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.
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)
关键词
微型扑翼飞行器
动态面控制
纵向
flapping-wing micro aerial vehicles （MAV）
dynamic surface control（DSC）
longitudinal
