Reliability Assessment of Aircraft Power and Actuation System Based on Three-axis Control

被引：0
|
作者：
Cui, Xiaoyu [1 ]
Wang, Shaoping [1 ]
Li, Qian [1 ]
Shi, Jian [1 ]
机构：
[1] Beihang Univ, Sch Automat Sci & Elect Engn, Beijing, Peoples R China
来源：
2015 IEEE/ASME INTERNATIONAL CONFERENCE ON ADVANCED INTELLIGENT MECHATRONICS (AIM) | 2015年
关键词：
reliability assessment; power and actuation system; three-axis control; dissimilar redundancy;
D O I：
暂无
中图分类号：
TM [电工技术]; TN [电子技术、通信技术];
学科分类号：
0808 ; 0809 ;
摘要：
As a key subsystem in aircraft, electro-hydraulic power and actuation system embodies performance and reliability that is crucial to aircraft safety, maneuverability and flight quality. The substantially increased system redundancy and high volume of dissimilar redundancy further complicate the aircraft electro-hydraulic control and actuation system. This paper presents the reliability model based on three-axis control as well as the reliability assessment method considering the function and performance. Application in several structures of aircraft power and actuation system indicates that the results of proposed method are closer to the actual situation.
引用
收藏
页码：382 / 387
页数：6
相关论文
共 50 条
  • [11] Flight test of aircraft three-axis attitude control without rudders based on distributed dual synthetic jets
    Zhao Z.
    Luo Z.
    Liu J.
    Deng X.
    Peng W.
    Li S.
    Lixue Xuebao/Chinese Journal of Theoretical and Applied Mechanics, 2022, 54 (05): : 1220 - 1228
  • [12] Three-axis contouring control based on a trajectory coordinate basis
    Lo, CC
    JSME INTERNATIONAL JOURNAL SERIES C-MECHANICAL SYSTEMS MACHINE ELEMENTS AND MANUFACTURING, 1998, 41 (02) : 242 - 247
  • [13] Three-axis optical alignment system
    Barns, C.
    Experimental Techniques, 1990, 14 (04) : 49 - 51
  • [14] Development of the control system for three-axis ultraprecision compact micromilling machine
    Wang, Bo
    Zhang, Peng
    Liang, Yingchun
    Dong, Shen
    JOURNAL OF VACUUM SCIENCE & TECHNOLOGY B, 2009, 27 (03): : 1285 - 1287
  • [15] Three-axis active control system for gravity gradient stabilised microsatellite
    Mohammed, A. M. Si
    Benyettou, M.
    Bentoutou, Y.
    Boudjemai, A.
    Hashida, Y.
    Sweeting, M. N.
    ACTA ASTRONAUTICA, 2009, 64 (7-8) : 796 - 809
  • [16] Three-axis MEMS combined sensor for electronic stability control system
    Jeong, Heewon
    Goto, Yasushi
    Aono, Takanori
    Nakamura, Toshiaki
    Hayashi, Masahide
    ELECTRONICS AND COMMUNICATIONS IN JAPAN, 2012, 95 (07) : 49 - 57
  • [17] Control and breakthrough detection of a three-axis robotic bone drilling system
    Lee, Wen-Yo
    Shih, Ching-Long
    MECHATRONICS, 2006, 16 (02) : 73 - 84
  • [18] Fuxxy Logic Control System of Three-Axis CNC Milling Machine
    Bobyr, M., V
    Yakushev, A. S.
    Milostnaya, N. A.
    2018 INTERNATIONAL SCIENTIFIC MULTI-CONFERENCE ON INDUSTRIAL ENGINEERING AND MODERN TECHNOLOGIES (FAREASTCON), 2018,
  • [19] Operational reliability assessment of an aircraft environmental control system
    Jenab, K.
    Rashidi, K.
    RELIABILITY ENGINEERING & SYSTEM SAFETY, 2009, 94 (02) : 456 - 462
  • [20] Control of a three-axis mount based on piezoelectric actuators for vibration reduction
    Mayer, Dirk
    Atzrodt, Heiko
    Herold, Sven
    AT-AUTOMATISIERUNGSTECHNIK, 2008, 56 (03) : 136 - 145
12345