Adaptive back‐stepping sliding mode attitude control of missile systems

SUMMARY This paper is devoted to the attitude control of a quaternion missile model, which is nonlinear in aerodynamics with atmospheric moment uncertainties, inertia uncertainties, bounded disturbances and actuator failures. By employing the back-stepping technique, the corresponding sliding mode controller is designed to guarantee the state variables of the closed loop system to converge to a small region of the reference states with the help of the adaptive law by estimating the total uncertainties, and be chatter-free. Also, simulation results are presented to illustrate the effectiveness of the control strategy. Copyright © 2013 John Wiley & Sons, Ltd.

[1]  Shihua Li,et al.  Stabilization of the attitude of a rigid spacecraft with external disturbances using finite-time control techniques , 2009 .

[2]  H.-Y. Chen,et al.  Adaptive sliding control with self-tuning fuzzy compensation for a piezoelectrically actuated X–Y table , 2010 .

[3]  Kai-Yew Lum,et al.  Passive Actuators' Fault-Tolerant Control for Affine Nonlinear Systems , 2010, IEEE Transactions on Control Systems Technology.

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

[5]  Ali Cinar,et al.  An adaptive fault‐tolerant control framework with agent‐based systems , 2012 .

[6]  Shihua Li,et al.  Global set stabilization of the spacecraft attitude control problem based on quaternion , 2010 .

[7]  Alexander L. Fradkov,et al.  Method of passification in adaptive control, estimation, and synchronization , 2006 .

[8]  Syuan-Yi Chen,et al.  Robust Nonsingular Terminal Sliding-Mode Control for Nonlinear Magnetic Bearing System , 2011, IEEE Transactions on Control Systems Technology.

[9]  Panagiotis Tsiotras.  Further passivity results for the attitude control problem , 1998, IEEE Trans. Autom. Control..

[10]  Jie Huang,et al.  Attitude Tracking and Disturbance Rejection of Rigid Spacecraft by Adaptive Control , 2009, IEEE Transactions on Automatic Control.

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

[12]  Tzu-Chun Kuo,et al.  Adaptive Sliding-Mode Control for NonlinearSystems With Uncertain Parameters , 2008, IEEE Transactions on Systems, Man, and Cybernetics, Part B (Cybernetics).

[13]  Yuanqing Xia,et al.  Robust Sliding-Mode Control for Uncertain Time-Delay Systems Based on Delta Operator , 2009, IEEE Transactions on Industrial Electronics.

[14]  Yuanqing Xia,et al.  Active disturbance rejection control for uncertain multivariable systems with time-delay , 2007 .

[15]  Yuanqing Xia,et al.  Design of Static Output Feedback Sliding Mode Control for Uncertain Linear Systems , 2010, IEEE Transactions on Industrial Electronics.

[16]  Jake Nease,et al.  An integrated fault diagnosis and safe‐parking framework for fault‐tolerant control of nonlinear systems , 2012 .

[17]  Anthony B. Page,et al.  Nonlinear adaptive and sliding mode flight path control of F/A-18 model , 2003 .

[18]  Yaote Chang,et al.  Adaptive Sliding Mode Control of Multi-Input Nonlinear Systems With Perturbations to Achieve Asymptotical Stability , 2009, IEEE Transactions on Automatic Control.

[19]  Yury Stepanenko,et al.  A Sliding Mode Controller with Improved Adaptation Laws for the Upper Bounds on the Norm of Uncertainties , 1998, Autom..

[20]  Baolin Wu,et al.  Decentralized Robust Adaptive Control for Attitude Synchronization Under Directed Communication Topology , 2011 .

[21]  Elbrous M. Jafarov,et al.  Robust sliding-mode control for the uncertain MIMO aircraft model F-18 , 2000, IEEE Trans. Aerosp. Electron. Syst..

[22]  B. Friedland.  Analysis Strapdown Navigation Using Quaternions , 1978, IEEE Transactions on Aerospace and Electronic Systems.

[23]  Weibing Gao,et al.  Variable structure control of nonlinear systems: a new approach , 1993, IEEE Trans. Ind. Electron..

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

[25]  Qi Li,et al.  Global set stabilisation of the spacecraft attitude using finite-time control technique , 2009, Int. J. Control.

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

[27]  Jin Young Choi,et al.  Adaptive control for feedback-linearized missiles with uncertainties , 2000, IEEE Trans. Aerosp. Electron. Syst..

[28]  Alexander L. Fradkov,et al.  Combined adaptive controller for UAV guidance , 2003, 2003 European Control Conference (ECC).

[29]  Yeon Fuh Jiang,et al.  Error analysis of quaternion transformations (inertial navigation) , 1991 .

[30]  Yuanqing Xia,et al.  Back-stepping sliding mode control for missile systems based on an extended state observer , 2011 .

[31]  Marios M. Polycarpou,et al.  Decentralized Fault Tolerant Control of a Class of Interconnected Nonlinear Systems , 2011, IEEE Transactions on Automatic Control.

[32]  Yuanqing Xia,et al.  Adaptive Backstepping Controller Design for Stochastic Jump Systems , 2009, IEEE Transactions on Automatic Control.

[33]  Seung-Hwan Kim,et al.  Robust Control of the Missile Attitude Based on Quaternion Feedback , 2001 .

[34]  Yuanqing Xia,et al.  Attitude Tracking of Rigid Spacecraft With Bounded Disturbances , 2011, IEEE Transactions on Industrial Electronics.