Intelligent dynamic surface control strategy for high-performance aircraft subject to uncertain aerodynamics

被引:0
|
作者
Sharma, Manish [1 ]
Dubey, Somya [2 ]
Puntambekar, Sachin [3 ]
Gupta, Vinit [3 ]
机构
[1] DY Patil Coll Engn, Pune 411044, India
[2] Dr APJ Abdul Kalam Univ, Indore 452016, India
[3] Medi Caps Univ, Indore 453331, India
关键词
high-performance aircraft systems; adaptive observers; wavelet networks; input constraints; Lyapunov functional;
D O I
10.1504/IJIEI.2023.133071
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
The uncertain dynamics and actuator saturation in attitude tracking of high-performance aircrafts have posed a serious challenge in deriving an accurate control strategy. This paper presents an adaptive observer-controller strategy to deal with these problems. It uses wavelet neural networks (WNN) to estimate the functional uncertainties in the nonlinear dynamics of the aircraft with 6 degree of freedom (6 DoF). WNN uses wavelets as activation function to achieve superior learning characteristics. This system is very close to the real time model as it is subjected to the modelling uncertainties and actuator saturation owing to the external random parameters which makes the control design very complicated. The novelty of this paper lies within the estimation of these highly random nonlinear uncertainties by the modified deep learning network, WNN and the respective controller-observer strategy. Simulation analysis has been performed to evaluate the performance of the theoretical development presented in the paper.
引用
收藏
页码:214 / 228
页数:16
相关论文
共 50 条
  • [21] FIXED-ORDER DYNAMIC COMPENSATION FOR A HIGH-PERFORMANCE FIGHTER AIRCRAFT
    BYRNS, EV
    CALISE, AJ
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1993, 16 (01) : 104 - 110
  • [22] Simple and high-performance cell balancing control strategy
    Chen, Zilong
    Liao, Wenjun
    Li, Pingfei
    Tan, Jinhui
    Chen, Yuping
    ENERGY SCIENCE & ENGINEERING, 2022, 10 (09) : 3592 - 3601
  • [23] A strategy for in-flight measurements of physiology of pilots of high-performance fighter aircraft
    West, John B.
    JOURNAL OF APPLIED PHYSIOLOGY, 2013, 115 (01) : 145 - 149
  • [24] Intelligent adaptive nonlinear flight control for a high performance aircraft with neural networks
    Savran, A
    Tasaltin, R
    Becerikli, Y
    ISA TRANSACTIONS, 2006, 45 (02) : 225 - 247
  • [25] APPLICATION OF TOTAL ENERGY CONTROL FOR HIGH-PERFORMANCE AIRCRAFT VERTICAL TRANSITIONS
    WARREN, A
    AIAA GUIDANCE, NAVIGATION AND CONTROL CONFERENCE, PTS 1 AND 2: A COLLECTION OF TECHNICAL PAPERS, 1989, : 1118 - 1126
  • [26] DIGITAL CONTROL OF HIGH-PERFORMANCE AIRCRAFT USING ADAPTIVE ESTIMATION TECHNIQUES
    VANLANDINGHAM, HF
    MOOSE, RL
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 1977, 13 (02) : 112 - 119
  • [27] Intelligent High-performance Dynamic Control for Two-stage Screw High-temperature Heat Pump System
    Luo, Win-Jet
    Lai, Jin-Chang
    Hsieh, Po-Yuan
    Fasya, Fikri Rahmat
    SENSORS AND MATERIALS, 2018, 30 (11) : 2599 - 2614
  • [28] APPLICATION OF TOTAL ENERGY CONTROL FOR HIGH-PERFORMANCE AIRCRAFT VERTICAL TRANSITIONS
    WARREN, A
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1991, 14 (02) : 447 - 452
  • [29] High-performance government in an uncertain world
    Lempert, RJ
    Popper, SW
    High-Performance Government: Structure, Leadership, Incentives, 2005, : 113 - 135
  • [30] ROTORS FOR HIGH-PERFORMANCE VTOL AIRCRAFT
    LICHTEN, RL
    JOURNAL OF THE ROYAL AERONAUTICAL SOCIETY, 1965, 69 (650): : R16 - &