Adaptive control for uncertain dynamical systems with nonlinear reference systems

被引:6
作者
Gruenwald, Benjamin C. [1 ]
Yucelen, Tansel [2 ]
De La Torre, Gerardo [3 ]
Muse, Jonathan A. [4 ]
机构
[1] Army Res Lab, Flight Sci Branch, Aberdeen Proving Ground, MD USA
[2] Univ S Florida, Dept Mech Engn, 4202 East Fowler Ave, Tampa, FL 33620 USA
[3] Northrop Grumman, Mission Syst, Chicago, IL USA
[4] Air Force Res Lab, Aerosp Syst Directorate, Wright Patterson AFB, OH USA
基金
美国国家航空航天局;
关键词
Uncertain dynamical systems; stabilisation and command following; adaptive control; nonlinear reference models; transient and steady-state performance; FLIGHT CONTROL; ROBUSTNESS; STABILITY; INVERSION;
D O I
10.1080/00207721.2020.1737269
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 reference model of an adaptive control law defines how a closed-loop dynamical system under consideration has to asymptotically (or approximately) behave in the presence of system uncertainties. While it is of common practice to use reference models with linear dynamics, this can lead to limitations on the achievable closed-loop dynamical system performance - especially for applications involving highly capable dynamical systems such as highly manoeuvrable aircraft, missiles, and space launch vehicles. Because, linear reference models for these applications can only approximate the desired closed-loop behaviour of these nonlinear dynamical systems in narrow regions of the state-space. Motivated from this standpoint, this paper's contribution is to present a new adaptive control architecture for uncertain dynamical systems based on nonlinear reference models. Specifically, we analytically show that the system error between the uncertain dynamical system and the nonlinear reference model asymptotically vanishes in steady-state and its performance is guaranteed during the transient-time. We further discuss the practicality of our approach and provide numerical examples to demonstrate its efficacy.
引用
收藏
页码:687 / 703
页数:17
相关论文
共 43 条
[1]   Stability and robustness analysis of nonlinear systems via contraction metrics and SOS programming [J].
Aylward, Erin M. ;
Parrilo, Pablo A. ;
Slotine, Jean-Jacques E. .
AUTOMATICA, 2008, 44 (08) :2163-2170
[2]  
Chellaboina V, 2001, IEEE DECIS CONTR P, P3230, DOI 10.1109/CDC.2001.980317
[3]  
Dydek ZT, 2010, IEEE CONTR SYST MAG, V30, P32, DOI 10.1109/MCS.2010.936292
[4]   Nonlinear Robust Adaptive Control of Flexible Air-Breathing Hypersonic Vehicles [J].
Fiorentini, Lisa ;
Serrani, Andrea ;
Bolender, Michael A. ;
Doman, David B. .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2009, 32 (02) :402-417
[5]  
Haddad W., 2008, Nonlinear Dynamical Systems and Control: A Lyapunov-Based Approach
[6]   Robust adaptive control for nonlinear uncertain systems [J].
Haddad, WM ;
Hayakawa, T ;
Chellaboina, V .
AUTOMATICA, 2003, 39 (03) :551-556
[7]   Direct adaptive control for non-linear uncertain systems with exogenous disturbances [J].
Haddad, WM ;
Hayakawa, T .
INTERNATIONAL JOURNAL OF ADAPTIVE CONTROL AND SIGNAL PROCESSING, 2002, 16 (02) :151-172
[8]   INSTABILITY ANALYSIS AND IMPROVEMENT OF ROBUSTNESS OF ADAPTIVE-CONTROL [J].
IOANNOU, PA ;
KOKOTOVIC, PV .
AUTOMATICA, 1984, 20 (05) :583-594
[9]  
Ioannou PA, 2012, ROBUST ADAPTIVE CONT
[10]   Disturbance-observer-based nonlinear friction compensation in table drive system [J].
Iwasaki, M ;
Shibata, T ;
Matsui, N .
IEEE-ASME TRANSACTIONS ON MECHATRONICS, 1999, 4 (01) :3-8