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电动静液作动器设计方法综述

付永领 韩旭 杨荣荣 齐海涛 付剑

付永领, 韩旭, 杨荣荣, 等 . 电动静液作动器设计方法综述[J]. 北京航空航天大学学报, 2017, 43(10): 1939-1952. doi: 10.13700/j.bh.1001-5965.2017.0195
引用本文: 付永领, 韩旭, 杨荣荣, 等 . 电动静液作动器设计方法综述[J]. 北京航空航天大学学报, 2017, 43(10): 1939-1952. doi: 10.13700/j.bh.1001-5965.2017.0195
FU Yongling, HAN Xu, YANG Rongrong, et al. Review on design method of electro-hydrostatic actuator[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(10): 1939-1952. doi: 10.13700/j.bh.1001-5965.2017.0195(in Chinese)
Citation: FU Yongling, HAN Xu, YANG Rongrong, et al. Review on design method of electro-hydrostatic actuator[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(10): 1939-1952. doi: 10.13700/j.bh.1001-5965.2017.0195(in Chinese)

电动静液作动器设计方法综述

doi: 10.13700/j.bh.1001-5965.2017.0195
基金项目: 

航空科学基金 20152851020

详细信息
    作者简介:

    付永领, 男, 博士, 教授, 博士生导师。主要研究方向:新型集成一体化功率电传作动技术、液压伺服系统理论与试验研究、特种机器人等

    付剑, 男, 博士。主要研究方向:新型集成一体化功率电传作动技术、复杂机电系统建模与仿真等

    通讯作者:

    付剑, E-mail: fujianbuaa@126.com

  • 中图分类号: TH122;V245.1

Review on design method of electro-hydrostatic actuator

Funds: 

Aeronautical Science Foundation of China 20152851020

More Information
  • 摘要:

    电动静液作动器(EHA)是一种起源于航空领域的新型高性能伺服作动装置,正逐渐成为各类大型装备的通用基础元部件,鉴于其机电液控热多学科耦合较大且要达到的综合指标又高,所以迫切需要一套高效科学的设计方法。从EHA完整设计过程的角度,综述其中的设计方法,为今后EHA产品的设计开发流程提供了基本支撑和多样化的技术手段。总结出基于自动化系统设计和多学科联合详细设计的EHA设计方法,并对其中的综合指标建立、建模仿真、优化设计、控制设计等关键技术进行了分析,给出适合不同设计任务特点的各步骤实现途径。展望了自动化详细设计、基于模型系统工程、3D打印等最新技术在EHA设计中的应用,为后续进一步提升EHA设计水平提供了参考。

     

  • 图 1  机电产品一般开发流程

    Figure 1.  General development process of mechatronic product

    图 2  加入虚拟性能验证的产品设计流程[33]

    Figure 2.  Product design process with virtual performance evaluation[33]

    图 3  EHA设计流程框架

    Figure 3.  EHA design process overview

    图 4  产品设计平台内涵框图[99]

    Figure 4.  Block diagram of product design platform[99]

    图 5  集成于ISIGHT的机电一体化系统优化设计平台[64]

    Figure 5.  Optimal design platform for mechatronic system integrated in ISIGHT[64]

    表  1  用于架构选择的定量与定性矩阵[43]

    Table  1.   Quantitative and qualitative matrix for concept selection[43]

      评价指标 指标值 单位
    定量指标 质量 kg
    可靠性/平均故障间隔时间 flight hour
    一次性成本 $或€
    重复性成本 $或€
    维护费用 $或€
      评价指标 满足或不满足
    定性指标 安装要求
    功能要求
    安全要求
    性能要求
    技术风险
    下载: 导出CSV
  • [1] JONES R.The more electric aircraft-assessing the benefits[J].Proceedings of the Institution of Mechanical Engineers, Part G:Journal of Aerospace Engineering, 2002, 216(5):259-269. doi: 10.1243/095441002321028775
    [2] BOSSCHE D.The A380 flight control electro-hydrostatic actuators, achievements and lessons learnt[C]//Proceedings of 25th International Congress of the Aeronautical Science.Hamburg:The German Society for Aeronautics and Astronautics, 2006:1-8.
    [3] THOMPSON K.Note on "the electric control of large aeroplanes"[J].IEEE Aerospace and Electronic Systems Magazine, 2002, 3(2):19-24.
    [4] ALDEN R.C-141 and C-130 power-by-wire flight control systems[C]//Proceedings of the IEEE 1991 National Aerospace and Electronics Conference.Piscataway, NJ:IEEE Press, 1991:535-539.
    [5] NAVAROO R.Performance of an electro-hydrostatic actuator on the F-18 systems research aircraft:NASA/TM-97-206224[R].Lancaster:Dryden Flight Research Center, 1997:1-32.
    [6] JENSEN S, JENNEY G, RAYMOND B, et al.Flight test experience with an electromechanical actuator on the F-18 systems research aircraft[C]//The 19th Digital Avionics Systems Conference Proceedings.Piscataway, NJ:IEEE Press, 2000:1-10.
    [7] KOPOLA D, DOELL C.High performance electromechanical actuation for primary flight surfaces (EPAD program results)[C]//Proceedings of the 1st International Conference on Recent Advances in Aerospace Actuation Systems and Components, 2001:135-139.
    [8] BILDSTEIN M.EHA for flight testing on airbus A321 power losses of fixed pump EHA versus variable pump EHA[C]//Proceedings of the International Conference on Recent Advances in Aerospace Hydraulics, 1998:101-103.
    [9] BLANDING D.Subsystem design and integration for the more electric aircraft[C]//Proceedings of 5th International Energy Conversion Engineering Conference and Exhibit.Reston:AIAA, 2007:1-8.
    [10] TODESCHI M.Airbus-EMAs for flight controls actuation system-perspectives[C]//Proceedings of the 4th International Conference on Recent Advances in Aerospace Actuation Systems and Components, 2010:1-8.
    [11] TODESCHI M.Airbus-EMAs for flight controls actuation system 2012 status and perspectives[C]//Proceedings of the 5th International Conference on Recent Advances in Aerospace Actuation Systems and Components, 2012:1-10.
    [12] KAMINAGA H, AMARI T, NIWA Y, et al.Electro-hydrostatic actuators with series dissipative property and their application to power assist devices[C]//Proceedings of the 20103rd IEEE RAS & EMBS International Conference on Biomedical Robotics and Biomechatronics.Piscataway, NJ:IEEE Press, 2010:76-81.
    [13] ISO.Aerospace-electrohydrostatic actuator (EHA)-characteristics to be defined in procurement specifications:ISO22072[S].Geneva:ISO, 2011.
    [14] 闻邦椿, 李小彭.科学发展观指导下的产品系统化设计的理论与方法[J].机械工程学报, 2013, 49(19):77-86. http://www.cnki.com.cn/Article/CJFDTOTAL-JXXB201319010.htm

    WEN B C, LI X P.Systematized design theory and method of products based on scientific development outlook[J].Journal of Mechanical Engineering, 2013, 49(19):77-86(in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-JXXB201319010.htm
    [15] 李少波, 胡建军, 谢庆生, 等.基于遗传编程与键合图的机电系统自动设计[J].系统仿真学报, 2002, 14(11):1513-1516. doi: 10.3969/j.issn.1004-731X.2002.11.029

    LI S B, HU J J, XIE Q S, et al.Automated design of mechatronic system based on genetic programming & bond graphs[J].Journal of System Simulation, 2002, 14(11):1513-1516(in Chinese). doi: 10.3969/j.issn.1004-731X.2002.11.029
    [16] GAVEL H, ÖLVANDER J, KRUS P.Optimal conceptual design of aircraft fuel transfer systems[J].Journal of Aircraft, 2006:43(5):1334-1340. http://www.refdoc.fr/Detailnotice?cpsidt=18197680
    [17] GAVEL H, ÖLVANDER J, JOHANSSON B.Aircraft fuel system synthesis aided by interactive morphology and optimization[C]//Proceedings of 45th AIAA Aerospace Sciences Meeting and Exhibit.Reston:AIAA, 2011:1-13.
    [18] NILSSON K, ANDERSSON J, KRUS P.Method for integrated systems design-A study of EHA systems[C]//Proceedings of International Conference on Recent Advances in Aerospace Hydraulics, 1998:7-14.
    [19] GAGNE D, SELLIER F, ROMAN C.Simulation and design process of mechatronics systems[C]//Proceedings of the 1st International Conference on Recent Advances in Aerospace Actuation Systems and Components, 2001:99-105.
    [20] ROOS F.Towards a methodology for integrated design of mechatronic servo systems[D].Stockholm:KTH Royal Institute of Technology, 2007.
    [21] ARRIOLA D, SCHÄFER A, THIELECKE F, et al.A model-based method to assist the architecture selection and preliminary design of flight control electro-mechanical actuators[C]//Proceedings of the 7st International Conference on Recent Advances in Aerospace Actuation Systems and Components, 2016:166-174.
    [22] HALABI T, BUDINGER M, MARE J.Optimal geometrical integration of electromechanical actuators[C]//Proceedings of the 4st International Conference on Recent Advances in Aerospace Actuation Systems and Components, 2010:35-41.
    [23] LISCOUET J, BUDINGER M, MARE J, et al.Modelling approach for the simulation-based preliminary design of power transmissions[J].Mechanism and Machine Theory, 2011, 46(3):276-289. doi: 10.1016/j.mechmachtheory.2010.11.010
    [24] SAFAVI E, CHAITANYA R, OLVANDER J, et al.Multidisciplinary optimization of aircraft vehicle system for conceptual analysis[C]//Proceedings of 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition.Reston:AIAA, 2013:1-9.
    [25] SAFAVI E, GOPINATHY V, OLVANDER J.A collaborative tool for conceptual aircraft systems design[C]//Proceedings of AIAA Modeling and Simulation Technologies Conference.Reston:AIAA, 2012:1-10.
    [26] GARMENDIA D, CHAKRABORTY I, MAVRIS D.Method for evaluating electrically actuated hybrid wing-body control surface layouts[J].Journal of Aircraft, 2015, 52(6):1780-1790. doi: 10.2514/1.C033061
    [27] CHAKRABORTY I, TRAWICK D, HEGDE C, et al.Development of a modeling and simulation environment for real-time performance analysis of electric actuators in maneuvering flight[C]//Proceedings of 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aero-space Exposition.Reston:AIAA, 2013:1-17.
    [28] CHAKRABORTY I, JACKSON D, TRAWICK D, et al.Development of a sizing and analysis tool for electro-hydrostatic and electromechanical actuators for the more electric aircraft[C]//Proceedings of 2013 Aviation Technology, Integration, and Operations Conference.Reston:AIAA, 2013:1-17.
    [29] CHAKRABORTY I, TRAWICK D, JACKSON D, et al.Electric control surface actuator design optimization and allocation for the more electric aircraft[C]//Proceedings of 2013 Aviation Technology, Integration, and Operations Conference.Reston:AIAA, 2013:1-17.
    [30] GARMENDIA D, CHAKRABORTY I, TRAWICK D, et al.Assessment of electrically actuated redundant control surface layouts for a hybrid wing body concept[C]//Proceedings of 14th AIAA Aviation Technology, Integration, and Operations Conference.Reston:AIAA, 2014:1-23.
    [31] GARMENDIA D, CHAKRABORTY I, MAVRIS D.Uncertainty quantification for the actuation power requirements of a hybrid wing body configuration with electrically actuated flight control surfaces[C]//Proceedings of 53rd AIAA Aerospace Sciences Meeting.Reston:AIAA, 2015:1-22.
    [32] CHAKRABORTY I, MAVRIS D, EMENETH M, et al.A system and mission level analysis of electrically actuated flight control surfaces using Pacelab SysArc[C]//Proceedings of 52nd Aerospace Sciences Meeting.Reston:AIAA, 2014:1-22.
    [33] KREITZ T, ARRIOLA D, THIELECKE F.Virtual performance evaluation for electro-mechanical actuators considering parameter uncertainties[C]//Proceedings of the 6th International Conference on Recent Advances in Aerospace Actuation Systems and Components, 2014:136-143.
    [34] 黄晨东, 范军.系统工程指导下的产品开发[M].北京:北京理工大学出版社, 2014.

    HUANG C D, FAN J.System engineering approach to products development[M].Beijing:Beijing Institute of Technology Press, 2014(in Chinese).
    [35] BLANDING D, SEXTON M, SEGAL M, et al.The application of confidence interval in the evaluation of electric actuation duty cycle[C]//Proceedings of 27th International Congress of the Aeronautical Sciences.Bonn:ICAS Presst, 2010:1-6.
    [36] 沈磊. 民用飞机电传飞控作动系统设计与工程运用[D]. 上海: 上海交通大学, 2012.

    SHEN L.Civil aircraft fly by wire flight contral actuation system design and engineering application[D].Shanghai:Shanghai Jiao Tong University, 2012(in Chinese).
    [37] HABIBI S, GOLDENBERG A.Design of a new high-performance electrohydraulic actuator[J].IEEE/ASME Transactions on Mechatronics, 2000, 5(2):158-164. doi: 10.1109/3516.847089
    [38] HABIBI S, SINGH G.Derivation of design requirements for optimization of a high performance hydrostatic actuation system[J].International Journal of Fluid Power, 2000, 1(2):11-27. doi: 10.1080/14399776.2000.10781088
    [39] HOSPITAL F, BUDINGER M, REYSSET A, et al.Preliminary design of aerospace linear actuator housings[J].Aircraft Engineering and Aerospace Technology, 2015, 87(3):224-237. doi: 10.1108/AEAT-02-2013-0046
    [40] 孔祥东, 俞滨, 权凌霄, 等.四足机器人对角小跑步态下液压驱动单元位置伺服控制特性参数灵敏度研究[J].机器人, 2015, 37(1):63-73. http://www.cnki.com.cn/Article/CJFDTOTAL-JQRR201501008.htm

    KONG X D, YU B, QUAN L X, et al.Characteristic parameters sensitivity of position servo control for hydraulic drive unit of a quadruped robot in trotting gait[J].Robot, 2015, 37(1):63-73(in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-JQRR201501008.htm
    [41] 孔祥东, 俞滨, 权凌霄, 等.四足仿生机器人液压驱动单元轨迹灵敏度分析[J].机械工程学报, 2013, 49(14):170-175. http://www.cnki.com.cn/Article/CJFDTOTAL-JXXB201314027.htm

    KONG X D, YU B, QUAN L X, et al.Trajectory sensitivity analysis of hydraulic drive unit of quadruped bionic robot[J].Journal of Mechanical Engineering, 2013, 49(14):170-175(in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-JXXB201314027.htm
    [42] PERSSON J, ÖLVANDER J.Comparison of sampling methods for a dynamic pressure regulator[C]//AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition.Reston:AIAA, 2011:1-11.
    [43] KIRCHMANN I, ROTTACH M, SCHNEIDER T.Application of EMA and EHA in aircraft systems[C]//The 7th International Conference on Recent Advances in Aerospace Actuation Systems and Components, 2016:10-14.
    [44] PETTERSSON K, KRUS P.Design optimization of complex hydromechanical transmissions[J].Journal of Mechanical Design, 2013, 135(9):091005. doi: 10.1115/1.4024732
    [45] ANDERSSON J, KRUS P, NILSSON K.Optimization as a support for selection and design of aircraft actuation systems:AIAA-1998-4887[R].Reston:AIAA, 1998.
    [46] 朱士强. 现代产品设计总体规划与管理的研究[D]. 沈阳: 东北大学, 2010.

    ZHU S Q.Study on theory of modern product design planning and management[D].Shenyang:Northeastern University, 2010(in Chinese).
    [47] JULIE M.Hydraulic system definition and simulation[C]//The 7th International Conference on Recent Advances in Aerospace Actuation Systems and Components, 2001:113-117.
    [48] FU J, MARE J, FU Y, et al.Incremental modelling and simulation of power drive electronics and motor for flight control electromechanical actuators application[C]//IEEE International Conference on Mechatronics and Automation.Piscataway, NJ:IEEE Press, 2015:1319-1325.
    [49] FU J, MARÉ J, FU Y.Modelling and simulation of flight control electromechanical actuators with special focus on model architecting, multidisciplinary effects and power flows[J].Chinese Journal of Aeronautics, 2017, 30(1):47-65. doi: 10.1016/j.cja.2016.07.006
    [50] CASCIO D, STRONG C, RICHARDS M.HV management process, from design to verification testing, applied to HV electronic assemblies[C]//The 5th International Conference on Recent Advances in Aerospace Actuation Systems and Components, 2012:152-161.
    [51] FRISCHEMEIER S.Electrohydrostatic actuators for aircraft primary flight control-types, modelling and evaluation[C]//5th Scandinavian International Conference on Fluid Power.Link-ping:Link ping University Electronic Press, 1997:1-16.
    [52] KRUS P, JOHANSSON B, AUSTRIN L.Concept optimization of aircraft systems using scaling models[C]//The 2th International Conference on Recent Advances in Aerospace Actuation Systems and Components, 2004:1-7.
    [53] SAFAVI E.Collaborative multidisciplinary design optimization:A framework applied on aircraft systems and industrial Robots[D].Link ping:Link ping University, 2013.
    [54] BUDINGER M, PASSIEUX J, GOGU C, et al.Scaling-law-based metamodels for the sizing of mechatronic systems[J].Mechatronics, 2013, 24(7):775-787. http://www.sciencedirect.com/science/article/pii/S0957415813002328
    [55] LENOBLE G, OLIVIER M, STEBLINKIN A, et al.Elevator actuator housing bay flight mission thermal integrated analysis[C]//The 7th International Conference on Recent Advances in Aerospace Actuation Systems and Components, 2016:118-126.
    [56] LISCOUËT J, BUDINGER M, MARÉ J.Design for reliability of electromechanical actuators[C]//The 4th International Conference on Recent Advances in Aerospace Actuation Systems and Components, 2010:174-182.
    [57] MARE J.Friction modelling and simulation at system level:A practical view for the designer[J].Proceedings of the Institution of Mechanical Engineers.Part I:Journal of Systems & Control Engineering, 2012, 226(6):728-741. doi: 10.1177/0959651812441749
    [58] BUDINGER M, LISCOUËT J, YU C, et al.Simulation based design of electromechanical actuators with Modelica[C]//ASME 2009 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference.New York:ASME, 2009:231-240.
    [59] PASIES-RUBERT O, MUR C, GARAY M, et al.Benefits of multiphysics models integration through cosimulation.case study:Heat monitoring on a primary flight control EMA[C]//The 6th International Conference on Recent Advances in Aerospace Actuation Systems and Components, 2014:144-149.
    [60] LING T, RAHMAT M, HUSAIN A.ANFIS modeling of electro-hydraulic actuator system through physical modeling and FCM gap statistic in initial FIS determination[J].Journal of Intelligent & Fuzzy Systems Applications in Engineering & Technology, 2014, 27(4):1743-1755. https://content.iospress.com/articles/journal-of-intelligent-and-fuzzy-systems/ifs1140
    [61] CARLSSON M, ANDERSSON H, GAVEL H, et al.Methodology for development and validation of multipurpose simulation models[C]//AIAA Aerospace Sciences Meeting Online Proceedings Including the New Horizons Forum and Aerospace Exposition.Reston:AIAA, 2013:1-13.
    [62] COOPER M.Simulating actuator energy demands of an aircraft in flight[D].Cranfield:Cranfield University, 2014.
    [63] KAMINAGA H, ONO J, NAKASHIMA Y, et al.Development of backdrivable hydraulic joint mechanism for knee joint of humanoid robots[C]//IEEE International Conference on Robotics and Automation.Piscataway, NJ:IEEE Press, 2009:1577-1582.
    [64] 朱德全. 基于联合仿真的机电液一体化系统优化设计方法研究[D]. 合肥: 中国科学技术大学, 2012.

    ZHU D Q.Study on optimization design method for mechanical-electrical-hydraulic integrated system based on collaborative simulation[D].Hefei:University of Science and Technology of China, 2012(in Chinese).
    [65] HEGDE C, CHAKRABORTY I, TRAWICK D, et al.A surrogate model based constrained optimization architecture for the optimal design of electrohydrostatic actuators for aircraft flight control surfaces[C]//AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition.Reston:AIAA, 2013:1488-1489.
    [66] RAO R, WAGHMARE G.Multi-objective design optimization of a plate-fin heat sink using a teaching-learning-based optimization algorithm[J].Applied Thermal Engineering, 2015, 76:521-529. doi: 10.1016/j.applthermaleng.2014.11.052
    [67] ROCCA G, TOOREN M.A knowledge based engineering approach to support automatic generation of FE models in aircraft design[C]//45th AIAA Aerospace Sciences Meeting and Exhibit.Reston:AIAA, 2007:1-12.
    [68] KRUS P.Complete aircraft simulation for distributed system design[C]//The 1st International Conference on Recent Advances in Aerospace Actuation Systems and Components, 2001:20-24.
    [69] ANDERSSON J.Multiobjective optimization inengineering design applications to fluid power systems[D].Link ping:Link-ping University, 2001.
    [70] LEI G, WANG T, ZHU J, et al.System-level design optimization method for electrical drive systems-robust approach[J].IEEE Transactions on Industrial Electronics, 2015, 62(8):4702-4713. doi: 10.1109/TIE.2015.2404305
    [71] OUYANG L, MA Y, BYUN J.An integrative loss function approach to multi-response optimization[J].Quality & Reliability Engineering, 2013, 31(2):193-204. doi: 10.1002/qre.1571/epdf
    [72] SUN Y, LIU Y, ZOU T, et al.Design and optimization of a novel six-axis force/torque sensor for space robot[J].Measurement, 2015, 65:135-148. doi: 10.1016/j.measurement.2015.01.005
    [73] 王晓慧, 万长煌, 夏人伟.一种复杂空间飞网系统参数优化设计方法[J].航空学报, 2016, 37(10):3064-3073. http://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201610017.htm

    WANG X H, WAN C H, XIA R W.Parameter optimization design method of complex space-web system[J].Acta Aeronautica et Astronautica Sinica, 2016, 37(10):3064-3073(in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201610017.htm
    [74] ÖLVANDER J.Robustness considerations in multi-objective optimal design[J].Journal of Engineering Design, 2005, 16(5):511-523. doi: 10.1080/09544820500287300
    [75] KRUS P, ANDERSSON J.Optimizing optimization for design optimization[C]//Proceedings of DETC 03ASME 2003 Design Engineering Technical Conferences and Computers and Information in Engineering Conference.New York:ASME, 2003:1-10.
    [76] ÖLVANDER J, KRUS P.Optimizing the optimization-A method for comparison of optimization algorithms[C]//Aiaa Multidisciplinary Design Optimization Specialists Conference.Reston:AIAA, 2013:1-13.
    [77] CHAKRABORTY I, MAVRIS D N, EMENETH M, et al.A methodology for vehicle and mission level comparison of more electric aircraft subsystem solutions:Application to the flight control actuation system[J].Proceedings of the Institution of Mechanical Engineers, Part G:Journal of Aerospace Engineering, 2015, 229(6):1088-1102. doi: 10.1177/0954410014544303
    [78] BRADLEY S, AGOGINO A.An intelligent real time design methodology for component selection:An approach to managing uncertainty[J].Journal of Mechanical Design, 1994, 116(4):980-988. doi: 10.1115/1.2919508
    [79] PASTRAKULJIC V.Design and modeling of a new electro hydraulic actuator[D].Toronto:University of Toronto, 1995.
    [80] MCCULLOUGH K.Design and characterization of a dual electro-hydrostatic actuator[D].Hamilton:McMaster University, 2011.
    [81] CHINNIAH Y, BURTON R, HABIBI S.Failure monitoring in a high performance hydrostatic actuation system using the extended Kalman filter[J].Mechatronics, 2006, 16(10):643-653. doi: 10.1016/j.mechatronics.2006.04.004
    [82] CHINNIAH Y.Fault detection in the electrohydraulic actuator using extended Kalman filter[D].Saskatoon:University of Saskatchewan, 2004.
    [83] LEE J, PARK S, KIM J.Design and experimental evaluation of a robust position controller for an electrohydrostatic actuator using adaptive antiwindup sliding mode scheme[J].Scientific World Journal, 2013, 2013(2):1-17.
    [84] 周国哲, 付永领, 杨荣荣, 等.基于遗传算法的电动静液作动器模型参数辨识[J].液压与气动, 2016(4):92-96. doi: 10.11832/j.issn.1000-4858.2016.04.018

    ZHOU G Z, FU Y L, YANG R R, et al.Parameter identification of electro-hydrostatic actuator based on genetic algorithm[J].Chinese Hydraulics & Pneumatics, 2016(4):92-96(in Chinese). doi: 10.11832/j.issn.1000-4858.2016.04.018
    [85] 邵云滨, 付永领, 郭建文, 等.一种改进的定频数字滞环电流控制策略[J].北京航空航天大学学报, 2017, 43(1):26-35. http://bhxb.buaa.edu.cn/CN/abstract/abstract13936.shtml

    SHAO Y B, FU Y L, GUO J W, et al.An improved constant-frequency digital hysteresis current control strategy[J].Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(1):26-35(in Chinese). http://bhxb.buaa.edu.cn/CN/abstract/abstract13936.shtml
    [86] ALLE N, HIREMATH S, MAKARAM S, et al.Review on electro hydrostatic actuator for flight control[J].International Journal of Fluid Power, 2016, 17(2):1-21. doi: 10.1080/14399776.2016.1169743?scroll=top
    [87] QUAN Z, QUAN L, ZHANG J.Review of energy efficient direct pump controlled cylinder electro-hydraulic technology[J].Renewable & Sustainable Energy Reviews, 2014, 35:336-346. http://www.sciencedirect.com/science/article/pii/S1364032114002639
    [88] ZHANG H, LIU X, WANG J, et al.Robust H sliding mode control with pole placement for a fluid power electrohydraulic actuator (EHA) system[J].The International Journal of Advanced Manufacturing Technology, 2014, 73(5):1095-1104.
    [89] YANG L.Controller design for hydraulic position control systems[D].Saskatoon:University of Saskatchewan, 2011.
    [90] YANG L, SHI Y, BURTON R.Modeling and robust discrete-time sliding-mode control design for a fluid power electrohydraulic actuator (EHA) system[J].IEEE/ASME Transactions on Mechatronics, 2009, 18(1):1-10. http://ieeexplore.ieee.org/document/5963720/
    [91] PACHTER M, HOUPIS C, KANG K.Modelling and control of an electro-hydrostatic actuator[J].International Journal of Robust and Nonlinear Control, 1995, 7(6):591-608.
    [92] GUO K, WEI J, FANG J, et al.Position tracking control of electro-hydraulic single-rod actuator based on an extended disturbance observer[J].Mechatronics, 2015, 27:47-56. doi: 10.1016/j.mechatronics.2015.02.003
    [93] SARIYILDIZ E, OHNISHI K.Stability and robustness of disturbance-observer-based motion control systems[J].IEEE Transactions on Industrial Electronics, 2015, 62(1):414-422. doi: 10.1109/TIE.2014.2327009
    [94] KIM K, JU L, KIM H, et al.Multiobjective optimal design for interior permanent magnet synchronous motor[J].IEEE Transactions on Magnetics, 2009, 45(3):1780-1783. doi: 10.1109/TMAG.2009.2012820
    [95] 陈洪武, 黄克正, 杨波.基于功能表面的产品结构设计自动化研究与实现[J].机械设计与研究, 2004, 20(3):24-27. http://youxian.cnki.com.cn/yxdetail.aspx?filename=BJHK20170711000&dbname=CAPJ2015

    CHEN H W, HUANG K Z, YANG B.Research and implementation on product design automation based on function[J].Machine Design and Research, 2004, 20(3):24-27(in Chinese). http://youxian.cnki.com.cn/yxdetail.aspx?filename=BJHK20170711000&dbname=CAPJ2015
    [96] AMADORI K, TARKIAN M, ÖLVANDER J, et al.Flexible and robust CAD models for design automation[J].Advanced Engineering Informatics, 2012, 26(2):180-195. doi: 10.1016/j.aei.2012.01.004
    [97] CUSSAT-BLANC S, POLLACK J.Cracking the egg:Virtual embryogenesis of real robots[J].Artificial Life, 2014, 20(3):361-383. doi: 10.1162/ARTL_a_00136
    [98] POLLACK J, HORNBY G, LIPSON H, et al.Computer creativity in the automatic design of robots[J].Leonardo, 2006, 36(2):115-121. doi: 10.1002/(SICI)1099-1239(199706)7:6%3C591::AID-RNC293%3E3.0.CO;2-M/abstract
    [99] 孙伟, 现代机械产品设计规划及可视优化设计方法研究[D]. 沈阳: 东北大学, 2007.

    SUN W.Study on product design planning and visual optimization design method of modern machinery[D].Shenyang:Northeastern University, 2007(in Chinese).
    [100] LAAN A, BERG T, HOOTSMANS L.Integrated multidisciplinary engineering solutions at Fokker aerostructures[C]//5th Ceas Air & Space Conference.Belgium:CEAS Press, 2015:1-14.
    [101] PERSSON J, FENG X, WAPPLING D, et al.A framework for multidisciplinary optimization of a balancing mechanism for an industrial robot[J].Journal of Robotics, 2015, 2015(2):1-8. http://dblp.uni-trier.de/db/journals/jr/jr2015.html
    [102] GUERRIER P, ZAZYNSKI T, GILSON E, et al.Additive manufacturing for next generation actuation[C]//The 7th International Conference on Recent Advances in Aerospace Actuation Systems and Components, 2016:42-47.
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  • 收稿日期:  2017-04-05
  • 录用日期:  2017-05-05
  • 刊出日期:  2017-10-20

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