{"title":"A six-degree-of-freedom proportional-derivative control strategy for bumblebee flight stabilization","authors":"Xuefei Cai, Hao Liu","doi":"10.1299/JBSE.21-00113","DOIUrl":null,"url":null,"abstract":"Flying insects perform active flight control with flapping wings by continuously adjusting their wing kinematics in stabilizing the body posture to stay aloft under complex natural environment. While the Proportional Derivative (PD) / Proportional Integral Derivative (PID)-based algorithms have been applied to examine specific single degree of freedom (DoF) and/or 3 DoF flight control associated with insect flights, a full 6 DoF flight control strategy remains yet poorly studied. Here we propose a novel 6 DoF PD controller specified for flight stabilization in flapping flights, in which proportional and derivative gains are optimized to facilitate a fast while precise flight control by combing Laplace transformation and root locus method. The vertical position, yaw, pitch and roll are directly stabilized by tuning the wing kinematics while the forward/backward position and lateral position are indirectly stabilized by controlling the pitch and roll, respectively. Coupled with a recently developed flight dynamic model informed by high-fidelity CFD simulation (Cai et al. 2021), this methodology is proven to be effective as a versatile and efficient tool to achieve fast flight stabilization under both small and large perturbations for bumblebee hovering. The 6 DoF PD flight control strategy proposed may provide a useful bioinspired flight-controller design for flapping-wing micro air vehicles (FWMAVs).","PeriodicalId":39034,"journal":{"name":"Journal of Biomechanical Science and Engineering","volume":"1 1","pages":""},"PeriodicalIF":0.0000,"publicationDate":"2021-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Journal of Biomechanical Science and Engineering","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1299/JBSE.21-00113","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q4","JCRName":"Engineering","Score":null,"Total":0}
引用次数: 1
Abstract
Flying insects perform active flight control with flapping wings by continuously adjusting their wing kinematics in stabilizing the body posture to stay aloft under complex natural environment. While the Proportional Derivative (PD) / Proportional Integral Derivative (PID)-based algorithms have been applied to examine specific single degree of freedom (DoF) and/or 3 DoF flight control associated with insect flights, a full 6 DoF flight control strategy remains yet poorly studied. Here we propose a novel 6 DoF PD controller specified for flight stabilization in flapping flights, in which proportional and derivative gains are optimized to facilitate a fast while precise flight control by combing Laplace transformation and root locus method. The vertical position, yaw, pitch and roll are directly stabilized by tuning the wing kinematics while the forward/backward position and lateral position are indirectly stabilized by controlling the pitch and roll, respectively. Coupled with a recently developed flight dynamic model informed by high-fidelity CFD simulation (Cai et al. 2021), this methodology is proven to be effective as a versatile and efficient tool to achieve fast flight stabilization under both small and large perturbations for bumblebee hovering. The 6 DoF PD flight control strategy proposed may provide a useful bioinspired flight-controller design for flapping-wing micro air vehicles (FWMAVs).
在复杂的自然环境下,飞虫通过扇动翅膀,不断调整翅膀的运动来实现主动飞行控制,稳定身体姿态,保持在高空。虽然基于比例导数(PD) /比例积分导数(PID)的算法已经应用于研究与昆虫飞行相关的特定单自由度(DoF)和/或3自由度飞行控制,但对完整的6自由度飞行控制策略的研究仍然很少。本文提出了一种用于扑翼飞行稳定的新型6自由度PD控制器,该控制器通过结合拉普拉斯变换和根轨迹法对比例增益和导数增益进行优化,实现了快速而精确的飞行控制。垂直位置、偏航、俯仰和滚转通过调整机翼运动学直接稳定,前后位置和侧向位置分别通过控制俯仰和滚转间接稳定。结合最近开发的高保真CFD模拟的飞行动力学模型(Cai et al. 2021),该方法被证明是一种多功能和高效的工具,可以在大黄蜂悬停的小扰动和大扰动下实现快速飞行稳定。所提出的六自由度PD飞行控制策略可为扑翼微型飞行器(FWMAVs)提供一种实用的仿生飞行控制器设计。