Research on optimal location of actuators in active vibration control for helicopter

被引：0
|
作者：
Hu, Jun
Gu, Zhongquan
机构：
来源：
Nanjing Hangkong Hangtian Daxue Xuebao/Journal of Nanjing University of Aeronautics & Astronautics | 2000年 / 32卷 / 01期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：69 / 74
相关论文
共 50 条
  • [1] Optimal location of actuators and sensors in active vibration control
    Bruant, I
    Proslier, L
    JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES, 2005, 16 (03) : 197 - 206
  • [2] OPTIMAL LOCATION OF ACTUATORS FOR ACTIVE DAMPING OF VIBRATION
    HOLNICKISZULC, J
    LOPEZALMANSA, F
    RODELLAR, J
    AIAA JOURNAL, 1993, 31 (07) : 1274 - 1279
  • [3] Optimal location and geometry of sensors and actuators for active vibration control of smart composite beams
    Prakash, Bhanu
    Yasin, M. Yaqoob
    Khan, A. H.
    Asjad, Mohammad
    Khan, Zahid A.
    AUSTRALIAN JOURNAL OF MECHANICAL ENGINEERING, 2022, 20 (04) : 981 - 999
  • [4] Optimization Selection Approach for Distribution of Actuators in Active Vibration Control of Helicopter
    Cheng Qi-you
    Deng Jing-hui
    Huang Jian-ping
    Ling Ai-min
    Lu Ke
    2015 34TH CHINESE CONTROL CONFERENCE (CCC), 2015, : 3248 - 3251
  • [5] Optimal location of piezoelectric actuators for active vibration control of thin axially functionally graded beams
    Isabelle Bruant
    Laurent Proslier
    International Journal of Mechanics and Materials in Design, 2016, 12 : 173 - 192
  • [6] Optimal placement of actuators and sensors for vibration active control
    Liu, FQ
    Zhang, LM
    Link, M
    IMAC - PROCEEDINGS OF THE 17TH INTERNATIONAL MODAL ANALYSIS CONFERENCE, VOLS I AND II, 1999, 3727 : 1820 - 1825
  • [7] Optimal location of piezoelectric actuators for active vibration control of thin axially functionally graded beams
    Bruant, Isabelle
    Proslier, Laurent
    INTERNATIONAL JOURNAL OF MECHANICS AND MATERIALS IN DESIGN, 2016, 12 (02) : 173 - 192
  • [8] The optimal location of piezoelectric actuators and sensors for vibration control of plates
    Kumar, K. Ramesh
    Narayanan, S.
    SMART MATERIALS AND STRUCTURES, 2007, 16 (06) : 2680 - 2691
  • [9] Study on optimal design of actuators for active control of structural responses of helicopter
    State Key Laboratory of Rotorcraft and Aeromechanics, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
    J Vib Shock, 2007, 3 (23-26):
  • [10] Hybrid Active Vibration Control of Helicopter Fuselage Driven by Piezoelectric Stack Actuators
    Lang, Kai
    Xia, Pinqi
    JOURNAL OF AIRCRAFT, 2019, 56 (02): : 719 - 729
12345