昆翅在飞行中的动态形变

通过理论模化途径研究昆翅在飞行中的动态形变机制.设计翅气动力试验平台,验证翅准静态形变影响气动力的"柔性楔形效应"理论解释.探讨昆翅的变刚度特性表明,弦向刚度分布规律符合二项式函数时具有优越性和现实性,进而指出昆姻结构的变刚度特性是产生高升力的基本条件.建立了柔性翅的简化力学模型,通过坐标变换法求解在气动力和惯性力共同...     

昆虫飞行高升力的一种新解释——柔性楔形效应

以探索仿生扑翼飞行机器人研制为目的,在研究"柔性楔形效应"的基础上,将昆翅视为柔性翅,提出用"柔性楔形效应"解释昆虫飞行高升力的观点.指出了用"柔性楔形效应"解释昆虫飞行高升力的仿生学意义.根据该观点,翅翼在自适应变形状态下施以简单的节律运动将是未来仿生扑翼飞行机器人翅翼驱动方式的发展趋势.仿生运动的模拟越简单越容易稳定地实现,实验小组已设计制作了仿生扑翼飞行机器人样机,并成功进行了多次室外放飞.     

微型拍翅式飞行机器人平飞位置控制的研究

对微型拍翅式飞行机器人平飞飞行的位置控制,提出了一个基于平均气动力的控制方案,在每个拍动周期结束后,根据位置的状态反馈误差调整参数.通过改变翅的拍动倾斜角和拍动频率来获得所需的平均气动力.在飞行机器人进行水平飞行和垂直飞行时,对控制系统进行解耦.最后对控制系统进行仿真,仿真结果表明该系统具有鲁棒性.     

直动从动件六圆弧盘形凸轮机构的运动学研究

建立了直动从动件六圆弧盘形凸轮机构从动件运动规律及压力角的表达式,分析了有关几何参数对运动特性的影响,可用于尖底及滚子接触直动从动件六圆弧盘形凸轮机构的优化设计．     

Design of Bionic Deformable Planetary-Wheeled Robots

In order to improve the robot＇s obstacle-climbing capability,a new bionic deformable planetary-wheeled robot based on the modular design was proposed. It mainly consisted of planetary wheels to surmount obstacles,a transformable chassis and an averagely segmentation body. The mobile system of the robot was mainly designed while considering the chassis transformability; a deformable four-bar linkage was adopted,which could realize the robot＇s wheelbase conversion from storing to driving. To improve the wheels＇ capability of obstacle-climbing,planetary wheels were adopted. At the same time,passive adaptation to various terrains was considered in the body design and an averaging system was included,which ensured that the planetary wheels could land simultaneously in rugged grounds. The robot＇s steering mode was analyzed and its kinematics model was built,which provided the theoretical evidence for studying the robot motion control.     

上动从动件六圆弧盘形凸轮机构的运动学研究

建立了直动从动件六圆弧盘形凸轮机构从动件运动规律及压力角的表达式,分析了有关几何参数对运动特性的影响,可用于尖底及滚子接直动从动件六圆弧盘形凸轮机构的优化设计。