文献类型：期刊文献

英文题名：On Position and Attitude Control of Flapping Wing Micro-aerial Vehicle

作者：Ma, Dexiu[1,2]; Jin, Long[2]; Fu, Dongyang[3]; Xiao, Xiuchun[3]; Liu, Mei[2]

机构：[1] School of Information Science and Engineering, Lanzhou University, Lanzhou, 730000, China; [2] Chongqing Key Laboratory of Big Data and Intelligent Computing, Chongqing Institute of Green and Intelligent Technology, Chinese Academy of Sciences, Chongqing, 400714, China; [3] School of Electronics and Information Engineering, Guangdong Ocean University, Zhanjiang, 524025, China

年份：2020

卷号：12557 LNCS

起止页码：207

外文期刊名：Lecture Notes in Computer Science (including subseries Lecture Notes in Artificial Intelligence and Lecture Notes in Bioinformatics)

收录：EI(收录号：20205109646960)

语种：英文

外文关键词：Aircraft control - MATLAB - Wings - Micro air vehicle (MAV) - Antennas - Aerodynamic drag - Flight control systems

外文摘要：The flapping wing micro-air vehicle (FWMAV) is a new type of aerial vehicle which uses mechanical structure to simulate bird flight. The FWMAV possesses the characteristics of small size, light weight, high flight efficiency and no occupation of runway. Firstly, we calculate the aerodynamic lift and drag on the wing surface. Then, through the analysis and summary of the existing FWMAV control technology, the attitude control model of the aerial vehicle is obtained. Besides, the control system based on STM32F103 is designed, which is equipped with a communication module and thus controls the position and flight attitude through the control signals received wirelessly. Finally, the feasibility of the system is verified by MATLAB and Simulink simulation. ? 2020, Springer Nature Switzerland AG.