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拍翅式微型飞行器运动学的研究
引用本文:周建华,王姝歆,颜景平.拍翅式微型飞行器运动学的研究[J].机械设计,2005,22(9):17-19.
作者姓名:周建华  王姝歆  颜景平
作者单位:东南大学,机械系,江苏,南京,210096
基金项目:东南大学211工程振兴行动计划(3008002102)
摘    要:对于拍翅式微型飞行器,设计了一种能产生大升力的翅拍动形式,分析计算了翅拍动所产生的气动力和气动力矩,导出了拍翅式微型飞行器机体的运动微分方程。利用该运动微分方程,可以对拍翅式微型飞行器的位置和姿态进行控制。

关 键 词:拍翅飞行  微型飞行器  运动微分方程
文章编号:1001-2354(2005)09-0017-03
收稿时间:2004-07-19
修稿时间:2004-07-192004-11-27

Study on kinematics of flapping wing typed micro air vehicle
ZHOU Jian-hua,WANG Shu-xin,YAN Jing-ping.Study on kinematics of flapping wing typed micro air vehicle[J].Journal of Machine Design,2005,22(9):17-19.
Authors:ZHOU Jian-hua  WANG Shu-xin  YAN Jing-ping
Abstract:A kind of movement style of flapping wings that could produce large lifting force was designed for the flapping wing typed micro air vehicle. Aerodynamic forces and moments produced by the flapping of wing were analyzed and calculated, and the motional differential equations for the body of flapping wing type micro air vehicle were derived. By the use of these motional differential equations, controls on position and attitude can be carried out on flapping wing typed micro air vehicles.
Keywords:flapping wing flying  micro air vehicle  motional differential equation
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