Citation: | Fu Yongling, Pang Yao, Liu Hesong, et al. Design and working mode analysis of dissimilar redundant actuator system[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, (4): 432-437,443. (in Chinese) |
[1] |
Bennett J W,Mecrow B C,Jack A G,et al.A prototype electrical actuator for aircraft flaps[J].IEEE Transactions on Industry Applications,2010,46(3):915-921
|
[2] |
Garcia A,Cusido J,Rosero J A,et al.Reliable electro-mechanical actuators in aircraft[J].IEEE Aerospace and Electronic Systems Magazine,2008,23(8):19-25
|
[3] |
Bennett J W,Mecrow B C,Atkinson D J.Safety-critical design of electromechanical actuation systems in commercial aircraft[J].IET Electric Power Applications,2011,5(1):37-47
|
[4] |
Qi Haitao,Mare J C,Fu Yongling.Force equalization in hybrid actuation systems[C]//Proceedings of the Seventh International Conference on Fluid Power Transmission and Control.Hangzhou:World Publishing Corporation,2009:342-348
|
[5] |
王占林,石立.力均衡式余度电液伺服系统的优化设计[J].航空学报,1989,10(8):366-370 Wang Zhanlin,Shi Li.The optimal design of multipass electric-hydraulic servo system with force balance type[J].Acta Aeronautica Et Astronautica Sinica,1989,10(8):366-370(in Chinese)
|
[6] |
Mare J C,Moulaire P.The decoupling of position controlled electrohydraulic actuators mounted in tandem or in series[C]//Proceedings of the Seventh Scandinavian International Conference on Fluid Power.Linkoping:Linkoping Universitet Institute of Technology,2001:93-99
|
[7] |
Jacazio G,Gastaldi L.Equalization techniques for dual redundant electro hydraulic servo actuators for flight control systems[C]//ASME Symposium on Fluid Power and Motion Control.Bath:American Society of Mechanical Engineers,2008:543-549
|
[8] |
Cochoy O,Hanke S,Carl U B.Concepts for position and load control for hybrid actuation in primary flight controls[J].Aerospace Science and Technology,2007,11(3):194-201
|
[9] |
Cochoy O,Carl U B,Thielecke F.Integration and control of electromechanical and electrohydraulic actuators in a hybrid primary flight control architecture[C]//International Conference on Recent Advances in Aerospace Actuation Systems and Components.Toulouse:INSA,2007:1-8
|
[10] |
付永领,齐海涛,王利剑,等.混合作动系统的工作模式研究[J].航空学报,2010,31(6):1177-1184 Fu Yongling,Qi Haitao,Wang Lijian,et al.Research on operating modes in hybrid actuation systems[J].Acta Aeronautica Et Astronautica Sinica,2010,31(6):1177-1184(in Chinese)
|
[11] |
王纪森,李志勇,彭博.非相似余度作动系统建模研究[J].机床与液压,2008,36(6):79-83 Wang Jisen,Li Zhiyong,Peng Bo.Modeling and analysis of the dissimilar redundant actuator system[J].Machine Tool and Hydraulics,2008,36(6):79-83(in Chinese)
|
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