Adaptive nonlinear generalized predictive control for hypersonic vehicle with unknown parameters and control constraints

In this article, an adaptive nonlinear generalized predictive controller is developed for the hypersonic vehicle with unknown parameter uncertainties and control surface constraints. A nominal controller based on generalized predictive control is first developed for the nominal longitudinal model. Considering the complicated practical flying environment and outer unknown disturbances, a parametric longitudinal dynamics model of the hypersonic vehicle is constructed. Then, an adaptive parameter estimation method is proposed to update the unknown controller parameters and parameter projection is applied to solve the control singularity and the parameter boundedness problem. Control surface is restricted to deflect in a range. To satisfy the above constraint, the predictive time should be selected appropriately. Through a large number of simulation experiments, the suitable ranges of the predictive time under different commands are given. All closed-loop signals are guaranteed to be bounded. And simulation results verify the effectiveness of the proposed controller.

[1]  Zhen Liu,et al.  Adaptive trajectory tracking control system design for hypersonic vehicles with parametric uncertainty , 2015 .

[2]  Yufei Xu,et al.  Passive Fault-Tolerant Control Design for Near-Space Hypersonic Vehicle Dynamical System , 2012, Circuits Syst. Signal Process..

[3]  Yufei Wang,et al.  Attitude tracking control for variable structure near space vehicles based on switched nonlinear systems , 2013 .

[4]  Chen Hong.  Nonlinear Model Predictive Control: The State and Open Problems , 2001 .

[5]  Yao Yu,et al.  Some Control Problems for Near Space Hypersonic Vehicles , 2013 .

[6]  Hamid Reza Karimi,et al.  Fuzzy Reliable Tracking Control for Flexible Air-breathing Hypersonic Vehicles , 2011 .

[7]  Jason Levin,et al.  Flight dynamic characteristics of a scramjet-powered generic hypersonic vehicle , 2009, 2009 American Control Conference.

[8]  Huijun Gao,et al.  Reference output tracking control for a flexible air-breathing hypersonic vehicle via output feedback , 2012 .

[9]  Vincent Cocquempot,et al.  Adaptive fault‐tolerant backstepping control against actuator gain faults and its applications to an aircraft longitudinal motion dynamics , 2013 .

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

[11]  Zhongke Shi,et al.  Neural control of hypersonic flight vehicle model via time-scale decomposition with throttle setting constraint , 2013, Nonlinear Dynamics.

[12]  Danwei W. Wang,et al.  Dynamic Surface Control of Constrained Hypersonic Flight Models with Parameter Estimation and Actuator Compensation , 2014 .

[13]  Mou Chen,et al.  Disturbance-Observer-Based Robust Flight Control for Hypersonic Vehicles Using Neural Networks , 2011 .

[14]  Vincent Cocquempot,et al.  Fuzzy Logic System-Based Adaptive Fault-Tolerant Control for Near-Space Vehicle Attitude Dynamics With Actuator Faults , 2013, IEEE Transactions on Fuzzy Systems.

[15]  Ruiyun Qi,et al.  Adaptive output feedback fault-tolerant control design for hypersonic flight vehicles , 2015, J. Frankl. Inst..

[16]  Wen-Hua Chen,et al.  Tracking control of small-scale helicopters using explicit nonlinear MPC augmented with disturbance observers , 2012 .

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

[18]  Ruiyun Qi,et al.  Adaptive backstepping control for a hypersonic vehicle with uncertain parameters and actuator faults , 2013, J. Syst. Control. Eng..

[19]  Peter J. Gawthrop,et al.  Optimal control of nonlinear systems: a predictive control approach , 2003, Autom..

[20]  Wang Qing,et al.  Robust adaptive control for hypersonic vehicle based on dynamic inversion , 2011 .

[21]  Bailing Tian,et al.  Multiple-time scale smooth second order sliding mode controller design for flexible hypersonic vehicles , 2015 .

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

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

[24]  Shu Lin,et al.  Model Predictive Control — Status and Challenges , 2013 .

[25]  Chenguang Yang,et al.  Global Neural Dynamic Surface Tracking Control of Strict-Feedback Systems With Application to Hypersonic Flight Vehicle , 2015, IEEE Transactions on Neural Networks and Learning Systems.

[26]  Yuri B. Shtessel,et al.  SLIDING MODE CONTROL OF THE X-33 VEHICLE IN LAUNCH AND RE-ENTRY MODES * , 1998 .

[27]  H. Khalil,et al.  Adaptive output feedback control of nonlinear systems represented by input-output models , 1994, Proceedings of 1994 33rd IEEE Conference on Decision and Control.

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

[29]  Meng Bin.  REVIEW ON THE CONTROL OF HYPERSONIC FLIGHT VEHICLES , 2009 .

[30]  Bin Jiang,et al.  Robust attitude control of near space vehicles with time-varying disturbances , 2013 .

[31]  Zhongke Shi,et al.  An overview on flight dynamics and control approaches for hypersonic vehicles , 2015, Science China Information Sciences.

[32]  Wu Hong-xin.  Characteristic Model-Based Adaptive Attitude Control for Hypersonic Vehicle , 2010 .

[33]  Jitao Sun,et al.  Approximate controllability of abstract stochastic impulsive systems with multiple time-varying delays , 2013 .

[34]  Changyin Sun,et al.  Robust adaptive integral-sliding-mode fault-tolerant control for airbreathing hypersonic vehicles , 2012, J. Syst. Control. Eng..

[35]  Peng Shi,et al.  Fault-tolerant control design for near-space vehicles based on a dynamic terminal sliding mode technique , 2012, J. Syst. Control. Eng..

[36]  Ian R. Petersen,et al.  Feedback linearization-based robust nonlinear control design for hypersonic flight vehicles , 2013, J. Syst. Control. Eng..

[37]  F. Allgöwer,et al.  A quasi-infinite horizon nonlinear model predictive control scheme with guaranteed stability , 1997 .

[38]  Bin Jiang,et al.  Fault-Tolerant Control for T–S Fuzzy Systems With Application to Near-Space Hypersonic Vehicle With Actuator Faults , 2012, IEEE Transactions on Fuzzy Systems.

[39]  Jinzhi Wang,et al.  Observer-based fault-tolerant control for an air-breathing hypersonic vehicle model , 2014 .

[40]  Zhao Guo-ron.  Evolution of Nonlinear Model Predictive Control Research , 2014 .

[41]  Yu Shu-you.  Review of fundamental properties and topics of model predictive control for nonlinear systems , 2013 .

[42]  Qun Zong,et al.  Command filtered back-stepping control of a flexible air-breathing hypersonic flight vehicle , 2014 .

[43]  Dongbing Gu,et al.  Receding horizon tracking control of wheeled mobile robots , 2006, IEEE Transactions on Control Systems Technology.

[44]  Bin Xu,et al.  Robust adaptive neural control of flexible hypersonic flight vehicle with dead-zone input nonlinearity , 2015 .

[45]  Zengqi Sun,et al.  Fuzzy tracking control design for hypersonic vehicles via T-S model , 2011, Science China Information Sciences.