Finite-time integrated guidance and control system for hypersonic vehicles

被引：0

作者：

Chong Zhenyu ^{[1
]}

Guo Jianguo ^{[1
]}

Zhao Bin ^{[1
]}

Guo Zongyi ^{[1
]}

Lu Xiaodong ^{[1
]}

机构：

[1] Northwestern Polytech Univ, Inst Precis Guidance & Control, Youyi West Rd, Xian 710072, Shaanxi, Peoples R China

来源：

TRANSACTIONS OF THE INSTITUTE OF MEASUREMENT AND CONTROL | 2021年 / 43卷 / 04期

基金：

中国国家自然科学基金;

关键词：

Hypersonic vehicle; sliding mode control; integrated guidance and control; finite-time convergence; DESIGN; AUTOPILOT; PHASE;

D O I：

10.1177/0142331220941934

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

A finite-time integrated guidance and control (IGC) method is proposed in this study for hypersonic vehicles. The IGC dynamic model is initially built by combining the 3D relative kinematics and dynamics equations. Then, by introducing the adaptive control technology and the backstepping approach, an IGC scheme with adaptive parameters is presented to guarantee the finite-time stability of a closed-loop control system on the basis of Lyapunov stability theory. Nonlinear simulation results demonstrate the effectiveness and robustness of the proposed IGC method for hypersonic vehicles compared with other robust IGC methods.

引用

页码：842 / 853

页数：12

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