Geometric Control Approach to Longitudinal Stability of Flapping Flight
Author:
Affiliation:
1. Department of Mechanical and Aerospace Engineering, University of California, Irvine, California 92697
2. Department of Aerospace and Ocean Engineering, Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24060
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.G001280
Reference40 articles.
1. Effect of the aerodynamic-induced parametric excitation on the longitudinal stability of hovering MAVs/insects
2. Flight dynamics and control of flapping-wing MAVs: a review
3. Animal Flight Dynamics I. Stability in Gliding Flight
4. Animal Flight Dynamics II. Longitudinal Stability in Flapping Flight
Cited by 30 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Analysis of the integrated pattern of hoverable flapping wing micro-air vehicle;Journal of Engineering Research;2024-07
2. Geometric control analysis of the unsteady aerodynamics of a pitching–plunging airfoil in dynamic stall;Physics of Fluids;2024-03-01
3. The effects of wing inertial forces and mean stroke angle on the pitch dynamics of hovering insects;Scientific Reports;2024-02-02
4. The effects of wing inertial forces on flight stability of hovering insects with varying stroke plane;Nonlinear Dynamics;2023-11-08
5. Review of insect-inspired wing micro air vehicle;Arthropod Structure & Development;2023-01
1.学者识别学者识别
2.学术分析学术分析
3.人才评估人才评估
"同舟云学术"是以全球学者为主线，采集、加工和组织学术论文而形成的新型学术文献查询和分析系统，可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容，当前同舟云学术共收录了国内外主流学术期刊6万余种，收集的期刊论文及会议论文总量共计约1.5亿篇，并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询！咨询电话：010-8811{复制后删除}0370
www.globalauthorid.com
TOP
Copyright © 2019-2024 北京同舟云网络信息技术有限公司 京公网安备11010802033243号 京ICP备18003416号-3