Volume 29 Issue 7
Jul.  2014
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YAN Chang-kai, ZHOU Xiao, ZHANG Hai-bo. Design and simulation of a control scheme for turbo-shaft engine in helicopter autorotation training process[J]. Journal of Aerospace Power, 2014, (7): 1744-1751. doi: 10.13224/j.cnki.jasp.2014.07.030
Citation: YAN Chang-kai, ZHOU Xiao, ZHANG Hai-bo. Design and simulation of a control scheme for turbo-shaft engine in helicopter autorotation training process[J]. Journal of Aerospace Power, 2014, (7): 1744-1751. doi: 10.13224/j.cnki.jasp.2014.07.030

Design and simulation of a control scheme for turbo-shaft engine in helicopter autorotation training process

doi: 10.13224/j.cnki.jasp.2014.07.030
  • Received Date: 2013-04-15
  • Publish Date: 2014-07-28
  • According to the special need of turbo-shaft engines for fast response in helicopter autorotaion training process, a robust control scheme for turbo-shaft engines, including both fuel mass flow and guided vanes angle control, was proposed and designed to reduce the turbine speed transient droop. Firstly, an improved comprehensive model of UH-60 helicopter/T700 engines, which can simulate autorotation decent and autorotation recovery, was presented. Secondly, robust control scheme for turbo-shaft engine based on fuel mass flow and guided vanes adjustment was preset in the simulation cases. The result shows clearly that the turbine speed transient droop, controlled by the proposed robust control scheme, is sharply reduced to 3% than traditional method only exploring fuel mass flow control, while the variation of fuel mass flow is much slower and the operation condition of the actuator is improved.

     

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  • [1]
    Lee A Y,Bryson A E,Hindson W S.Optimal landing of a helicopter in autorotation[R].NASA-CR-177082,1985.
    [2]
    Rogers S P,Asbury C N.A flight training simulator for instructing the helicopter autorotation maneuver:enhanced version[R].NASA-20010018610,2000.
    [3]
    德雷尔马克.直升机和倾转旋翼飞行器飞行仿真引论[M].孙传伟,孙文胜,刘勇,等译.北京:航空工业出版社,2012:210-211.
    [4]
    Shanthakumaran P,Harding J,Thompson T,et al.Flight simulation model application for AH-64A apache engine integration[C]//The 49th Annual Forum of the American Helicopter Society.St.Louis:American Helicopter Sociey,1993:261-282.
    [5]
    黄开明,黄金泉,周文祥,等.直升机自转下滑过程发动机的控制规律[J].航空动力学报,2009,24(11):2595-2600. HUANG Kaiming,HUANG Jinquan,ZHOU Wenxiang,et al.Control law of turboshaft engine for helicopter autorotation training[J].Journal of Aerospace Power,2009,24(11):2595-2600.(in Chinese)
    [6]
    Houston S S.Modeling and analysis of helicopter flight mechanics in autorotation[J].Journal of Aircraft,2003,40(4):675-682.
    [7]
    陈国强.直升机/发动机实时优化控制规律与硬件平台研究[D].南京:南京航空航天大学,2012. CHEN Guoqiang.Study for real-time optimization control and hardware platform based on integrated helicopter/turboshaft engine system[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2012.(in Chinese)
    [8]
    Paramour M G,Jennings P D.Operational requirements for helicopter engine for UK services[R].[S.I.]:
    [9]
    Smith B J,Zaranski R D.Next generation control system for helicopter engines[R].Washington DC:57th International Annual Forum Proceedings of AHS,2001.
    Advisory Group for Aerospace Research and Development.Meeting on Technology Requirements for Small Gas Turbine,1993.
    [10]
    周剑波.变几何涡轴发动机综合控制技术研究[D].南京:南京航空航天大学,2011. ZHOU Jianbo.Research on integrated control technology for variable geometry turbo-shaft engine[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2011.(in Chinese)
    [11]
    周剑波,时瑞军,张秋贵,等.进口导叶可调的涡轴发动机性能寻优控制模式[J].航空动力学报,2011,26(10):2371-2375. ZHOU Jianbo,SHI Ruijun,ZHANG Qiugui,et al.Performance seeking control of turbo shaft engine with variable inlet guide vanes[J].Journal of Aerospace Power,2011,26(10):2371-2375.(in Chinese)
    [12]
    Howlett J J.UH-60A black hawk engineering simulation program[R].NASA Contractor Report 166309,1981.
    [13]
    Lee D J,Barg H,Baek K.Autorotation of an unmanned helicopter by a reinforcement learning algorithm[R].AIAA-2008-7279,2008.
    [14]
    Prouty R W.Helicopter performance,stability and control[M].Melbourne:Krieger Publishing Company,1995.
    [15]
    聂洽耶夫.航空动力装置控制规律与特性[M].单凤桐,译.北京: 国防工业出版社,1995.
    [16]
    Dalamagkidis K,Valavanis K P,Piegl L A.Autonomous autorotation of unmanned rotor craft using nonlinear model predictive control[J].Journal of Intelligent and Robotic Systems,2010,57(1/2/3/4):351-369.
    [17]
    俞立.线性矩阵不等式处理方法[M].北京:清华大学出版社,2002:104-107.
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