SCIENCE CHINA Information Sciences, Volume 64 , Issue 11 : 212201(2021) https://doi.org/10.1007/s11432-019-2823-9

Fixed-time attitude tracking control for spacecraft based on a fixed-time extended state observer

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  • ReceivedOct 17, 2019
  • AcceptedFeb 5, 2020
  • PublishedOct 25, 2021



This work was supported in part by National Natural Science Foundation of China (Grant No. 61720106010), in part by Science and Technology on Space Intelligent Control Laboratory (Grant No. KGJZDSYS-2018-05).


[1] Du H, Li S, Qian C. Finite-Time Attitude Tracking Control of Spacecraft With Application to Attitude Synchronization. IEEE Trans Automat Contr, 2011, 56: 2711-2717 CrossRef Google Scholar

[2] Hu J, Zhang H, Xie Y C. Automatic control system design of Shenzhou spacecraft for rendezvous and docking. Sci Sin-Tech, 2014, 44: 12-19 CrossRef Google Scholar

[3] Dong H, Hu Q, Ma G. Dual-quaternion based fault-tolerant control for spacecraft formation flying with finite-time convergence. ISA Trans, 2016, 61: 87-94 CrossRef Google Scholar

[4] Buzzoni A, Altavilla G, Galleti S. Optical tracking of deep-space spacecraft in Halo L2 orbits and beyond: The Gaia mission as a pilot case. Adv Space Res, 2016, 57: 1515-1527 CrossRef ADS arXiv Google Scholar

[5] Xia K, Huo W. Adaptive control for spacecraft rendezvous subject to actuator faults and saturations. ISA Trans, 2018, 80: 176-186 CrossRef Google Scholar

[6] Cui B, Xia Y, Liu K. Velocity-Observer-Based Distributed Finite-Time Attitude Tracking Control for Multiple Uncertain Rigid Spacecraft. IEEE Trans Ind Inf, 2020, 16: 2509-2519 CrossRef Google Scholar

[7] Xiao B, Friswell M I, Hu Q. Robust fault-tolerant control for spacecraft attitude stabilisation subject to input saturation. IET Control Theor Appl, 2011, 5: 271-282 CrossRef Google Scholar

[8] Huo X, Hu Q, Xiao B. Finite-time fault tolerant attitude stabilization control for rigid spacecraft. ISA Trans, 2014, 53: 241-250 CrossRef Google Scholar

[9] Ma G F, Li B, Yu Y B. Observer-based fault diagnosis incorporating adaptive sliding mode control for spacecraft attitude stabilization. In: Proceedings of the 34th Chinese Control Conference (CCC), 2015. 6224--6229. Google Scholar

[10] Jin E, Sun Z. Robust controllers design with finite time convergence for rigid spacecraft attitude tracking control. Aerospace Sci Tech, 2008, 12: 324-330 CrossRef Google Scholar

[11] An-Min Zou , Kumar K D, Zeng-Guang Hou K D. Finite-Time Attitude Tracking Control for Spacecraft Using Terminal Sliding Mode and Chebyshev Neural Network. IEEE Trans Syst Man Cybern B, 2011, 41: 950-963 CrossRef Google Scholar

[12] Zou A M. Finite-Time Output Feedback Attitude Tracking Control for Rigid Spacecraft. IEEE Trans Contr Syst Technol, 2014, 22: 338-345 CrossRef Google Scholar

[13] Yoo D, Yau S S T, Gao Z. Optimal fast tracking observer bandwidth of the linear extended state observer. Int J Control, 2007, 80: 102-111 CrossRef Google Scholar

[14] Yang J, Cui H, Li S. Optimized Active Disturbance Rejection Control for DC-DC Buck Converters With Uncertainties Using a Reduced-Order GPI Observer. IEEE Trans Circuits Syst I, 2018, 65: 832-841 CrossRef Google Scholar

[15] Lu K, Xia Y, Zhu Z. Sliding mode attitude tracking of rigid spacecraft with disturbances. J Franklin Institute, 2012, 349: 413-440 CrossRef Google Scholar

[16] Xia Y, Yang H, You X. Adaptive control for attitude synchronisation of spacecraft formation via extended state observer. IET Control Theor Appl, 2014, 18: 2171-2185 CrossRef Google Scholar

[17] Hu Q, Shao X, Chen W H. Robust Fault-Tolerant Tracking Control for Spacecraft Proximity Operations Using Time-Varying Sliding Mode. IEEE Trans Aerosp Electron Syst, 2018, 54: 2-17 CrossRef ADS Google Scholar

[18] Yang J, Li T, Liu C. Nonlinearity Estimator-Based Control of A Class of Uncertain Nonlinear Systems. IEEE Trans Automat Contr, 2020, 65: 2230-2236 CrossRef Google Scholar

[19] Venkataraman S T, Gulati S. Terminal sliding modes: a new approach to nonlinear control synthesis, In: Proceedings of International Conference on Advanced Robotics Robots in Unstructured Environments, 1991. 443--448. Google Scholar

[20] Feng Y, Yu X, Man Z. Non-singular terminal sliding mode control of rigid manipulators. Automatica, 2002, 38: 2159-2167 CrossRef Google Scholar

[21] Shen G, Xia Y, Zhang J. Finite-time trajectory tracking control for entry guidance. Int J Robust NOnlinear Control, 2018, 28: 5895-5914 CrossRef Google Scholar

[22] Zhao L, Jia Y. Finite-time attitude tracking control for a rigid spacecraft using time-varying terminal sliding mode techniques. Int J Control, 2015, 88: 1150-1162 CrossRef ADS Google Scholar

[23] Hu Q, Niu G. Attitude output feedback control for rigid spacecraft with finite-time convergence. ISA Trans, 2017, 70: 173-186 CrossRef Google Scholar

[24] Cao L, Qiao D, Chen X. Laplace ?1 Huber based cubature Kalman filter for attitude estimation of small satellite. Acta Astronaut, 2018, 148: 48-56 CrossRef ADS Google Scholar

[25] Xia Y, Zhu Z, Fu M. Back-stepping sliding mode control for missile systems based on an extended state observer. IET Control Theor Appl, 2011, 5: 93-102 CrossRef Google Scholar

[26] Talole S E, Kolhe J P, Phadke S B. Extended-State-Observer-Based Control of Flexible-Joint System With Experimental Validation. IEEE Trans Ind Electron, 2010, 57: 1411-1419 CrossRef Google Scholar

[27] Zhou C, Zhou D. Robust dynamic surface sliding mode control for attitude tracking of flexible spacecraft with an extended state observer. Proc Institution Mech Engineers Part G-J Aerospace Eng, 2017, 231: 533-547 CrossRef Google Scholar

[28] Yang J, Shi X P, Li L, et al. Nonlinear observer based time delay fault-tolerant attitude control for flexible spacecraft during orbit maneuver. In: Proceeding of the 27th Chinese Control and Decision Conference (CCDC), 2015. 50--57. Google Scholar

[29] Zhong C, Guo Y, Yu Z. Finite-time attitude control for flexible spacecraft with unknown bounded disturbance. Trans Institute Measurement Control, 2016, 38: 240-249 CrossRef Google Scholar

[30] Li B, Hu Q, Yu Y. Observer-Based Fault-Tolerant Attitude Control for Rigid Spacecraft. IEEE Trans Aerosp Electron Syst, 2017, 53: 2572-2582 CrossRef ADS Google Scholar

[31] Pukdeboon C. Extended state observer-based third-order sliding mode finite-time attitude tracking controller for rigid spacecraft. Sci China Inf Sci, 2019, 62: 12206 CrossRef Google Scholar

[32] Zhang L, Wei C, Wu R. Fixed-time extended state observer based non-singular fast terminal sliding mode control for a VTVL reusable launch vehicle. Aerospace Sci Tech, 2018, 82-83: 70-79 CrossRef Google Scholar

[33] Hardy G, Littlewood J, Polya G. Inequalities. Cambridge: Cambridge University Press, 1952. Google Scholar

[34] Huang X, Lin W, Yang B. Global finite-time stabilization of a class of uncertain nonlinear systems. Automatica, 2005, 41: 881-888 CrossRef Google Scholar

[35] Kollatc L. Problems on Eigenvalues. Moscow: Science, 1968. Google Scholar

[36] Bhat S P, Bernstein D S. Geometric homogeneity with applications to finite-time stability. Math Control Signals Syst, 2005, 17: 101-127 CrossRef Google Scholar

[37] Yu S, Yu X, Shirinzadeh B. Continuous finite-time control for robotic manipulators with terminal sliding mode. Automatica, 2005, 41: 1957-1964 CrossRef Google Scholar

[38] Polyakov A. Nonlinear Feedback Design for Fixed-Time Stabilization of Linear Control Systems. IEEE Trans Automat Contr, 2012, 57: 2106-2110 CrossRef Google Scholar

[39] Khalil H. Nonlinear Systems. Englewood Cliffs: Prentice-Hall Press, 2002. Google Scholar

[40] Basin M, Yu P, Shtessel Y. Finite- and fixed-time differentiators utilising HOSM techniques. IET Control Theor Appl, 2017, 22: 1144-1152 CrossRef Google Scholar

[41] Lu K, Xia Y, Fu M. Controller design for rigid spacecraft attitude tracking with actuator saturation. Inf Sci, 2013, 220: 343-366 CrossRef Google Scholar

[42] Basin M V, Yu P, Shtessel Y B. Hypersonic Missile Adaptive Sliding Mode Control Using Finite- and Fixed-Time Observers. IEEE Trans Ind Electron, 2018, 65: 930-941 CrossRef Google Scholar


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