Decentralized H_∞ control for attitude coordination of spacecraft formation
详细信息 查看官网全文
- 英文论文题名：Decentralized H_∞ control for attitude coordination of spacecraft formation
- 论文作者：Pingli Lu ; Gang Liu ; Xiangdong Liu
- 英文论文作者：Pingli Lu ; Gang Liu ; Xiangdong Liu ; School of Automation ; Beijing Institute of Technology
- 年：2017
- 作者机构：School of Automation,Beijing Institute of Technology;
- 英文论文关键词：Attitude coordination ; linear matrix inequality ; nonlinear H∞ control ; multiple spacecraft ; spacecraft formation
- 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（B）
- 英文会议录名称：Proceedings of the 36th Chinese Control Conference（B）
- 语种：英文
- 分类号：V448.22
- 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：282k
- 原文格式：D
- 会议级别：全国
摘要
In this paper, a robust H_∞ decentralized controller is proposed for attitude coordination of spacecraft formation flying with external disturbance based on the relative attitudes and angular velocities of neighboring spacecraft. The controller is composed of nonlinear terms for performance enhancement and linear terms for attitude coordination and stabilization. The proposed control method guarantees the attitude alignment with zero final angular velocity and robust disturbance attenuation for spacecraft formation when the communication topology is connected. A feature of the proposed approach is that the robust H_∞controller parameters can be obtained by solving linear matrix inequalities(LMIs), which makes the design more transparent.Finally, the numerical simulations of a spacecraft formation are provided to show the effectiveness of the proposed consensus algorithm.
In this paper, a robust H_∞ decentralized controller is proposed for attitude coordination of spacecraft formation flying with external disturbance based on the relative attitudes and angular velocities of neighboring spacecraft. The controller is composed of nonlinear terms for performance enhancement and linear terms for attitude coordination and stabilization. The proposed control method guarantees the attitude alignment with zero final angular velocity and robust disturbance attenuation for spacecraft formation when the communication topology is connected. A feature of the proposed approach is that the robust H_∞controller parameters can be obtained by solving linear matrix inequalities(LMIs), which makes the design more transparent.Finally, the numerical simulations of a spacecraft formation are provided to show the effectiveness of the proposed consensus algorithm.
In this paper, a robust H_∞ decentralized controller is proposed for attitude coordination of spacecraft formation flying with external disturbance based on the relative attitudes and angular velocities of neighboring spacecraft. The controller is composed of nonlinear terms for performance enhancement and linear terms for attitude coordination and stabilization. The proposed control method guarantees the attitude alignment with zero final angular velocity and robust disturbance attenuation for spacecraft formation when the communication topology is connected. A feature of the proposed approach is that the robust H_∞controller parameters can be obtained by solving linear matrix inequalities(LMIs), which makes the design more transparent.Finally, the numerical simulations of a spacecraft formation are provided to show the effectiveness of the proposed consensus algorithm.
引文
[1]R.Kristiansen and P.J.Nicklasson,Spacecraft formation flying:A review and new results on state feedback control,Acta Astronautica,65(11-12):1537-1552,2009.
[2]D.P.Scharf,F.Y.Hadegh and S.R.Ploen,A survey of spacecraft formation flying guidance and control(Part 2):Control,Proceeding of the 2004 American Control Conference,2004,June 30-July 2,Boston,Massachusetts.
[3]V.Kapila,A.G.Sparks,J.M.Buffington and Q.Yan,Spacecraft formation flying:Dynamics and control,Journal of Guidance,Control and Dynamics,23(3):561-564,2000.
[4]G.Krieger,I.Hajnsek,K.P.Papathanassiou,M.Younis and A.Moreira,Interferometric synthetic aperture radar(SAR)missions employing formation flying,Proceedings of the IEEE,98(5):816-843,2010.
[5]C.Ma,Q.Zeng and X.Zhao,Distributed adaptive attitude synchronization for spacecraft formation flying with sampled-data information flows,Journal of the Franklin Institute,352(7):2796-2809,2015.
[6]C.He and J.Huang,Unit quaternion-based output feedback control for leader-following attitude consensus of multiple rigid spacecraft systems,Intelligent Control and Automation IEEE:2578-2583,2015.
[7]H.Cai and J.Huang,The leader-following attitude control of multiple rigid spacecraft systems,Automatica,50(4):1109-1115,2014.
[8]B.Xian,C.Diao and B.Zhao,Nonlinear robust output feedback tracking control of a quadrotor UAV using quaternion representation,Nonlinear Dynamics 79(4):2735-2752,2015.
[9]J.Lawton and R.W.Beard,Synchronized multiple spacecraft rotations,Automatica 38(8):1359-1364,2002.
[10]M.C.Vandyke and C.D.Hall,Decentralized Coordinated Attitude Control Within a Formation of Spacecraft,Journal of Guidance Control&Dynamics,29(5):1101-1109,2006.
[11]Z.Meng,W.Ren and Z.You,Distributed finite-time attitude containment control for multiple rigid bodies,Automatica 46:2092-2099,2010.
[12]E.J.Jin,X.L.Jiang and Z.W.Sun,Robust decentralized attitude coordination control of spacecraft formation,Systems and Control Letters 57:567-577,2008.
[13]R.Merris,Laplacian matrices of graphs:a survey,Linear Algebra and its Applications,197-198:143-176,1994.
[14]W.Ren,Synchronized multiple spacecraft rotations:a revisit in the context of consensus building,Proceedings of the 2007American Control Conference,July 2007:3174-3179.
[15]P.C.Hughes,Spacecraft Attitude Dynamics,New York:Dover Publications,2004.
[16]L.L.Show,J.C.Juang and Y.W.Jan,An LMI-based nonlinear attitude control approach,IEEE Transactions on Control Systems Technology,11(1):73-83,2003.
[2]D.P.Scharf,F.Y.Hadegh and S.R.Ploen,A survey of spacecraft formation flying guidance and control(Part 2):Control,Proceeding of the 2004 American Control Conference,2004,June 30-July 2,Boston,Massachusetts.
[3]V.Kapila,A.G.Sparks,J.M.Buffington and Q.Yan,Spacecraft formation flying:Dynamics and control,Journal of Guidance,Control and Dynamics,23(3):561-564,2000.
[4]G.Krieger,I.Hajnsek,K.P.Papathanassiou,M.Younis and A.Moreira,Interferometric synthetic aperture radar(SAR)missions employing formation flying,Proceedings of the IEEE,98(5):816-843,2010.
[5]C.Ma,Q.Zeng and X.Zhao,Distributed adaptive attitude synchronization for spacecraft formation flying with sampled-data information flows,Journal of the Franklin Institute,352(7):2796-2809,2015.
[6]C.He and J.Huang,Unit quaternion-based output feedback control for leader-following attitude consensus of multiple rigid spacecraft systems,Intelligent Control and Automation IEEE:2578-2583,2015.
[7]H.Cai and J.Huang,The leader-following attitude control of multiple rigid spacecraft systems,Automatica,50(4):1109-1115,2014.
[8]B.Xian,C.Diao and B.Zhao,Nonlinear robust output feedback tracking control of a quadrotor UAV using quaternion representation,Nonlinear Dynamics 79(4):2735-2752,2015.
[9]J.Lawton and R.W.Beard,Synchronized multiple spacecraft rotations,Automatica 38(8):1359-1364,2002.
[10]M.C.Vandyke and C.D.Hall,Decentralized Coordinated Attitude Control Within a Formation of Spacecraft,Journal of Guidance Control&Dynamics,29(5):1101-1109,2006.
[11]Z.Meng,W.Ren and Z.You,Distributed finite-time attitude containment control for multiple rigid bodies,Automatica 46:2092-2099,2010.
[12]E.J.Jin,X.L.Jiang and Z.W.Sun,Robust decentralized attitude coordination control of spacecraft formation,Systems and Control Letters 57:567-577,2008.
[13]R.Merris,Laplacian matrices of graphs:a survey,Linear Algebra and its Applications,197-198:143-176,1994.
[14]W.Ren,Synchronized multiple spacecraft rotations:a revisit in the context of consensus building,Proceedings of the 2007American Control Conference,July 2007:3174-3179.
[15]P.C.Hughes,Spacecraft Attitude Dynamics,New York:Dover Publications,2004.
[16]L.L.Show,J.C.Juang and Y.W.Jan,An LMI-based nonlinear attitude control approach,IEEE Transactions on Control Systems Technology,11(1):73-83,2003.