A longitudinal trajectory tracking method with L1 adaptive control for hypersonic reentry vehicles

被引:5
|
作者
Han, GenSen [1 ]
Zhou, Jun [1 ]
Guo, JianGuo [1 ]
Lu, Qing [1 ]
机构
[1] Northwestern Polytech Univ, Inst Precis Guidance & Control, Xian 710072, Shaanxi, Peoples R China
基金
中国国家自然科学基金;
关键词
Hypersonic vehicle; trajectory tracking; optimal control; Script capital L-1 adaptive control; uncertainty estimate; LINEARIZATION CONTROL; GUIDANCE; DESIGN; GENERATION;
D O I
10.1177/0142331219872598
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper presents a longitudinal trajectory tracking scheme with L1 adaptive control for hypersonic reentry vehicles (HRVs). A linear time-varying (LTV) multiple input multiple output (MIMO) model, in which influences of lateral states, earth rotation, and linearization are considered as model uncertainties, is derived based on state and input errors of longitudinal model. The normalization of error model is used to reduce differences of magnitude orders in state and input matrix elements which may affect the stability of L1 adaptive controller. In order to achieve an accurate tracking performance, a linear quadratic regulator (LQR) controller is employed as the baseline controller, augmented with an L1 adaptive controller to attenuate the matched and unmatched uncertainties. Based on the augmented controller, the optimization process is executed with the estimate of uncertainties at the same time. The simulation results of LQR controller, L1 augmentation controller and robust H infinity controller show that the L1 adaptive control method can reduce the terminal and integral of squared state errors validly. Terminal state errors in all simulation scenarios are less than 2.5m/s, 1e-3 and 10m, respectively, which reflects its effectiveness in increasing robustness of baseline controller.
引用
收藏
页码:386 / 403
页数:18
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