Robust finite-time adaptive control algorithm for satellite fast attitude maneuver

Abstract A robust adaptive finite-time controller for satellite fast attitude maneuver is proposed in this paper. The finite-time sliding mode is proposed based on standard sliding mode, hence the terminal convergence rate could be largely improved, and the inherent robustness to some typical perturbations is maintained. A new method is proposed to deal with the singularity issue based on the property of Euler rotation. In order to deal with inertia matrix uncertainty, finite-time adaptive law for inertia matrix estimation variables is proposed. Considering that the variable estimation system has no direct feedback, an auxiliary state converging slower than system is designed to achieve finite-time stability. The overall global finite-time stability is proved by Lyapunov method and the performance of the controller is demonstrated by numerical simulation results.

[1]  Okyay Kaynak,et al.  Tracking Control of Robotic Manipulators With Uncertain Kinematics and Dynamics , 2016, IEEE Transactions on Industrial Electronics.

[2]  Yu Guo,et al.  Robust adaptive attitude tracking coordination control for spacecraft formation with unknown time-varying inertia , 2019 .

[3]  Jing Na,et al.  Adaptive neural network control for robotic manipulators with guaranteed finite-time convergence , 2019, Neurocomputing.

[4]  Zhengrong Xiang,et al.  Finite‐time output tracking for a class of switched nonlinear systems , 2017 .

[5]  Yan Xiao,et al.  Finite time fault-tolerant attitude control for rigid-flexible coupling satellites based on Legendre neural network , 2018 .

[6]  Bangchun Wen,et al.  A fuzzy adaptive backstepping control based on mass observer for trajectory tracking of a quadrotor UAV , 2018, International Journal of Adaptive Control and Signal Processing.

[7]  Joseph Z. Ben-Asher,et al.  Time-Efficient Angular Steering Laws for Rigid Satellite , 2011 .

[8]  Ming Liu,et al.  Finite-Time Control for Spacecraft Formation with Dual-Number-Based Description , 2012 .

[9]  Zhaowei Sun,et al.  Finite-time attitude synchronization controllers design for spacecraft formations via behavior-based approach , 2013 .

[10]  Bing Xiao,et al.  Adaptive attitude tracking control of a 3-degrees-of-freedom experimental helicopter with actuator dead-zone , 2019, J. Syst. Control. Eng..

[11]  Vaios Lappas,et al.  Rapid Rotational Maneuvering of Rigid Satellites with Hybrid Actuators Configuration , 2013 .

[12]  Sun Zhaowei,et al.  Time Efficient Robust PID Plus Controller for Satellite Attitude Stabilization Control Considering Angular Velocity and Control Torque Constraint , 2017 .

[13]  Liang Sun,et al.  Saturated Adaptive Hierarchical Fuzzy Attitude-Tracking Control of Rigid Spacecraft With Modeling and Measurement Uncertainties , 2019, IEEE Transactions on Industrial Electronics.

[14]  Zong-Yao Sun,et al.  Fast Finite-Time Partial State Feedback Stabilization of High-Order Nonlinear Systems with Dynamic Uncertainties , 2019, 2019 12th Asian Control Conference (ASCC).

[15]  Li You,et al.  Near time-optimal controller based on analytical trajectory planning algorithm for satellite attitude maneuver , 2019, Aerospace Science and Technology.

[16]  Shunan Wu,et al.  Quaternion-based finite time control for spacecraft attitude tracking , 2011 .

[17]  Liang Sun,et al.  Attitude Tracking Control of Gravity Gradient Microsatellite in Maneuvering for Space Exploration , 2018, Microgravity Science and Technology.

[18]  Hamid Reza Karimi,et al.  Simultaneous Input and State Estimation for Integrated Motor-Transmission Systems in a Controller Area Network Environment via an Adaptive Unscented Kalman Filter , 2020, IEEE Transactions on Systems, Man, and Cybernetics: Systems.

[19]  Baris Fidan,et al.  Adaptive Linear Quadratic Attitude Tracking Control of a Quadrotor UAV Based on IMU Sensor Data Fusion , 2019, Sensors.

[20]  Lin Zhao,et al.  Adaptive fuzzy finite-time command filtered tracking control for permanent magnet synchronous motors , 2019, Neurocomputing.

[21]  Yuanqing Xia,et al.  Exponential Stabilization of Takagi–Sugeno Fuzzy Systems With Aperiodic Sampling: An Aperiodic Adaptive Event-Triggered Method , 2019, IEEE Transactions on Systems, Man, and Cybernetics: Systems.

[22]  Zhaowei Sun,et al.  Time efficient sliding mode controller based on Bang–Bang logic for satellite attitude control , 2018 .

[23]  Qinglei Hu,et al.  Robust Backstepping Sliding Mode Attitude Tracking and Vibration Damping of Flexible Spacecraft with Actuator Dynamics , 2009 .

[24]  Hamid Reza Karimi,et al.  An Adaptive Event-Triggered Synchronization Approach for Chaotic Lur’e Systems Subject to Aperiodic Sampled Data , 2019, IEEE Transactions on Circuits and Systems II: Express Briefs.

[25]  Shen Yin,et al.  Velocity-Free Fault-Tolerant and Uncertainty Attenuation Control for a Class of Nonlinear Systems , 2016, IEEE Transactions on Industrial Electronics.

[26]  Xibin Cao,et al.  Flexible satellite attitude maneuver via constrained torque distribution and active vibration suppression , 2017 .

[27]  Lihua Xie,et al.  Robust track‐following control of hard disk drives using improved integral sliding mode combined with phase lead peak filter , 2008 .

[28]  Zhaowei Sun,et al.  Finite time control strategy for satellite attitude maneuver based on hybrid actuator , 2018, Trans. Inst. Meas. Control.

[29]  Ligang Wu,et al.  A Structure Simple Controller for Satellite Attitude Tracking Maneuver , 2017, IEEE Transactions on Industrial Electronics.

[30]  Zhaowei Sun,et al.  Dual-quaternion-based finite-time control for spacecraft tracking in six degrees of freedom , 2013 .

[31]  Zhaowei Sun,et al.  Robust finite time control algorithm for satellite attitude control , 2017 .

[32]  Ljupco Kocarev,et al.  Twisting-Based Finite-Time Consensus for Euler–Lagrange Systems With an Event-Triggered Strategy , 2020, IEEE Transactions on Network Science and Engineering.

[33]  Qinglei Hu.  Sliding mode maneuvering control and active vibration damping of three-axis stabilized flexible spacecraft with actuator dynamics , 2008 .

[34]  Shunan Wu,et al.  Robust Finite-Time Control for Flexible Spacecraft Attitude Maneuver , 2014 .