A New Approach for Active Control of Rotorcraft Vibration
Author:
Affiliation:
1. Integrated Systems, Inc., Palo Alto, Calif.
2. NASA Ames Research Center, Moffett Field, Calif.
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/10.2514/3.56151
Reference14 articles.
Cited by 11 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. Active Twist Control of Smart Helicopter Rotor - A Survey;Journal of Aerospace Sciences and Technologies;2023-08-11
2. Kalman observer design for marine craft models represented in frequency domain;MORSKIE INTELLEKTUAL`NYE TEHNOLOGII);2021-06-20
3. An offset hub active vibration control system for mitigating helicopter vibrations during power loss: Simulation and experimental demonstration;Aerospace Science and Technology;2018-06
4. Active control of frequency varying disturbances in a diesel engine;Control Engineering Practice;2012-11
5. Closed-Loop Aeromechanical Stability of Hingeless Rotor Helicopters with Higher Harmonic Control;Journal of Guidance, Control, and Dynamics;2006-01
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