Aerodynamics of Drones with Auxetic Landing Gears During Perching Conditions
Magesh. M1, Jawahar. P.K2
1Magesh. M, Assistant Professor, Department of Aerospace Engineering, B S Abdur Rahman Crescent Institute of Science and Technology, Chennai (Tamil Nadu), India.
2Jawahar. P.K, Professor, Department of Electronics and Instrumentation Engineering, B S Abdur Rahman Crescent Institute of Science and Technology, Chennai (Tamil Nadu), India.
Manuscript received on 10 November 2019 | Revised Manuscript received on 18 December 2019 | Manuscript Published on 31 December 2019 | PP: 517-522 | Volume-9 Issue-2S4 December 2019 | Retrieval Number: B12251292S419/2019©BEIESP | DOI: 10.35940/ijitee.B1225.1292S419
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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: This research investigates a quad copter that acts as a contactor of the perching process of birds with its auxetic graspers on the cylindrical surfaces. The perching system generates a time of yaw when a pitch / rolling control input during the drone landing is introduced by two different circumstances (high and forward flight). While in all situations the aggregate need for revolution every minute, pitch and energy consumption vs. flight vs, the auxetic environment enhances drone resistance in the treatment for spontaneous vibration talking. The suggested method stabilises frequency, yawing and rotating period with respect to the variable rate during perching.
Keywords: About four Key Words or Phrases in Alphabetical Order, Separated by Commas.
Scope of the Article: Aerospace Engineering