Adaptive tracking control for spacecraft hovering to noncooperative target with trajectory generator

By using the nonlinear line-of-sight (LOS) relative motion model, this paper considers the tracking control for spacecraft hovering problem with mass uncertainty. As a stepping stone, the classical second order system is introduced to construct the dynamic process. Then, by utilizing the skew-symmetric property and a differentiable projection function, an adaptive tracking control scheme is proposed, which allows the convenience of adjusting the system state convergence rate and generated thrust force. The establishment of practical stability of closed-loop error system is guaranteed by Lyapunov’s second method. Finally, simulations are given to demonstrate the system performance with proposed control scheme.

[1]  Hyungjoo Yoon,et al.  Adaptive tracking control of spacecraft relative motion with mass and thruster uncertainties , 2014 .

[2]  Brij N. Agrawal,et al.  Adaptive control of uncertain Hamiltonian Multi-Input Multi-Output systems : With application to spacecraft control , 2009, 2008 American Control Conference.

[3]  G. Duan,et al.  Output feedback elliptical orbital rendezvous via state-dependent Riccati differential equations , 2013 .

[4]  Qiang Cong,et al.  On-orbit service (OOS) of spacecraft: A review of engineering developments , 2019, Progress in Aerospace Sciences.

[5]  Haibo Ji,et al.  Integrated relative position and attitude control for spacecraft rendezvous with ISS and finite-time convergence , 2019, Aerospace Science and Technology.

[6]  Zongxia Jiao,et al.  Robust Nonlinear Adaptive Relative Pose Control for Cooperative Spacecraft During Rendezvous and Proximity Operations , 2017, IEEE Transactions on Control Systems Technology.

[7]  Peng Li,et al.  Line-of-sight nonlinear model predictive control for autonomous rendezvous in elliptical orbit , 2017 .

[8]  Marios M. Polycarpou,et al.  Backstepping-Based Flight Control with Adaptive Function Approximation , 2005 .

[9]  Yi Huang,et al.  Adaptive fixed-time relative position tracking and attitude synchronization control for non-cooperative target spacecraft fly-around mission , 2017, J. Frankl. Inst..

[10]  John D. Childs,et al.  A review of space robotics technologies for on-orbit servicing , 2015 .

[11]  Jingqing Han,et al.  From PID to Active Disturbance Rejection Control , 2009, IEEE Trans. Ind. Electron..

[12]  Anke Xue,et al.  Robust control for spacecraft rendezvous system with actuator unsymmetrical saturation: a gain scheduling approach , 2018, Int. J. Control.

[13]  Guangren Duan,et al.  Robust adaptive integrated translation and rotation control of a rigid spacecraft with control saturation and actuator misalignment , 2013 .

[14]  B. Agrawal,et al.  Novel Expressions of Equations of Relative Motion and Control in Keplerian Orbits , 2009 .

[15]  Yingmin Jia,et al.  Robust adaptive fixed‐time tracking control of 6‐DOF spacecraft fly‐around mission for noncooperative target , 2018 .

[16]  Jianping Yuan,et al.  A novel nonlinear control for tracking and rendezvous with a rotating non-cooperative target with translational maneuver , 2017 .

[17]  Guang-Ren Duan,et al.  Adaptive sliding‐mode control for spacecraft relative position tracking with maneuvering target , 2018, International Journal of Robust and Nonlinear Control.

[18]  Zhijun Cai,et al.  A sufficiently smooth projection operator , 2006, IEEE Transactions on Automatic Control.