Adaptive Nonsingular Terminal Sliding Mode Control for Attitude Tracking of Spacecraft With Actuator Faults

In this paper, an adaptive nonsingular terminal sliding mode control (ANTSMC) is investigated for attitude tracking of spacecraft with actuator faults. First, a nonsingular fast terminal sliding mode surface is designed to avoid the singularity. Finite-time attitude control is developed using the nonsingular terminal sliding mode technique, which can make the attitude and angular velocity tracking errors converge to zero in finite time in the presence of uncertainties and external disturbances. Second, the total uncertainty is deduced to be bounded. The adaptive laws are incorporated to develop the ANTSMC, removing the restriction on the upper bound of the lumped uncertainty. The finite-time convergence of the closed-loop system with ANTSMC is proved using the Lyapunov stability theory. Finally, the simulation results are presented to demonstrate the performance of the proposed controllers.

[1]  Ming Liu,et al.  Anti-Disturbance Backstepping Attitude Control for Rigid-Flexible Coupling Spacecraft , 2018, IEEE Access.

[2]  Mingyu Fu,et al.  A Robust Finite-Time Output Feedback Control Scheme for Marine Surface Vehicles Formation , 2018, IEEE Access.

[3]  Shihua Li,et al.  Finite-Time Attitude Tracking Control of Spacecraft With Application to Attitude Synchronization , 2011, IEEE Transactions on Automatic Control.

[4]  K. Cai,et al.  Globally Stabilizing Proportional-Integral-Derivative Control Laws for Rigid-Body Attitude Tracking , 2011 .

[5]  Yuanqing Xia,et al.  Finite-Time Attitude Control for Rigid Spacecraft Based on Adaptive Super-Twisting Algorithm , 2014, Finite Time and Cooperative Control of Flight Vehicles.

[6]  Jan Tommy Gravdahl,et al.  Spacecraft attitude control using explicit model predictive control , 2005, Autom..

[7]  Yuanqing Xia,et al.  Attitude stabilization of rigid spacecraft with finite‐time convergence , 2011 .

[8]  Michael I. Friswell,et al.  Fixed-Time Attitude Control for Rigid Spacecraft With Actuator Saturation and Faults , 2016, IEEE Transactions on Control Systems Technology.

[9]  Danwei Wang,et al.  Active Fault-Tolerant Control System Design for Spacecraft Attitude Maneuvers with Actuator Saturation and Faults , 2019, IEEE Transactions on Industrial Electronics.

[10]  Naser Pariz,et al.  RETRACTED ARTICLE: Immersion and invariance based fault tolerant adaptive spacecraft attitude control , 2014 .

[11]  Chutiphon Pukdeboon,et al.  Nonsingular terminal sliding mode based finite-time control for spacecraft attitude tracking , 2014 .

[12]  Yuanqing Xia,et al.  Adaptive attitude tracking control for rigid spacecraft with finite-time convergence , 2013, Autom..

[13]  Jyh-Ching Juang,et al.  An LMI-based nonlinear attitude control approach , 2003, IEEE Trans. Control. Syst. Technol..

[14]  Zhifeng Gao,et al.  Active fault-tolerant control approach design for rigid spacecraft with multiple actuator faults , 2018, J. Syst. Control. Eng..

[15]  Lei Guo,et al.  Adaptive Fault-Tolerant Attitude Tracking Control of Spacecraft With Prescribed Performance , 2017, IEEE/ASME Transactions on Mechatronics.

[16]  Fang Wang,et al.  Finite-time sliding mode attitude control for rigid spacecraft without angular velocity measurement , 2017, J. Frankl. Inst..

[17]  Seyed Majid Smaeilzadeh,et al.  A finite-time adaptive robust control for a spacecraft attitude control considering actuator fault and saturation with reduced steady-state error , 2019 .

[18]  A. Aihua Zhang,et al.  Finite Time Fault Tolerant Attitude Control-Based Observer for a Rigid Satellite Subject to Thruster Faults , 2017, IEEE Access.

[19]  Yong Guo,et al.  Terminal Sliding Mode Control for Attitude Tracking of Spacecraft under Input Saturation , 2017 .

[20]  Yuanqing Xia,et al.  Finite‐time attitude control of multiple rigid spacecraft using terminal sliding mode , 2015 .

[21]  An-Min Zou,et al.  Finite-time attitude tracking control for rigid spacecraft with control input constraints , 2017 .

[22]  Jianping Yuan,et al.  Fast spacecraft adaptive attitude tracking control through immersion and invariance design , 2017 .

[23]  Xi Liu,et al.  Finite-Time Attitude Tracking Control for Spacecraft Using Terminal Sliding Mode and Chebyshev Neural Network , 2011, IEEE Transactions on Systems, Man, and Cybernetics, Part B (Cybernetics).

[24]  Zhifeng Gao,et al.  Active Fault Tolerant Control Scheme for Satellite Attitude Systems: Multiple Actuator Faults Case , 2018, International Journal of Control, Automation and Systems.

[25]  Mohammad Haeri,et al.  Finite time control of robotic manipulators with position output feedback , 2017 .

[26]  Youmin Zhang,et al.  Finite-Time Attitude Tracking of Spacecraft With Fault-Tolerant Capability , 2015, IEEE Transactions on Control Systems Technology.

[27]  Keck Voon Ling,et al.  Inverse optimal adaptive control for attitude tracking of spacecraft , 2005, IEEE Trans. Autom. Control..

[28]  Xiaowei Shao,et al.  Learning observer based and event-triggered control to spacecraft against actuator faults , 2018, Aerospace Science and Technology.

[29]  Shen-Min Song,et al.  Robust Finite-time Attitude Tracking Control of Rigid Spacecraft Under Actuator Saturation , 2018 .

[30]  Qinglei Hu,et al.  Active fault‐tolerant attitude control for flexible spacecraft with loss of actuator effectiveness , 2013 .

[31]  Yuanli Cai,et al.  Fixed-time control for spacecraft attitude tracking based on quaternion , 2015 .

[32]  Shihua Li,et al.  Finite-Time Attitude Stabilization for a Spacecraft Using Homogeneous Method , 2012 .

[33]  Wenchuan Cai,et al.  Indirect Robust Adaptive Fault -Tolerant Control for Attitude Tracking of Spacecraft , 2008 .

[34]  Zhaowei Sun,et al.  Robust controllers design with finite time convergence for rigid spacecraft attitude tracking control , 2008 .

[35]  Yingmin Jia,et al.  Finite-time output feedback attitude stabilisation for rigid spacecraft with input constraints , 2016 .

[36]  Zhao Wang,et al.  Comments on the paper: Robust controllers design with finite time convergence for rigid spacecraft attitude tracking control , 2011 .

[37]  Mingxuan Sun,et al.  Adaptive Backstepping Control Design for Uncertain Rigid Spacecraft With Both Input and Output Constraints , 2018, IEEE Access.