Design of Full-envelope Flight Control Based on the MDADT
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- 英文论文题名：Design of Full-envelope Flight Control Based on the MDADT
- 论文作者：Qing Wang ; Xiaohui Liang ; Chaoyang Dong
- 英文论文作者：Qing Wang ; Xiaohui Liang ; Chaoyang Dong ; Department of Automation Science and Electrical Engineering ; Beihang University ; Department of Aeronautic Science and Engineering ; Beihang University
- 年：2017
- 作者机构：Department of Automation Science and Electrical Engineering,Beihang University;Department of Aeronautic Science and Engineering,Beihang University;
- 英文论文关键词：MDADT ; full-envelope flight controller ; switched linear system ; stability criterion ; HiMAT
- 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：V249.1
- 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：7
- 文件大小：994k
- 原文格式：D
- 会议级别：全国
摘要
With the regarding to the demand that the parameters vary rapidly over a wide range for the highly maneuverable technology(Hi MAT) vehicle, a switched linear model with the locally overlapped characteristic is established for a full-envelope flight. Based on the mode-dependent average dwell time(MDADT) method, a stability criterion for the above switched linear model is proposed, and an application to a full-envelope flight controller is designed, which shows fewer restrictions than that of the average dwell time(ADT). Furthermore, a numerical simulation is given to prove the correctness and feasibility of this method.
With the regarding to the demand that the parameters vary rapidly over a wide range for the highly maneuverable technology(Hi MAT) vehicle, a switched linear model with the locally overlapped characteristic is established for a full-envelope flight. Based on the mode-dependent average dwell time(MDADT) method, a stability criterion for the above switched linear model is proposed, and an application to a full-envelope flight controller is designed, which shows fewer restrictions than that of the average dwell time(ADT). Furthermore, a numerical simulation is given to prove the correctness and feasibility of this method.
With the regarding to the demand that the parameters vary rapidly over a wide range for the highly maneuverable technology(Hi MAT) vehicle, a switched linear model with the locally overlapped characteristic is established for a full-envelope flight. Based on the mode-dependent average dwell time(MDADT) method, a stability criterion for the above switched linear model is proposed, and an application to a full-envelope flight controller is designed, which shows fewer restrictions than that of the average dwell time(ADT). Furthermore, a numerical simulation is given to prove the correctness and feasibility of this method.
引文
[1]Zhang J,Li F,Yang X,Stability Analysis of Switched Systems.New York:Springer International Publishing,2016.
[2]Xu L,Wang Q,Li W,Hou Y,Stability analysis and stabilisation of full-envelope networked flight control systems:switched system approach.IET Control Theory&Applications,6(2):286-296,2012.
[3]Yang D,Zhao J,Hf output tracking control for a class of switched LPV systems and its application to an aero-engine model.International Journal of Robust&Nonlinear Control.2016.
[4]Yang H,Jiang B,Gong H J,Fault Recoverability of Switched Systems with Application to Longitudinal Flight Process,AIAA Guidance,Navigation,and Control Conference,2013.
[5]Dong C Y,Li W,Wang Q,Hf Control of Switched Systems with Nonideal Switchings and its Application to Morphing Aircraft,Procedia Engineering.67(67):100-109,2013.
[6]Zhao X,Shi P,Yin Y,Nguang SK,New Results on Stability of Slowly Switched Systems:A Multiple Discontinuous Lyapunov Function Approach,IEEE Transactions on Automatic Control,99:1-1,2016.
[7]Zhang L,Zhuang S,Braatz RD,Switched model predictive control of switched linear systems:Feasibility,stability and robustness,Automatica,67:8-21,2016
[8]Ali Bagherzadeh M,Ghaisari J,Askari J,Robust exponential stability and stabilisation of parametric uncertain switched linear systems under arbitrary switching,IET Control Theory&Applications,10(4):381-90,2016
[9]Deaecto G S,Dynamic output feedback Hf control of continuous-time switched affine systems,Automatica,71:44-49,2016
[10]Liberzon D,Morse A S,Basic problems in stability and design of switched systems,IEEE Control Systems Magazine,19(5):59-70,2010.
[11]Zhao X,Zhang L,Shi P,Liu M,Stability and Stabilization of Switched Linear Systems With Mode-Dependent Average Dwell Time.IEEE Transactions on Automatic Control,57(7):1809-1815,2012.
[12]Hespanha J P,Morse A S.Stability of switched systems with average dwell-time,in Proceedings of the 38th IEEE Conference on Decision and Control,1999:2655-2660
[13]Zhao X,Yin S,Li H,Niu B,Switching Stabilization for a Class of Slowly Switched Systems,IEEE Transactions on Automatic Control,60(1):221-226,2015.
[14]Hou Y,Dong C,Wang Q.Stability Analysis of Switched Linear Systems with Locally Overlapped Switching Law,Journal of Guidance,Control,and Dynamics,33(2):396-403,2010.
[15]Hou Y,Wang Q,Dong C,Gain Scheduled Control:Switched Polytopic System Approach,Journal of Guidance,Control,and Dynamics,34(2):623-629,2011.
[16]Hartmann GL,Barrett MF,Greene C S,Control design for an unstable vehicle,NASA CR-170393,1980.
[17]Liu S,Kramer J,Indiveri G,Delbrück T,Linear Systems Theory,CRC Press,2009.
[2]Xu L,Wang Q,Li W,Hou Y,Stability analysis and stabilisation of full-envelope networked flight control systems:switched system approach.IET Control Theory&Applications,6(2):286-296,2012.
[3]Yang D,Zhao J,Hf output tracking control for a class of switched LPV systems and its application to an aero-engine model.International Journal of Robust&Nonlinear Control.2016.
[4]Yang H,Jiang B,Gong H J,Fault Recoverability of Switched Systems with Application to Longitudinal Flight Process,AIAA Guidance,Navigation,and Control Conference,2013.
[5]Dong C Y,Li W,Wang Q,Hf Control of Switched Systems with Nonideal Switchings and its Application to Morphing Aircraft,Procedia Engineering.67(67):100-109,2013.
[6]Zhao X,Shi P,Yin Y,Nguang SK,New Results on Stability of Slowly Switched Systems:A Multiple Discontinuous Lyapunov Function Approach,IEEE Transactions on Automatic Control,99:1-1,2016.
[7]Zhang L,Zhuang S,Braatz RD,Switched model predictive control of switched linear systems:Feasibility,stability and robustness,Automatica,67:8-21,2016
[8]Ali Bagherzadeh M,Ghaisari J,Askari J,Robust exponential stability and stabilisation of parametric uncertain switched linear systems under arbitrary switching,IET Control Theory&Applications,10(4):381-90,2016
[9]Deaecto G S,Dynamic output feedback Hf control of continuous-time switched affine systems,Automatica,71:44-49,2016
[10]Liberzon D,Morse A S,Basic problems in stability and design of switched systems,IEEE Control Systems Magazine,19(5):59-70,2010.
[11]Zhao X,Zhang L,Shi P,Liu M,Stability and Stabilization of Switched Linear Systems With Mode-Dependent Average Dwell Time.IEEE Transactions on Automatic Control,57(7):1809-1815,2012.
[12]Hespanha J P,Morse A S.Stability of switched systems with average dwell-time,in Proceedings of the 38th IEEE Conference on Decision and Control,1999:2655-2660
[13]Zhao X,Yin S,Li H,Niu B,Switching Stabilization for a Class of Slowly Switched Systems,IEEE Transactions on Automatic Control,60(1):221-226,2015.
[14]Hou Y,Dong C,Wang Q.Stability Analysis of Switched Linear Systems with Locally Overlapped Switching Law,Journal of Guidance,Control,and Dynamics,33(2):396-403,2010.
[15]Hou Y,Wang Q,Dong C,Gain Scheduled Control:Switched Polytopic System Approach,Journal of Guidance,Control,and Dynamics,34(2):623-629,2011.
[16]Hartmann GL,Barrett MF,Greene C S,Control design for an unstable vehicle,NASA CR-170393,1980.
[17]Liu S,Kramer J,Indiveri G,Delbrück T,Linear Systems Theory,CRC Press,2009.