019 Springer Nature Singapore Pte Ltd.
About this paper
Cite this paper
Vijayanandh, R., Senthil Kumar, M., Naveenkumar, K., Raj Kumar, G., Naveen Kumar, R. (2019). Design Optimization of Advanced Multi-rotor Unmanned Aircraft System Using FSI. In: Chandrasekhar, U., Yang, LJ., Gowthaman, S. (eds) Innovative Design, Analysis and Development Practices in Aerospace and Automotive Engineering (I-DAD 2018). Lecture Notes in Mechanical Engineering. Springer, Singapore. https://doi.org/10.1007/978-981-13-2718-6_28
Download citation
DOI: https://doi.org/10.1007/978-981-13-2718-6_28
Published:
Publisher Name: Springer, Singapore
Print ISBN: 978-981-13-2717-9
Online ISBN: 978-981-13-2718-6
eBook Packages: EngineeringEngineering (R0)