Trajectory tracking of solid launch vehicle in ascending based on differential inclusion stabilization

被引:0
作者
Liu F. [1 ]
Wang S. [1 ]
Yang M. [1 ]
Chao T. [1 ]
机构
[1] Control and Simulation Center, Harbin Institute of Technology, Harbin
来源
Zhongguo Guanxing Jishu Xuebao/Journal of Chinese Inertial Technology | 2022年 / 30卷 / 03期
关键词
Deviation stabilization; Differential inclusion system; Solid launch vehicles; Trajectory tracking;
D O I
10.13695/j.cnki.12-1222/o3.2022.03.015
中图分类号
学科分类号
摘要
Aiming at the problem that the traditional solid launched vehicles (SLV) trajectory tracking method cannot adapt to a large range of parameter uncertainties, a differential inclusion stabilization based trajectory tracking controller is proposed. Firstly, the uncertainties are combined with the dynamic equation to establish the differential inclusion system about the state deviations. Secondly, a state feedback law based on linear matrix inequality (LMI) is designed to stabilize the polytopic part of differential inclusion systems to solve the large range parameter uncertainties. Then, the magnitude constraints of the correction of the angle of attack and sideslip are transformed into LMI. Finally, an adaptive law is designed to estimate the disturbance in the differential inclusion system. Combined with the state feedback law and the control variable constraints, a differential inclusion adaptive saturated trajectory tracking controller is constructed. The simulation results show that the terminal state deviations converge and meet the terminal accuracy within the given parameter uncertainty ranges. Compared with the tracking controller based on extended state observer, the proposed controller widens the applicable uncertainty boundaries. © 2022, Editorial Department of Journal of Chinese Inertial Technology. All right reserved.
引用
收藏
页码:378 / 387
页数:9
相关论文
共 20 条
[1]  
Zheng J, Chang J, Et al., Trajectory optimization for a TBCC-powered supersonic vehicle with transition thrust pinch, Aerospace Science and Technology, 84, pp. 214-222, (2019)
[2]  
Wang H, Zhang R, Liang Z, Et al., Orbital guidance method for solid rocket based on improved sequential convex optimization, Journal of Chinese Inertial Technology, 29, 1, pp. 119-125, (2021)
[3]  
Lu P., Entry guidance and trajectory control for a reusable launch vehicle, Journal of Guidance Control and Dynamics, 20, pp. 143-149, (1997)
[4]  
Kartal Y, Kolaric P, Lopez V, Et al., Backstepping approach for design of PID controller with guaranteed performance for micro-air UAV, Control Theory and Technology, 18, 1, pp. 19-33, (2019)
[5]  
Lichota P, Dul F, Karbowski A., System identification and LQR controller design with incomplete state observation for aircraft trajectory tracking, Energies, 13, 20, pp. 5354-5381, (2020)
[6]  
Chao T, Wang Y, Wang S, Et al., Trajectory tracking control for non-minimum phase hypersonic vehicles, Systems Engineering and Electronics, 40, 7, pp. 1548-1553, (2018)
[7]  
Chen X, Wang X., Study of landing control of unmanned helicopter based on sliding mode variable structure, Ordance Industry Automation, 38, 2, pp. 11-15, (2019)
[8]  
Nie W, Li H, Zhang R., Model-free adaptive optimal design for trajectory tracking control of rocket-powered vehicle, Chinese Journal of Aeronautics, 33, 6, pp. 1703-1716, (2022)
[9]  
Lei R, Chen L., Decentralized fault-tolerant control for dual-arm space robot based on state observation, Journal of Chinese Inertial Technology, 27, 2, pp. 248-254, (2019)
[10]  
Liu J, Gai W, Zhang J, Et al., Nonlinear adaptive backstepping with ESO for the quadrotor trajectory tracking control in the multiple disturbances, International Journal of Control, Automation and Systems, 17, 11, pp. 2754-2768, (2019)