Barrier Lyapunov function based adaptive finite-time control for hypersonic flight vehicles with state constraints

被引:81
作者
Dong, Chaoyang [1 ]
Liu, Yang [1 ]
Wang, Qing [2 ]
机构
[1] Beihang Univ, Sch Aeronaut Sci & Engn, Beijing, Peoples R China
[2] Beihang Univ, Sch Automat Sci & Elect Engn, Beijing, Peoples R China
基金
中国国家自然科学基金;
关键词
Hypersonic flight vehicle; Barrier Lyapunov function; Finite-time convergence; Flight state constraint; Adaptive backstepping; FEEDBACK NONLINEAR-SYSTEMS; FAULT-TOLERANT CONTROL; TRACKING CONTROL; BACKSTEPPING CONTROL; INPUT SATURATION; STABILIZATION; DESIGN;
D O I
10.1016/j.isatra.2019.06.011
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 investigates the finite-time tracking control problem of the hypersonic flight vehicle (HFV) with state constraints. Firstly, a control-oriented model is introduced to enable the application of adaptive backstepping scheme. To meet strict requirements in terms of working conditions of HFV, barrier Lyapunov function is adopted to constrain the tracking errors, while piecewise saturation function is constructed to restrict the virtual signals. To guarantee the finite-time convergent property of HFV dynamics, an adaptive scheme in accordance with finite-time stability theory is designed. Meanwhile, a sliding mode differentiator is employed to estimate the derivatives of the virtual control laws. Novel auxiliary systems are then designed to consider the side effects of the possible saturation and to maintain the finite-time convergent property. In the final stage, the effectiveness and performance of the proposed method is demonstrated by numerical simulations. (C) 2019 ISA. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:163 / 176
页数:14
相关论文
共 49 条
[21]   Barrier Lyapunov Functions-based adaptive control for a class of nonlinear pure-feedback systems with full state constraints [J].
Liu, Yan-Jun ;
Tong, Shaocheng .
AUTOMATICA, 2016, 64 :70-75
[22]   Adaptive fuzzy control of a class of nonaffine nonlinear system with input saturation based on passivity theorem [J].
Molavi, Ali ;
Jalali, Aliakbar ;
Naraghi, Mandi Ghasemi .
ISA TRANSACTIONS, 2017, 69 :202-213
[23]   Flight-Test Experiment Design for Characterizing Stability and Control of Hypersonic Vehicles [J].
Morelli, Eugene A. .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2009, 32 (03) :949-959
[24]   Barrier Lyapunov functions for the output tracking control of constrained nonlinear switched systems [J].
Niu, Ben ;
Zhao, Jun .
SYSTEMS & CONTROL LETTERS, 2013, 62 (10) :963-971
[25]   Control-oriented modeling of an air-breathing hypersonic vehicle [J].
Parker, Jason T. ;
Serrani, Andrea ;
Yurkovich, Stephen ;
Bolender, Michael A. ;
Doman, David B. .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2007, 30 (03) :856-869
[26]   Feedback linearization-based robust nonlinear control design for hypersonic flight vehicles [J].
Rehman, Obaid Ur ;
Petersen, Ian R. ;
Fidan, Baris .
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART I-JOURNAL OF SYSTEMS AND CONTROL ENGINEERING, 2013, 227 (I1) :3-11
[27]   Adaptive Neural Control for Output Feedback Nonlinear Systems Using a Barrier Lyapunov Function [J].
Ren, Beibei ;
Ge, Shuzhi Sam ;
Tee, Keng Peng ;
Lee, Tong Heng .
IEEE TRANSACTIONS ON NEURAL NETWORKS, 2010, 21 (08) :1339-1345
[28]   Experimental Study of Test-Medium Vitiation Effects on Dual-Mode Scramjet Performance [J].
Rockwell, Robert D., Jr. ;
Goyne, Christopher P. ;
Haw, Willie ;
Krauss, Roland H. ;
McDaniel, James C. ;
Trefny, Charles J. .
JOURNAL OF PROPULSION AND POWER, 2011, 27 (05) :1135-1142
[29]   Finite-time tracking control of hypersonic vehicle with input saturation [J].
Sun, Jing-Guang ;
Xu, Sheng-Li ;
Song, Shen-Min ;
Dong, Xi-Jun .
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 71 :272-284
[30]   State-Estimator-Integrated Robust Adaptive Tracking Control for Flexible Air-Breathing Hypersonic Vehicle With Noisy Measurements [J].
Tao, Xinlong ;
Yi, Jianqiang ;
Pu, Zhiqiang ;
Xiong, Tianyi .
IEEE TRANSACTIONS ON INSTRUMENTATION AND MEASUREMENT, 2019, 68 (11) :4285-4299