Energy-efficient Adaptive Control for Cooperative Spacecraft Rendezvous and Docking
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- 英文论文题名：Energy-efficient Adaptive Control for Cooperative Spacecraft Rendezvous and Docking
- 论文作者：XIA Kewei ; ZHU Bing
- 英文论文作者：XIA Kewei ; ZHU Bing ; The Seventh Research Division ; Science and Technology on Aircraft Control Laboratory ; Beihang University
- 年：2017
- 作者机构：The Seventh Research Division,Science and Technology on Aircraft Control Laboratory,Beihang University;
- 英文论文关键词：Rendezvous and docking ; adaptive control ; energy-efficiency ; optimal 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;V526
- 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：323k
- 原文格式：D
- 会议级别：全国
摘要
An energy-efficient adaptive control is developed for a pursuer spacecraft docking with a cooperative spacecraft.The pursuer spacecraft is subject to parameter uncertainties. A six degree-of-freedom(6-DOF) nonlinear model is expressed by coupled relative attitude and orbit dynamics. In the proposed control, inverse optimality approach is applied, such that the conventional Hamilton-Jacobi-Bellman equation can be avoided, and the controller is energy-efficient. Lyapunov theory is used to prove that the closed-loop systems are asymptotically stable despite of unknown inertial parameters. Numerical simulations demonstrate the effectiveness of our control strategy.
An energy-efficient adaptive control is developed for a pursuer spacecraft docking with a cooperative spacecraft.The pursuer spacecraft is subject to parameter uncertainties. A six degree-of-freedom(6-DOF) nonlinear model is expressed by coupled relative attitude and orbit dynamics. In the proposed control, inverse optimality approach is applied, such that the conventional Hamilton-Jacobi-Bellman equation can be avoided, and the controller is energy-efficient. Lyapunov theory is used to prove that the closed-loop systems are asymptotically stable despite of unknown inertial parameters. Numerical simulations demonstrate the effectiveness of our control strategy.
An energy-efficient adaptive control is developed for a pursuer spacecraft docking with a cooperative spacecraft.The pursuer spacecraft is subject to parameter uncertainties. A six degree-of-freedom(6-DOF) nonlinear model is expressed by coupled relative attitude and orbit dynamics. In the proposed control, inverse optimality approach is applied, such that the conventional Hamilton-Jacobi-Bellman equation can be avoided, and the controller is energy-efficient. Lyapunov theory is used to prove that the closed-loop systems are asymptotically stable despite of unknown inertial parameters. Numerical simulations demonstrate the effectiveness of our control strategy.
引文
[1]R.Kristiansen,P.J.Nicklasson,J.T.Gravdahl.Spacecraft coordination control in 6DOF:Integrator backstepping vs passivity-based control.Automatica,44(11),2896-2901(2008).
[2]K.Subbarao,S.Welsh.Nonlinear control of motion synchronization for satellite proximity operations.J.Guidance,Control&Dynamics.31(5),1284-1294(2008).
[3]F.Zhang,G.R.Duan.Integrated translational and rotational finite-time maneuver of a rigid spacecraft with actuator misalignment.IET control theory&applications.6(9),1192-1204(2012).
[4]K.Xia,W.Huo.Robust nonlinear control for spacecraft rendezvous and docking with disturbance observer.Proceedings of the 35th Chinese Control Conference,Chengdu,China,July 27-29,398-403(2016),
[5]K.Xia,W.Huo.Robust adaptive backstepping neural networks control for spacecraft rendezvous and docking with uncertainties.Nonlinear Dynamics.84(3),1683-1695(2016).
[6]K.Xia,W.Huo.Robust adaptive backstepping neural networks control for spacecraft rendezvous and docking with input saturation.ISA Transactions.62,249-257(2016).
[7]M.Xin,H.J.Pan.Integrated nonlinear optimal control of spacecraft in proximity operations.International Journal of Control.83(2),347-363(2010).
[8]M.Xin,H.J.Pan.Indirect robust control of spacecraft via optimal control solution.IEEE Transactions on Aerospace and Electronic Systems.48(2),1798-1809(2012).
[9]M.Krstic,P.Tsiotras.Inverse optimal stabilization of a rigid spacecraft.IEEE Transactions on Automatic Control.44(5),1042C1049(1999).
[10]W.Luo,Y.C.Chu,K.V.Yang.Inverse optimal adaptive control for attitude tracking of spacecraft.IEEE Transactions on Automatic Control.50(11),1639C1654(2005).
[11]K.Dupree,P.M.Patre,M.Johnson,and W.E.Dixon.Inverse optimal adaptive control of a nonlinear Euler-Lagrange system,Part I:full state feedback.Joint 48th IEEE Conference on Decision and Control and 28th Chinese Control Conference Shanghai,P.R.China,December 16-18,321-326(2009).
[12]J.J.Slotine,W.Li.Applied nonlinear control.Prentice-Hall,USA.1991.
[13]M.J.Sidi.Spacecraft Dynamics and Control:A Practical Engineering Approach.Cambridge University Press,New York.1997.
[14]R.Kristiansen,P.J.Nicklasson.Spacecraft formation flying:a review and new results on state feedback control.Acta Astronautica,65(11),1537-1552(2009).
[15]H.Schaub,J.L.Junkins.Analytical mechanics of space systems.AIAA Education Series,AIAA,Reston,VA,593-601(2003).
[2]K.Subbarao,S.Welsh.Nonlinear control of motion synchronization for satellite proximity operations.J.Guidance,Control&Dynamics.31(5),1284-1294(2008).
[3]F.Zhang,G.R.Duan.Integrated translational and rotational finite-time maneuver of a rigid spacecraft with actuator misalignment.IET control theory&applications.6(9),1192-1204(2012).
[4]K.Xia,W.Huo.Robust nonlinear control for spacecraft rendezvous and docking with disturbance observer.Proceedings of the 35th Chinese Control Conference,Chengdu,China,July 27-29,398-403(2016),
[5]K.Xia,W.Huo.Robust adaptive backstepping neural networks control for spacecraft rendezvous and docking with uncertainties.Nonlinear Dynamics.84(3),1683-1695(2016).
[6]K.Xia,W.Huo.Robust adaptive backstepping neural networks control for spacecraft rendezvous and docking with input saturation.ISA Transactions.62,249-257(2016).
[7]M.Xin,H.J.Pan.Integrated nonlinear optimal control of spacecraft in proximity operations.International Journal of Control.83(2),347-363(2010).
[8]M.Xin,H.J.Pan.Indirect robust control of spacecraft via optimal control solution.IEEE Transactions on Aerospace and Electronic Systems.48(2),1798-1809(2012).
[9]M.Krstic,P.Tsiotras.Inverse optimal stabilization of a rigid spacecraft.IEEE Transactions on Automatic Control.44(5),1042C1049(1999).
[10]W.Luo,Y.C.Chu,K.V.Yang.Inverse optimal adaptive control for attitude tracking of spacecraft.IEEE Transactions on Automatic Control.50(11),1639C1654(2005).
[11]K.Dupree,P.M.Patre,M.Johnson,and W.E.Dixon.Inverse optimal adaptive control of a nonlinear Euler-Lagrange system,Part I:full state feedback.Joint 48th IEEE Conference on Decision and Control and 28th Chinese Control Conference Shanghai,P.R.China,December 16-18,321-326(2009).
[12]J.J.Slotine,W.Li.Applied nonlinear control.Prentice-Hall,USA.1991.
[13]M.J.Sidi.Spacecraft Dynamics and Control:A Practical Engineering Approach.Cambridge University Press,New York.1997.
[14]R.Kristiansen,P.J.Nicklasson.Spacecraft formation flying:a review and new results on state feedback control.Acta Astronautica,65(11),1537-1552(2009).
[15]H.Schaub,J.L.Junkins.Analytical mechanics of space systems.AIAA Education Series,AIAA,Reston,VA,593-601(2003).