Adaptive controller for a strength testbed for aircraft structures

被引：3
|
作者：
Laperdin A.I. [1 ]
Yurkevich V.D. [2 ]
机构：
[1] Chaplygin Siberian Scientific Research Institute of Aviation, ul. Polzunova 21, Novosibirsk
[2] Novosibirsk State Technical University, pr. Karla Marksa 20, Novosibirsk
来源：
Optoelectronics, Instrumentation and Data Processing | 2017年 / 53卷 / 4期
基金：
俄罗斯基础研究基金会;
关键词：
adaptive controller; aircraft structures; control system; PI controller; strength tests; structural loading; time-scale separation method;
D O I：
10.3103/S8756699017040069
中图分类号：
学科分类号：
摘要：
The problem of control system design for a strength testbed of aircraft structures is considered. A method for calculating the parameters of a proportional-integral controller (control algorithm) using the time-scale separation method for the testbed taking into account the dead time effect in the control loop is presented. An adaptive control algorithm structure is proposed which limits the amplitude of high-frequency oscillations in the control system with a change in the direction of motion of the rod of the hydraulic cylinders and provides the desired accuracy and quality of transients at all stages of structural loading history. The results of tests of the developed control system with the adaptive control algorithm on an experimental strength testbed for aircraft structures are given. © 2017, Allerton Press, Inc.
引用
收藏
页码：351 / 357
页数：6
相关论文
共 50 条
  • [21] Adaptive Fuzzy Sliding Mode Controller Design for Saucer-shaped Aircraft
    Liu, Yong
    Zhou, Qiang
    Lan, Tian
    Lei, Junwei
    2017 2ND INTERNATIONAL CONFERENCE ON CONTROL AND ROBOTICS ENGINEERING (ICCRE2017), 2017,
  • [22] Direct adaptive neural flight controller for F-8 fighter aircraft
    Suresh, S
    Omkar, SN
    Mani, V
    Sundararajan, N
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2006, 29 (02) : 454 - 464
  • [23] H∞ Robust Adaptive Controller for a Morphing Aircraft Based on SRAD and LPV model
    Jie, Zhang
    PROCEEDINGS OF THE 30TH CHINESE CONTROL AND DECISION CONFERENCE (2018 CCDC), 2018, : 5250 - 5255
  • [24] Model-free adaptive attitude controller for a tilt-rotor aircraft
    Xia, Q.-Y. (xqy@nuaa.edu.cn), 1600, Chinese Institute of Electronics (35):
  • [25] Adaptive Controller Design for Generic Quadrotor Aircraft Platform Subject to Slung Load
    Feng, Ying
    Rabbath, Camille Alain
    Rakheja, Subhash
    Su, Chun-Yi
    2015 IEEE 28TH CANADIAN CONFERENCE ON ELECTRICAL AND COMPUTER ENGINEERING (CCECE), 2015, : 1135 - 1139
  • [26] Unfalsified Adaptive Controller Design for Pilot-Aircraft System(ICCAS 2015)
    Wei Liming
    Shan, Fu
    Dan, Huang
    2015 15TH INTERNATIONAL CONFERENCE ON CONTROL, AUTOMATION AND SYSTEMS (ICCAS), 2015, : 1494 - 1499
  • [27] Integrated 4D trajectory and attitude adaptive controller for civil aircraft
    Fan Y.
    Shao X.
    Li Q.
    Ren Z.
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2019, 40 (02):
  • [28] Adaptive attitude control for Supersonic Aircraft based on Backstepping and Neural Networks Controller
    Zhou, Lilin
    Liu, Lei
    Cheng, Zhongtao
    Wang, Yongji
    Yang, Ye
    PROCEEDINGS OF THE 2019 31ST CHINESE CONTROL AND DECISION CONFERENCE (CCDC 2019), 2019, : 2154 - 2159
  • [29] Adaptive fuzzy fault-tolerant controller for aircraft autolanding under failures
    Rong, Hai-Jun
    Sundararajan, N.
    Saratchandran, P.
    Huang, Guang-Bin
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2007, 43 (04) : 1586 - 1603
  • [30] Lockheed Martin modifying aircraft for JSF testbed
    Aviat Week Space Technol (New York), 1 (19):
12345