Networked Guaranteed Cost Control for Turbofan Aero-engines
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- 英文论文题名：Networked Guaranteed Cost Control for Turbofan Aero-engines
- 论文作者：Ruichao Li ; Yingqing Guo ; Yifeng Chen ; Zhanyue Zhao
- 英文论文作者：Ruichao Li ; Yingqing Guo ; Yifeng Chen ; Zhanyue Zhao ; School of Power and Energy ; Northwestern Polytechnical University
- 年：2017
- 作者机构：School of Power and Energy,Northwestern Polytechnical University;
- 英文论文关键词：Turbofan Aero-engines ; Networked Control Systems ; Guaranteed Cost Control ; Time-delay ; Packet-dropout
- 会议召开时间：2017-07-26
- 会议录名称：第36届中国控制会议论文集（A）
- 英文会议录名称：Proceedings of the 36th Chinese Control Conference（A）
- 语种：英文
- 分类号：V235.13
- 学会代码：KZLL
- 会议名称：第36届中国控制会议
- 会议地点：中国辽宁大连
- 主办单位：中国自动化学会控制理论专业委员会
- 学会名称：中国自动化学会控制理论专业委员会
- 页数：6
- 文件大小：527k
- 原文格式：D
- 会议级别：全国
摘要
In this paper, a guaranteed cost controller is designed for a mixed-flow two-spool turbofan engine to ensure its dynamical performance under networked conditions. The linear state-space engine model is first identified, based on which a networked engine control(NEC) system is established where the transmission delay and the packet dropout are considered simultaneously. Then the networked guaranteed cost control theory is introduced which guarantees both the robustness against delay/dropout and the satisfactory dynamic performance. This controller design is formulated as an optimization problem which is solved by the cone complementarity linearization algorithm. In the meanwhile, the corresponding performance index is also calculated, which provides a reference for the future development of the distributed engine control system. Finally, simulations are performed on an aerothermodynamics component-level engine simulator to demonstrate the validity and applicability of the proposed approach.
In this paper, a guaranteed cost controller is designed for a mixed-flow two-spool turbofan engine to ensure its dynamical performance under networked conditions. The linear state-space engine model is first identified, based on which a networked engine control(NEC) system is established where the transmission delay and the packet dropout are considered simultaneously. Then the networked guaranteed cost control theory is introduced which guarantees both the robustness against delay/dropout and the satisfactory dynamic performance. This controller design is formulated as an optimization problem which is solved by the cone complementarity linearization algorithm. In the meanwhile, the corresponding performance index is also calculated, which provides a reference for the future development of the distributed engine control system. Finally, simulations are performed on an aerothermodynamics component-level engine simulator to demonstrate the validity and applicability of the proposed approach.
In this paper, a guaranteed cost controller is designed for a mixed-flow two-spool turbofan engine to ensure its dynamical performance under networked conditions. The linear state-space engine model is first identified, based on which a networked engine control(NEC) system is established where the transmission delay and the packet dropout are considered simultaneously. Then the networked guaranteed cost control theory is introduced which guarantees both the robustness against delay/dropout and the satisfactory dynamic performance. This controller design is formulated as an optimization problem which is solved by the cone complementarity linearization algorithm. In the meanwhile, the corresponding performance index is also calculated, which provides a reference for the future development of the distributed engine control system. Finally, simulations are performed on an aerothermodynamics component-level engine simulator to demonstrate the validity and applicability of the proposed approach.
引文
[1]D.E.Culley,R.Thomas,and J.Saus,“Concepts for distributed engine control,”in 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference&Exhibit,no.AIAA 2007-5709,Cincinnati,OH,2007.
[2]J.A.De Castro,C.A.Palmer,and A.Behbahani,“Meeting the requirements of distributed engine control via decentralized,modular smart sensing,”in 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference&Exhibit,no.AIAA 2010-6748,Nashville,TN,2010.
[3]A.Behbahani and B.Tulpule,“Perspective for distributed intelligent engine controls of the future,”in 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference&Exhibit,no.AIAA 2010-6631,Nashville,TN,2010.
[4]D.Culley,“Transition in gas turbine control system architecture:modular,distributed,and embedded,”in ASME Turbo Expo 2010:Power for Land,Sea,and Air.Glasgow,UK:American Society of Mechanical Engineers,2010,pp.287–297.
[5]A.W.Berner,“Challenges for implementing a distributedcontrol system for turbine engines,”in ASME Turbo Expo2010:Power for Land,Sea,and Air.Glasgow,UK:American Society of Mechanical Engineers,2010,pp.401–407.
[6]R.K.Belapurkar,“Stability and performance of propulsion control systems with distributed control architectures and failures,”Ph.D.dissertation,The Ohio State University,2012.
[7]R.K.Yedavalli,R.K.Belapurkar,and A.Behbahani,“Design of distributed engine control systems for stability under communication packet dropouts,”Journal of Guidance,Control,and Dynamics,vol.32,no.5,pp.1544–1549,2009.
[8]Y.-J.Sun,C.-H.Lien,and J.-G.Hsieh,“Comments on”dstability of continuous time-delay systems subjected to a class of highly structured perturbations”,”IEEE Transactions on Automatic Control,vol.43,no.5,p.689,1998.
[9]D.Huang and S.K.Nguang,“State feedback guaranteed cost control of uncertain networked control systems,”in 1st International Symposium on Systems and Control in Aerospace and Astronautics.IEEE,2006,pp.858–863.
[10]X.Jin-Song,F.Bing-Quan,Y.S.Lee,and Y.Jin,“Guaranteed cost controller design of networked control systems with state delay,”Acta Automatica Sinica,vol.33,no.2,pp.170–174,2007.
[11]T.Bin,L.Guo-Ping,and W.-H.Gui,“Networked guaranteed cost control of uncertain systems,”Control Theory and Applications,vol.25,no.1,pp.105–110,2008.
[12]G.C.Goodwin,S.F.Graebe,and M.E.Salgado,Control system design.Prentice Hall New Jersey,2001,vol.240,ch.22.13,pp.693–695.
[13]E.G.L,O.F,and A.M,“A cone complementarity linearization algorithm for static output-feedback and related problems,”IEEE transactions on Automatic Control,vol.42,no.8,pp.1171–1176,1997.
[14]S.-G.Zhang,Y.-Q.Guo,and J.Lu,“Research on aircraft engine component-level models based on gasturb/matlab,”Journal of Aerospace Power,vol.27,no.12,pp.2850–2856,2012.
[15]L.C.Jaw and J.D.Mattingly,Aircraft engine controls:design,system analysis,and health monitoring.American Institute of Aeronautics and Astronautics,2009.
[2]J.A.De Castro,C.A.Palmer,and A.Behbahani,“Meeting the requirements of distributed engine control via decentralized,modular smart sensing,”in 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference&Exhibit,no.AIAA 2010-6748,Nashville,TN,2010.
[3]A.Behbahani and B.Tulpule,“Perspective for distributed intelligent engine controls of the future,”in 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference&Exhibit,no.AIAA 2010-6631,Nashville,TN,2010.
[4]D.Culley,“Transition in gas turbine control system architecture:modular,distributed,and embedded,”in ASME Turbo Expo 2010:Power for Land,Sea,and Air.Glasgow,UK:American Society of Mechanical Engineers,2010,pp.287–297.
[5]A.W.Berner,“Challenges for implementing a distributedcontrol system for turbine engines,”in ASME Turbo Expo2010:Power for Land,Sea,and Air.Glasgow,UK:American Society of Mechanical Engineers,2010,pp.401–407.
[6]R.K.Belapurkar,“Stability and performance of propulsion control systems with distributed control architectures and failures,”Ph.D.dissertation,The Ohio State University,2012.
[7]R.K.Yedavalli,R.K.Belapurkar,and A.Behbahani,“Design of distributed engine control systems for stability under communication packet dropouts,”Journal of Guidance,Control,and Dynamics,vol.32,no.5,pp.1544–1549,2009.
[8]Y.-J.Sun,C.-H.Lien,and J.-G.Hsieh,“Comments on”dstability of continuous time-delay systems subjected to a class of highly structured perturbations”,”IEEE Transactions on Automatic Control,vol.43,no.5,p.689,1998.
[9]D.Huang and S.K.Nguang,“State feedback guaranteed cost control of uncertain networked control systems,”in 1st International Symposium on Systems and Control in Aerospace and Astronautics.IEEE,2006,pp.858–863.
[10]X.Jin-Song,F.Bing-Quan,Y.S.Lee,and Y.Jin,“Guaranteed cost controller design of networked control systems with state delay,”Acta Automatica Sinica,vol.33,no.2,pp.170–174,2007.
[11]T.Bin,L.Guo-Ping,and W.-H.Gui,“Networked guaranteed cost control of uncertain systems,”Control Theory and Applications,vol.25,no.1,pp.105–110,2008.
[12]G.C.Goodwin,S.F.Graebe,and M.E.Salgado,Control system design.Prentice Hall New Jersey,2001,vol.240,ch.22.13,pp.693–695.
[13]E.G.L,O.F,and A.M,“A cone complementarity linearization algorithm for static output-feedback and related problems,”IEEE transactions on Automatic Control,vol.42,no.8,pp.1171–1176,1997.
[14]S.-G.Zhang,Y.-Q.Guo,and J.Lu,“Research on aircraft engine component-level models based on gasturb/matlab,”Journal of Aerospace Power,vol.27,no.12,pp.2850–2856,2012.
[15]L.C.Jaw and J.D.Mattingly,Aircraft engine controls:design,system analysis,and health monitoring.American Institute of Aeronautics and Astronautics,2009.