基于动态面的微型扑翼飞行器纵向控制  

Longitudinal Control of Flapping-wing Micro Aerial Vehicle Based on Dynamic Surface Control

作　　者：董维中 崔龙[1] 王志东[1,2] 

机构地区：[1]中国科学院大学中国科学院沈阳自动化研究所机器人学国家重点实验室,沈阳110016 [2]日本千叶工业大学先进机器人系

出　　处：《自动化与仪表》2017年第12期1-4,13,共5页Automation & Instrumentation

基　　金：国防基础科研计划(B1320133018)

摘　　要：对于仿生学研究重点之一的微型扑翼飞行器,提出了一种X型翼的微型扑翼飞行器总体设计;给出了该扑翼飞行器气动力计算方程;利用理论力学建立了飞行器纵向模型;采用动态面方法设计了纵向控制器。经过实验仿真证明,基于动态面的纵向稳定控制器能够使飞行器在平衡点附近稳定。Abstract：As 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 can make the aircraft stable near the equilibrium point.

关 键 词：微型扑翼飞行器 动态面控制 纵向 

分 类 号：V276[航空宇航科学与技术—飞行器设计] V279.2