基于干扰观测器的高超声速飞行器预测控制器设计

doi:10.7527/S1000-6893.2013.0390

Abstract

Abstract:

A new kind of attitude controller based on the predictive control method is proposed for hypersonic vehicles with strong coupling characteristics and model uncertainties. Firstly, a novel predictive controller is presented according to the predictive control model combined with the dynamic model of a hypersonic vehicle and an expected reference model, a disturbance observer is designed to compensate timely for the controller and to satisfy the rolling optimization requirements. Secondly, the whole control system stability is strictly proven by Lyapunov stability theory based on the error between the observed value and the real value, and the control accuracy is determined by the predictive length. Finally, the performances and robustness are assessed through a hypersonic vehicle simulation analysis. Several simulation results all show that the predictive controller can guarantee stability and high control precision under the conditions of model parameter nominal and large-scale model parameter perturbation, and the disturbance observer can follow the tracks of the disturbance rapidly.

Key words: hypersonic vehicles, predictive control, reference model, disturbance observer, error bounds

CLC Number:

ZHANG Tianyi, ZHOU Jun, GUO Jianguo. Design of Predictive Controller for Hypersonic Vehicles Based on Disturbance Observer[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(1): 215-222.

References

[1] Yu W B, Chen W C. Guidance scheme for glide range maximization of a hypersonic vehicle, AIAA-2011-6714[R]. Reston: AIAA, 2011.

[2] Morelli E A., Derry S D., Smith M. Aerodynamic parameter estimation for the X-43A from flight data, AIAA-2005-5921[R]. Reston: AIAA, 2005.

[3] Li J, Zuo B, Duan M U, et al. Adaptive terminal sliding mode control for air-breathing hypersonic vehicles under control input constraints[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(2): 220-232. (in Chinese) 李静, 左斌, 段洣毅, 等. 输入受限的吸气式高超声速飞行器自适应Terminal滑模控制[J]. 航空学报, 2012, 33(2): 220-232.

[4] Zhang Z H, Yang L Y, Shen G Z. Switching LPV control method in wide flight envelope for hypersonic vehicles[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(9): 1706-1716. (in Chinese) 张增辉, 杨凌宇, 申功璋. 高超声速飞行器大包线切换LPV控制方法[J]. 航空学报, 2012, 33(9): 1706-1716.

[5] Chen H, Liu Z Y, Xie X H. Nonlinear predictive control: the state and open problems[J]. Control and Decision, 2001, 16(4): 385-391. (in Chinese) 陈虹, 刘志远, 解小华. 非线性模型预测控制的现状与问题[J]. 控制与决策, 2001, 16(4): 385-391.

[6] Rehman O U, Fidan B, Petersen R I. Uncertainty modeling and robust minimax LQR control of hypersonic flight vehicles, AIAA-2010-8285[R]. Reston: AIAA, 2010.

[7] Garcia G A, Keshmiri S. Nonlinear model predictive controller for navigation, guidance and control of a fixed-wing UAV, AIAA-2011-6310[R]. Reston: AIAA, 2011.

[8] Kang Y, Hedrick J K. Linear tracking for a fixed-wing UAV using nonlinear model predictive control[J]. IEEE Transactions on Control Systems Technology, 2009, 17(5): 1202-1210.

[9] Shao X W, Zhang J, Niu Y T. Nonlinear predictive attitude control of hypersonic vehicle[J]. Journal of Ballistics, 2009, 21(4): 42-46. (in Chinese) 邵晓巍, 张军, 牛云涛. 高超声速飞行器的非线性预测姿态控制[J]. 弹道学报, 2009, 21(4): 42-46.

[10] Fang W, Jiang C S. Adaptive variable universe fuzzy predictive control for aerospace vehicle[J]. Control and Decision, 2008, 23(12): 1373-1376. (in Chinese) 方炜, 姜长生. 空天飞行器的自适应变论域模糊预测控制[J]. 控制与决策, 2008, 23(12): 1373-1376.

[11] Fang W, Jiang C S. Nonlinear predictive control of an aerospace vehicle based on adaptive fuzzy systems[J]. Acta Aeronautica et Astronautica Sinica, 2008, 29(4): 988-994. (in Chinese) 方炜, 姜长生. 基于自适应模糊系统的空天飞行器非线性预测控制[J]. 航空学报, 2008, 29(4): 988-994.

[12] Sun Z W, Wu S N, Li H. Variable structure attitude control of staring mode spacecraft with disturbance observer[J]. Journal of Harbin Institute of Technology, 2010, 42(9): 1374-1377. (in Chinese) 孙兆伟, 邬树楠, 李晖. 带有干扰观测器的凝视航天器姿态变结构控制[J]. 哈尔滨工业大学学报, 2010, 42(9): 1374-1377.

[13] Cheng L, Jiang C S, Du Y L. The research of SMDO based NGPC method for NSV control system[J]. Journal of Astronautics, 2010, 31(2): 423-431. (in Chinese) 程路, 姜长生, 都延丽. 基于滑模干扰观测器的近空间飞行器非线性广义预测控制[J]. 宇航学报, 2010, 31(2): 423-431.

[14] Chen W H. Disturbance observer based control for nonlinear systems[J]. IEEE/ASME Transactions on Mechatronics, 2004, 9(4): 706-710.

[15] Zhou F Q, Wang Y, Zhou J. Design of variable structure controller for dynamic vehicle coupling system[J]. Journal of Astronautics, 2011, 32(1): 66-71. (in Chinese) 周凤岐, 王延, 周军. 高超声速飞行器耦合系统变结构控制设计[J]. 宇航学报, 2011, 32(1): 66-71.

[16] Zhou J. The variable structure adaptive control theory and application for uncertain systems[D]. Xi'an: School of Aeronautics, Northwestern Polytechnical University, 1993. (in Chinese) 周军. 不确定系统的变结构自适应控制理论及应用[D]. 西安: 西北工业大学航天学院, 1993.

[17] Li W L, Li J T. Uncertainty observers for uncertainty systems[J]. Control Theory and Application, 2007, 24(6): 933-935. (in Chinese) 李文林, 李均涛. 不确定系统的不确定项观测器设计[J]. 控制理论与应用, 2007, 24(6): 933-935.

Design of Predictive Controller for Hypersonic Vehicles Based on Disturbance Observer

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments

[1]	HU Wei, WAN Wenzhang, CHEN Mou. Neural network and disturbance observer based control for automatic carrier landing of UAV [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S1): 726963-726963.
[2]	YAN Liming, GUO Xin, ZHAO Dongdong. Model predictive torque control of permanent magnet synchronous motor using novel analytic weighting factor assignment [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(12): 327785-327785.
[3]	CHAI Yuan, LUO Jianjun, WANG Mingming. Predictive game control for on-orbit transportation by multiple microsatellites with impulsive thrust [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(12): 326112-326112.
[4]	YAN Liming, ZHAO Dongdong, JIAO Ningfei. Robust model based-predictive torque control of aviation AC induction motor [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(9): 324700-324700.
[5]	GUO Hongzhen, CHEN Mou. Safety formation control of quadrotor UAVs based on prescribed performance [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(8): 525789-525789.
[6]	GAO Chang, LI Zhengzhou, HUANG Jiangtao, HE Yuanyuan, WU Yingchuan, LE Jialing, GUI Feng. High-accuracy aerodynamic optimization of hypersonic vehicles based on continuous adjoint [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(7): 124490-124490.
[7]	ZHAO Dongdong, ZHAO Guosheng, XIA Lei, FANG Chun, MA Rui, HUANGFU Yigeng. Modeling and control of fuel cell cathode gas supply system for UAV [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(7): 324659-324659.
[8]	LU Yao. Backstepping control for hypersonic flight vehicles based on tracking differentiator [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(11): 524737-524737.
[9]	DONG Kaikai, LUO Jianjun, MA Weihua, GAO Dengwei, TAN Longyu. Global trajectory planning and control of rendezvous of non-cooperative targets based on double-layer MPC [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(11): 524903-524903.
[10]	LIU Jinglong, ZHANG Chongfeng, ZOU Huaiwu, LI Ning, WU Linna. On-orbit precise operation control method for flexible joint space robots based on disturbance observer [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(1): 523899-523899.
[11]	SHAO Shuyi, CHEN Mou, ZHAO Qijun. Discrete-time fault-tolerant control for quadrotor UAV based on disturbance observer [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(S2): 724283-724283.
[12]	LI Yaping, WANG Fang, ZHOU Chao. Prescribed performance filter backstepping control of hypersonic vehicle with full state constraints [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(11): 623857-623857.
[13]	PIAO Minnan, CHEN Zhigang, SUN Mingwei, CHEN Zengqiang. Adaptive aeroservoelasticity suppression of hypersonic vehicles [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(11): 623698-623698.
[14]	GUO Jianguo, LU Ningbo, ZHOU Jun. Fuzzy control of finite time attitude coupling in hypersonic vehicles [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(11): 623838-623838.
[15]	WANG Jiawei, ZHANG Ran, HAO Zeming, LI Huifeng. Real-time trajectory optimization for hypersonic vehicles with Proximal-Newton-Kantorovich convex programming [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(11): 624051-624051.