Arduino-based altitude and heading control of a flapping wing micro-air-vehicle

doi:10.21535/just.v5i2.987

淡江大學機構典藏 > 工學院 > 機械與機電工程學系暨研究所 > 期刊論文 > Item 987654321/112902

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題名:	Arduino-based altitude and heading control of a flapping wing micro-air-vehicle
作者:	Nikhil Panchal;Lung-Jieh Yang;Xin-Yang Zheng;Suseendar Marimuthu;Balasubramanian Esakki
關鍵詞:	Altitude hold;barometer;directional flight;inertial measurement unit (IMU);flapping wing micro air vehicle (FWMAV)
日期:	2017-12
上傳時間:	2018-03-09 12:10:45 (UTC+8)
摘要:	This paper presents the development of hardware module to perform versatile flight controls of flapping wing micro air vehicles (FWMAVs) or ornithopters. Firstly the authors survey the developed avionics, including the configurations of full integration and with discrete components, respectively for flight and control of FWMAVs in the literature. MEMS micro-barometers and micro-compass are frequently interfaced with a microcontroller to determine the altitude and orientation of FWMAVs. Herein a custom-developed printed-circuit-board (PCB) is also integrated with an inertial-measurement-unit (IMU) and a barometer to obtain constant altitude of the air vehicle. The heading of the FWMAV is controlled using a micro-compass with reference to magnetometer direction in the IMU. Simulation and hardware testing were carried out using an ATmega-328P micro-controller onboard. The result confirms that the proposed control system can be adopted to control the FWMAVs efficiently some comments on the necessity of integration about the control avionics are also addressed.
關聯:	Journal of Unmanned Systems Technology 5(2), p.24-30
DOI:	10.21535/just.v5i2.987
顯示於類別:	[機械與機電工程學系暨研究所] 期刊論文

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