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Alternative TitleLongitudinal Control of Flapping-wing Micro Aerial Vehicle Based on Dynamic Surface Control
董维中; 崔龙; 王志东
Source Publication自动化与仪表
Volume32Issue:12Pages:1-4, 13
Contribution Rank1
Funding Organization国防基础科研计划(B1320133018)
Keyword微型扑翼飞行器 动态面控制 纵向
Other AbstractAs one of the most important research directions of bionics,flapping-wing micro aerial vehicles(MAV) have attracted the attention of a large number of researchers in recent years. An overall design of flapping-wing MAV with X-shaped wing is presented. The aerodynamic calculation equation of flapping-wing aircraft is given. The longitudinal model of aircraft is established by theoretical mechanics. The longitudinal controller is designed by using the dynamic surface control method. The simulation results show that the longitudinal stability controller based on dynamic surface can make the aircraft stable near the equilibrium point.
Document Type期刊论文
Corresponding Author董维中
Recommended Citation
GB/T 7714
董维中,崔龙,王志东. 基于动态面的微型扑翼飞行器纵向控制[J]. 自动化与仪表,2017,32(12):1-4, 13.
APA 董维中,崔龙,&王志东.(2017).基于动态面的微型扑翼飞行器纵向控制.自动化与仪表,32(12),1-4, 13.
MLA 董维中,et al."基于动态面的微型扑翼飞行器纵向控制".自动化与仪表 32.12(2017):1-4, 13.
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