An Experimental Research on Design and Development of Tricopter
Suman Kumar Das1, Dinesh Kumar Gouda2, Anirudha Dash3
1Mr. Suman Kumar Das, Automobile department, Parala Maharaja Engineering College, Berhampur, India.
2Dinesh Kumar Gouda, Automobile department, Parala Maharaja Engineering College, Berhampur, India.
3Anirudha Dash, Automobile department, Parala Maharaja Engineering College, Berhampur, India.
Manuscript received on 15 August 2019. | Revised Manuscript received on 20 August 2019. | Manuscript published on 30 September 2019. | PP: 5119-5123 | Volume-8 Issue-3 September 2019 | Retrieval Number: C5728098319/2019©BEIESP | DOI: 10.35940/ijrte.C5728.098319
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© The Authors. Blue Eyes Intelligence Engineering and Sciences Publication (BEIESP). This is an open access article under the CC-BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/)
Abstract: TThe paper is giving a detail description on the design and simulation of tricopter. As the tricopter runs on the newton third law of motion and thrust forces so the paper discussed the detail procedure to calculating the principle fundamental forces acting on the tricopter. This research paper presents the design steps for a tricopter with the use of motor, propeller, battery, flight controller and power distribution board. The CAD design of tricopter helps to visualise the major flight component of tricopter and its orientation. The major advantage of this tricopter is that it can balance various flight parameters like aileron, rudder and throttle. The application of this tricopter includes fire service, military surveillance, product delivery system and medico application. The objective is to provide the summary of design, calibration, and fabrication of the tricopter.
Keywords: Tricopter, Flight Controller, Servo Control, Calibration, Fabrication.
Scope of the Article: Recent Trends & Developments in Computer Networks