Robust adaptive integral-sliding-mode fault-tolerant control for airbreathing hypersonic vehicles

In this article, the problem of robust fault-tolerant tracking control is investigated for the longitudinal model of airbreathing hypersonic vehicle in the presence of actuator faults and external disturbances. First, a fault-tolerant control strategy based on finite time integral sliding mode is presented for the longitudinal model of airbreathing hypersonic vehicle, which guarantees that velocity and altitude track their reference signals in finite time. However, this method needs to know the minimum value of actuator efficiency factor and the upper bound of external disturbances. Then, an improved adaptive fault-tolerant control scheme is developed, where two adaptive laws are used to estimate the upper bound of external disturbances and the minimum value of actuator efficiency factor. Finally, simulation results show that the proposed control strategy is effective in rejecting external disturbances and handling actuator faults.

[1]  Anuradha M. Annaswamy,et al.  Adaptive control of hypersonic vehicles in the presence of modeling uncertainties , 2009, 2009 American Control Conference.

[2]  Li Hui-feng,et al.  Index approach law based sliding control for a hypersonic aircraft , 2008, 2008 2nd International Symposium on Systems and Control in Aerospace and Astronautics.

[3]  Petros A. Ioannou,et al.  Adaptive Sliding Mode Control Design fo ra Hypersonic Flight Vehicle , 2004 .

[4]  Baris Fidan,et al.  Flight Dynamics and Control of Air-Breathing Hypersonic Vehicles: Review and New Directions , 2003 .

[5]  Zengqi Sun,et al.  Fuzzy dynamic characteristic modeling and adaptive control of nonlinear systems and its application to hypersonic vehicles , 2011, Science China Information Sciences.

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

[7]  Yufei Xu,et al.  Fault Tolerant Control for a Class of Nonlinear Systems with Application to Near Space Vehicle , 2011, Circuits Syst. Signal Process..

[8]  Zhihong Man,et al.  Non-singular terminal sliding mode control of rigid manipulators , 2002, Autom..

[9]  Qinglei Hu,et al.  Robust fault-tolerant control for spacecraft attitude stabilisation subject to input saturation , 2011 .

[10]  Yanze Hou,et al.  Stability Analysis of Switched Linear Systems with Locally Overlapped Switching Law , 2010 .

[11]  Guang-Hong Yang,et al.  Adaptive Reliable $H_{\infty}$ Filtering Against Sensor Failures , 2007, IEEE Transactions on Signal Processing.

[12]  Dennis S. Bernstein,et al.  Finite-Time Stability of Continuous Autonomous Systems , 2000, SIAM J. Control. Optim..

[13]  Qun Zong,et al.  Brief paper: Higher order sliding mode control with self-tuning law based on integral sliding mode , 2010 .

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

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

[16]  Huai-Ning Wu,et al.  Active fault-tolerant fuzzy control design of nonlinear model tracking with application to chaotic systems , 2009 .

[17]  Peng Shi,et al.  Fault-tolerant control for a near space vehicle with a stuck actuator fault based on a Takagi-Sugeno fuzzy model , 2010 .

[18]  Changyin Sun,et al.  Composite controller design for an airbreathing hypersonic vehicle , 2012, J. Syst. Control. Eng..

[19]  Qun Zong,et al.  Output feedback back-stepping control for a generic Hypersonic Vehicle via small-gain theorem , 2012 .

[20]  Petros A. Ioannou,et al.  Robust Neural Adaptive Control of a Hypersonic Aircraft , 2003 .

[21]  Michael A. Bolender,et al.  NONLINEAR ROBUST/ADAPTIVE CONTROLLER DESIGN FOR AN AIR- BREATHING HYPERSONIC VEHICLE MODEL (PREPRINT) , 2007 .

[22]  Yao Zhang,et al.  Output feedback control of hypersonic vehicles based on neural network and high gain observer , 2011, Science China Information Sciences.

[23]  Georgi M. Dimirovski,et al.  Output feedback control for uncertain linear systems with faulty actuators based on a switching method , 2009 .

[24]  Shumin Fei,et al.  FINITE-TIME CONTROL OF A BIOREACTOR SYSTEM USING TERMINAL SLIDING MODE , 2009 .

[25]  Xinghuo Yu,et al.  Terminal sliding mode control design for uncertain dynamic systems , 1998 .

[26]  Lingjie Chen,et al.  Stability and Stabilization of a Class of Multimode Linear Discrete-Time Systems With Polytopic Uncertainties , 2009, IEEE Transactions on Industrial Electronics.

[27]  Han Ho Choi,et al.  LMI-Based Sliding Surface Design for Integral Sliding Mode Control of Mismatched Uncertain Systems , 2007, IEEE Transactions on Automatic Control.

[28]  Fuchun Sun,et al.  Multi-objective robust control based on fuzzy singularly perturbed models for hypersonic vehicles , 2011, Science China Information Sciences.

[29]  Yanze Hou,et al.  Stability analysis and stabilisation of full-envelope networked flight control systems: switched system approach , 2012 .

[30]  Guang-Hong Yang,et al.  Adaptive Fault-Tolerant Tracking Control Against Actuator Faults With Application to Flight Control , 2006, IEEE Transactions on Control Systems Technology.

[31]  Robert F. Stengel,et al.  Robust Nonlinear Control of a Hypersonic Aircraft , 1999 .

[32]  Dennis S. Bernstein,et al.  Geometric homogeneity with applications to finite-time stability , 2005, Math. Control. Signals Syst..

[33]  Youmin Zhang,et al.  Bibliographical review on reconfigurable fault-tolerant control systems , 2003, Annu. Rev. Control..

[34]  Fuchun Sun,et al.  Adaptive discrete-time controller design with neural network for hypersonic flight vehicle via back-stepping , 2011, Int. J. Control.

[35]  A. Serrani,et al.  Nonlinear Robust Adaptive Control of Flexible Air-Breathing Hypersonic Vehicles , 2009 .

[36]  Huijun Gao,et al.  Guaranteed cost control with poles assignment for a flexible air-breathing hypersonic vehicle , 2011, Int. J. Syst. Sci..

[37]  Peng Shi,et al.  Stability, ${l}_{2}$ -Gain and Asynchronous ${H}_{{\infty}}$ Control of Discrete-Time Switched Systems With Average Dwell Time , 2009, IEEE Transactions on Automatic Control.

[38]  Huai-Ning Wu,et al.  H∞ fuzzy control design of discrete‐time nonlinear active fault‐tolerant control systems , 2009 .

[39]  David B. Doman,et al.  Nonlinear Longitudinal Dynamical Model of an Air-Breathing Hypersonic Vehicle , 2007 .

[40]  Yufei Xu,et al.  Adaptive Fault-Tolerant Tracking Control of Near-Space Vehicle Using Takagi–Sugeno Fuzzy Models , 2010, IEEE Transactions on Fuzzy Systems.

[41]  Ian R. Petersen,et al.  Robust nonlinear control design of a hypersonic flight vehicle using minimax linear quadratic Gaussian control , 2010, 49th IEEE Conference on Decision and Control (CDC).

[42]  Christopher I. Marrison,et al.  Design of Robust Control Systems for a Hypersonic Aircraft , 1998 .

[43]  Hongming Gao,et al.  Multi-Objective Fault-Tolerant Output Tracking Control of a Flexible Air-Breathing Hypersonic Vehicle , 2010 .

[44]  James Lam,et al.  Necessary and Sufficient Conditions for Analysis and Synthesis of Markov Jump Linear Systems With Incomplete Transition Descriptions , 2010, IEEE Transactions on Automatic Control.

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

[46]  Bin Yao,et al.  High performance adaptive robust control of nonlinear systems: a general framework and new schemes , 1997, Proceedings of the 36th IEEE Conference on Decision and Control.

[47]  Kumpati S. Narendra,et al.  Adaptive control using multiple models, switching and tuning , 2003 .

[48]  Ye Zhao,et al.  Asynchronous Filtering of Discrete-Time Switched Linear Systems With Average Dwell Time , 2011, IEEE Transactions on Circuits and Systems I: Regular Papers.