Distributed coordinated control for satellite formation system with communication delay
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- 英文论文题名：Distributed coordinated control for satellite formation system with communication delay
- 论文作者：Yalan Zhou ; Yanchao Sun ; Chuanjiang Li ; Mengmeng Liu
- 英文论文作者：Yalan Zhou ; Yanchao Sun ; Chuanjiang Li ; Mengmeng Liu ; Harbin Institute of Technology
- 年：2017
- 作者机构：Harbin Institute of Technology;
- 英文论文关键词：satellite formation ; finite-time control ; neural network ; distributed coordinated control
- 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：V448.2
- 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：1757k
- 原文格式：D
- 会议级别：全国
摘要
When a follower satellite is tracking the leader satellite, the communication delay will affect the tracking performance. To solve this problem, we build a dynamic model based on directed communication topology. Then we use neural network to obtain the real-time estimate of model uncertainties and external disturbances, and use adaptive control to compensate for residual effects. Based on nonsingular terminal sliding-mode control and neural network, we propose a finite-time control for the follower satellite to track the leader under the effect of communication delay. Lyapunov method is used to prove the finite-time stability. Simulation results are also provided to show the effectiveness of the control law.
When a follower satellite is tracking the leader satellite, the communication delay will affect the tracking performance. To solve this problem, we build a dynamic model based on directed communication topology. Then we use neural network to obtain the real-time estimate of model uncertainties and external disturbances, and use adaptive control to compensate for residual effects. Based on nonsingular terminal sliding-mode control and neural network, we propose a finite-time control for the follower satellite to track the leader under the effect of communication delay. Lyapunov method is used to prove the finite-time stability. Simulation results are also provided to show the effectiveness of the control law.
When a follower satellite is tracking the leader satellite, the communication delay will affect the tracking performance. To solve this problem, we build a dynamic model based on directed communication topology. Then we use neural network to obtain the real-time estimate of model uncertainties and external disturbances, and use adaptive control to compensate for residual effects. Based on nonsingular terminal sliding-mode control and neural network, we propose a finite-time control for the follower satellite to track the leader under the effect of communication delay. Lyapunov method is used to prove the finite-time stability. Simulation results are also provided to show the effectiveness of the control law.
引文
[1]Y.C.Sun,G.F.Ma,M.M.Liu,and L.M.Chen,Distributed finite-time configuration containment control for satellite formation,Proceedings of the Institution of Mechanical Engineers Part G:Journal of Aerospace Engineering,Epub ahead of print,DOI:10.1177/0954410016656877,2016
[2]S.D'Amico,J.S.Ardaens,and R.Larsson,Spaceborne autonomous formation-flying experiment on the PRISMA mission,Journal of Guidance,Control,and Dynamics,35(3):834-850,2012.
[3]H.C.Lim,and H.Bang,Adaptive control for satellite formation flying under thrust misalignment,Acta Astronautica,65(1-2):112-122,2009.
[4]H.Liu,J.F.Li,and B.Y.Hexi,Sliding mode control for low-thrust earth-orbiting spacecraft formation maneuvering,Aerosp Sci Technol,10:636-643,2006.
[5]Z.Y.Meng,W.Ren,and Z.You,Decentralized cooperative attitude tracking using modified rodriguez parameters based on relative attitude information,International Journal of Control,83:2427-2439,2010.
[6]S.R.Sahoo,and R.N.Banavar,Attitude synchronization of satellites with internal actuation,European Journal of Control,20:152-161,2014.
[7]W.Ren,Distributed cooperative attitude synchronization and tracking for multiple rigid bodies,IEEE Transactions on Control Systems Technology,18(2):383-392,2010.
[8]H.Min,S.Wang,F.Sun,et al,Decentralized adaptive attitude synchronization of spacecraft formation,Systems&Control Letters,61(1):238-246,2012.
[9]F.C.Liu,J.Mei,and G.F.Ma,Formation control for relative translation of modular spacecraft with unknown disturbances,Control and Decision,29(6):985-990,2014.
[10]Y.C.Sun,L.M.Chen,G.F.Ma,and C.J.Li,Adaptive neural network tracking control for multiple uncertain Euler-Lagrange systems with communication delays,Journal of the Franklin Institute,Epub ahead of print,DOI:10.1016/j.jfranklin.2017.01.021,2017.
[11]M.Hu,and G.J.Zeng,Finite-time control for satellite formation flight,Aerospace Control and Application,38(1):23-28,2012.
[12]Q.L.Hu,J.Zhang,and G.F.Ma,L2-gain based adaptive sliding mode coordinated attitude control of satellite formation with time-varying delays,Systems Engineering and Electronics,35(11):2356-2363,2013.
[13]B.Q.Zhang,S.M.Song,and X.L.Chen,Robust coordinated control for formation flying satellites with time delays and switching topologies,Journal of Astronautics,33(7):910-919,2012.
[14]Y.C.Sun,W.J.Wang,G.F.Ma,Z.Li,and C.J.Li,Backstepping-based distributed coordinated tracking for multiple uncertain Euler-Lagrange systems,Journal of Systems Engineering and Electronics,27(5):1083-1095,2016.
[15]L.Yang,and J.Y.Yang,Nonsingular fast terminal sliding-mode control for nonlinear dynamical systems,International Journal of Robust and Nonlinear Control,21(16):1865-1879,2011.
[16]S.Mondal,and C.Mahanta,Adaptive second-order sliding mode controller for a twin rotor multi-input-multi-output system,IET Control Theory&Applications,6(14):2157-2167,2012.
[2]S.D'Amico,J.S.Ardaens,and R.Larsson,Spaceborne autonomous formation-flying experiment on the PRISMA mission,Journal of Guidance,Control,and Dynamics,35(3):834-850,2012.
[3]H.C.Lim,and H.Bang,Adaptive control for satellite formation flying under thrust misalignment,Acta Astronautica,65(1-2):112-122,2009.
[4]H.Liu,J.F.Li,and B.Y.Hexi,Sliding mode control for low-thrust earth-orbiting spacecraft formation maneuvering,Aerosp Sci Technol,10:636-643,2006.
[5]Z.Y.Meng,W.Ren,and Z.You,Decentralized cooperative attitude tracking using modified rodriguez parameters based on relative attitude information,International Journal of Control,83:2427-2439,2010.
[6]S.R.Sahoo,and R.N.Banavar,Attitude synchronization of satellites with internal actuation,European Journal of Control,20:152-161,2014.
[7]W.Ren,Distributed cooperative attitude synchronization and tracking for multiple rigid bodies,IEEE Transactions on Control Systems Technology,18(2):383-392,2010.
[8]H.Min,S.Wang,F.Sun,et al,Decentralized adaptive attitude synchronization of spacecraft formation,Systems&Control Letters,61(1):238-246,2012.
[9]F.C.Liu,J.Mei,and G.F.Ma,Formation control for relative translation of modular spacecraft with unknown disturbances,Control and Decision,29(6):985-990,2014.
[10]Y.C.Sun,L.M.Chen,G.F.Ma,and C.J.Li,Adaptive neural network tracking control for multiple uncertain Euler-Lagrange systems with communication delays,Journal of the Franklin Institute,Epub ahead of print,DOI:10.1016/j.jfranklin.2017.01.021,2017.
[11]M.Hu,and G.J.Zeng,Finite-time control for satellite formation flight,Aerospace Control and Application,38(1):23-28,2012.
[12]Q.L.Hu,J.Zhang,and G.F.Ma,L2-gain based adaptive sliding mode coordinated attitude control of satellite formation with time-varying delays,Systems Engineering and Electronics,35(11):2356-2363,2013.
[13]B.Q.Zhang,S.M.Song,and X.L.Chen,Robust coordinated control for formation flying satellites with time delays and switching topologies,Journal of Astronautics,33(7):910-919,2012.
[14]Y.C.Sun,W.J.Wang,G.F.Ma,Z.Li,and C.J.Li,Backstepping-based distributed coordinated tracking for multiple uncertain Euler-Lagrange systems,Journal of Systems Engineering and Electronics,27(5):1083-1095,2016.
[15]L.Yang,and J.Y.Yang,Nonsingular fast terminal sliding-mode control for nonlinear dynamical systems,International Journal of Robust and Nonlinear Control,21(16):1865-1879,2011.
[16]S.Mondal,and C.Mahanta,Adaptive second-order sliding mode controller for a twin rotor multi-input-multi-output system,IET Control Theory&Applications,6(14):2157-2167,2012.