Optimization Design of Flapping Mechanism of Micro Air Vehicle Based on Matlab and Adams

被引：0
|
作者：
Xiao, Shengjie [1 ]
Deng, Huichao [1 ]
Zhang, Xuedong [1 ]
Ding, Xilun [2 ]
机构：
[1] Beihang Univ BUAA, Sch Mech Engn & Automat, Beijing 100191, Peoples R China
[2] Beihang Univ BUAA, Sch Mech Engn & Automat, Beijing Adv Innovat Ctr Biomed Engn, Beijing 100191, Peoples R China
来源：
2018 IEEE INTERNATIONAL CONFERENCE ON ROBOTICS AND BIOMIMETICS (ROBIO) | 2018年
基金：
中国国家自然科学基金;
关键词：
D O I：
暂无
中图分类号：
TM [电工技术]; TN [电子技术、通信技术];
学科分类号：
0808 ; 0809 ;
摘要：
In view of the shortcomings of the previous mechanism design for the flapping wing micro air vehicle(FMAV), such as small flapping angle and low transmission efficiency, a new type mechanism of FMAV is designed in this paper. Large aerodynamic force is generated by the large amplitude flapping angle and high frequency flapping. By combining the new control mechanism, the maneuverability of the aircraft and the load demand during the mission are improved. Meanwhile, this new type mechanism meets the design requirements of the miniaturization and flexibility, and provide the theoretical basis and application value for the mission of the aircraft to carry out the border patrol, the disaster rescue and the reconnaissance missions.
引用
收藏
页码：312 / 317
页数：6
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