Submit your paper : editorIJETjournal@gmail.com Paper Title : DESIGN AND DEVELOPMENT OF SWASHPLATE-LESS HELICOPTER ISSN : 2395-1303 Year of Publication : 2021 10.29126/23951303/IJET-V7I3P32 MLA Style: -Kallamkunta Mukesh Reddy, S M Nachiketha, T G Prajwal, Prajwal Gowda, V Yamini Anoosha , " DESIGN AND DEVELOPMENT OF SWASHPLATE-LESS HELICOPTER " Volume 7 - Issue 3 May - June,2021 International Journal of Engineering and Techniques (IJET) ,ISSN:2395-1303 , www.ijetjournal.org APA Style: -Kallamkunta Mukesh Reddy, S M Nachiketha, T G Prajwal, Prajwal Gowda, V Yamini Anoosha , " DESIGN AND DEVELOPMENT OF SWASHPLATE-LESS HELICOPTER " Volume 7 - Issue 3 May - June,2021 International Journal of Engineering and Techniques (IJET) ,ISSN:2395-1303 , www.ijetjournal.org Abstract - Helicopters are rotorcraft with horizontally rotating rotors that provide lift and thrust. The helicopter will take off and land vertically, hover, and fly forward, backward, and laterally as a result of this. These motions are created with the aid of a complex swash plate. This mechanical system has a lot of wear and tear, and the pumps are more expensive per unit. This needs to be replaced. Making a helicopter with the technical simplicity of a drone would be a fascinating way to reconcile the technically complex flying helicopter and the technological complex flying quad copter. This can be accomplished with just a programmed micro controller and no swash plate. This gives rise to the concept of a helicopter without a swash plate. By removing the complicated controls of a traditional helicopter swash plate or the dispersed propeller array of a quad rotor, this concept enables new inexpensive, durable, and light weight aircraft Reference 1. Paulos. J. and Yim, M., An Under actuated Propeller for Attitude Control in Micro Air Vehicles, 2013 IEEE/RSJ International Conference on Intelligent Robots and Systems (IROS), Tokyo. 2. Carlos Malpica and Roberto Celi, Simulation based bandwidth analysis of a swash plate less rotor helicopter, Alfred Gessow Rotorcraft Center, University of Maryland. 3. Bennet Caraher., Cyclic Blade Pitch Control for Small UAV without a Swash plate, AIAA Atmospheric Flight Mechanics Conference, SciTech Forum, Grapevine, TX,20174. Paulos. J, and Yim. M., Flight Performance of a Swash plate less Micro Air Vehicle, 2015 IEEE International Conference on Robotics and Automation (ICRA), Seattle, WA, May 2015. 5. James John. Rotorcraft blades pitch control through torque modulation, 2017. 6. V. Kumar and N. Michael, Opportunities and challenges with autonomous micro aerial vehicles, The International Journal of Robotics Research. 7. Leishman, G. J., Principles of Helicopter Aerodynamics, Cambridge University Press, Cambridge, 2nd ed., 2006. 8. Bousman, W. G., The Effects of Structural Flap-Lag and Pitch-Lag Coupling on Soft Inplane Hingeless Rotor Stability in Hover, Tech. Rep. TP-3002, NASA, May 2011 Keywords — Engineering, Helicopter, Swashplate, Arduino, PLA, Matlab. |