Novel model reference adaptive control with application to wing rock example

被引:3
作者
Roshanian, Jafar [1 ]
Rahimzadeh, Ehssan [1 ]
机构
[1] KN Toosi Univ Technol, Dept Aerosp Engn, Tehran, Iran
关键词
New adaptive laws; model reference adaptive control; model reference adaptive control with integral feedback; exponential quadratic Lyapunov function; tracking performance; robustness; wing rock; LYAPUNOV FUNCTIONS; STABILITY ANALYSIS; SYSTEMS; SUPPRESSION; MOTION; MRAC;
D O I
10.1177/0954410020987041
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In this study, we propose new adaptive laws for adjusting the controller parameters of the model reference adaptive control (MRAC) and MRAC with integral feedback schemes. The innovation presented in this study is considering a new form for the Lyapunov function candidate to prove the stability of the closed-loop system. In general, a Lyapunov function candidate contains two sets of quadratic expressions. The first set contains the state tracking error variable, while the second one consists of the controller parameter estimation errors. We prove that by choosing the tracking error quadratic expressions in the form of the exponential function, new adaptive laws that contain the tracking error quadratic expressions are obtained. The difference between the standard MRAC adaptive laws and the proposed new adaptive laws is the state tracking error exponential quadratic expression appears in the adaptive laws. It is shown that the adaptive laws obtained by the exponential quadratic Lyapunov function are similar to those obtained by the quadratic Lyapunov function except that the adaptive gains are variable with time. The advantage of using these new adaptive laws is improving the tracking performance of the closed-loop system, which has been proven analytically and verified by numerical simulations. Also, the robustness analysis of the proposed MRAC controller in the presence of the exogenous disturbance is studied. We consider the single degree of freedom of the wing rock example to evaluate the performance of the designed controllers.
引用
收藏
页码:1911 / 1929
页数:19
相关论文
共 49 条
  • [1] Logarithmic Lyapunov functions for direct adaptive stabilization with normalized adaptive laws
    Akhtar, S
    Venugopal, R
    Bernstein, DS
    [J]. INTERNATIONAL JOURNAL OF CONTROL, 2004, 77 (07) : 630 - 638
  • [2] Stability analysis of nonlinear quadratic systems via polyhedral Lyapunov functions
    Amato, F.
    Calabrese, F.
    Cosentino, C.
    Merola, A.
    [J]. 2008 AMERICAN CONTROL CONFERENCE, VOLS 1-12, 2008, : 2291 - +
  • [3] Suppression of Nonlinear Wing-rock Oscillations by Adaptive Control with the Implicit Reference Model<bold> </bold>
    Andrievsky, Boris
    Kudryashova, Elena V.
    Kuznetsov, Nikolay V.
    Kuznetsova, Olga A.
    Mokaev, Timur N.
    Tomashevich, Stanislav
    [J]. ICNPAA 2018 WORLD CONGRESS: 12TH INTERNATIONAL CONFERENCE ON MATHEMATICAL PROBLEMS IN ENGINEERING, AEROSPACE AND SCIENCES, 2018, 2046
  • [4] [Anonymous], 1979, Stability of Adaptive Controllers
  • [5] [Anonymous], 2012, Dover Books on Electrical Engineering Series
  • [6] A set-theoretic model reference adaptive control architecture for disturbance rejection and uncertainty suppression with strict performance guarantees
    Arabi, Ehsan
    Gruenwald, Benjamin C.
    Yucelen, Tansel
    Nguyen, Nhan T.
    [J]. INTERNATIONAL JOURNAL OF CONTROL, 2018, 91 (05) : 1195 - 1208
  • [7] Astrom K.J., 2013, ADAPTIVE CONTROL
  • [8] Decentralized fault-tolerant MRAC for a class of large-scale systems with time-varying delays and actuator faults
    Deng, Chao
    Yang, Guang-Hong
    Er, Meng Joo
    [J]. JOURNAL OF PROCESS CONTROL, 2019, 75 : 171 - 186
  • [9] ANALYTIC PREDICTION OF THE MAXIMUM AMPLITUDE OF SLENDER WING ROCK
    ERICSSON, LE
    [J]. JOURNAL OF AIRCRAFT, 1989, 26 (01): : 35 - 39
  • [10] VARIOUS SOURCES OF WING ROCK
    ERICSSON, LE
    [J]. JOURNAL OF AIRCRAFT, 1990, 27 (06): : 488 - 494