SAR optimization and Convolutional Neural Network based fault estimations and for auto-landing control model

被引:1
作者
Ayyasamy, T. [1 ]
Nirmala, S. [2 ]
Saravanakumar, A. [3 ]
机构
[1] Anna Univ, Dhanalakshmi Srinivasan Engn Coll Autonomous, Dept Aeronaut Engn, Chennai, India
[2] Anna Univ, Dept Elect & Commun Engn, Chennai, India
[3] Anna Univ, Madras Inst Technol, Dept Aeronaut Engn, Chennai, India
关键词
CNN; LSTM; SAR; Fault estimation; Auto-landing; Pitch; Altitude; Roll; Yaw angle; ALGORITHM;
D O I
10.1016/j.robot.2023.104409
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
During auto landing, the aircraft flies at a significantly low altitude and low speed. So the consequent accidents and flight crashes are highly possible. Several constrained space and foremost external interruption while landing is considered as one of the most complex phases of the aircraft. Therefore it is necessary to recover the aircraft from various major disturbances and to estimate the rate of fault during aircraft landing. In addition to this, for the effective design of an aircraft, it is essential in determining the fault that affects the aircraft. To overcome the issues, this article aim to propose a novel CNNLSTM-SAR-based fault estimation approach to estimate the fault rate from various state trajectories of the aircraft. Here we employed a Convolution Neural Network (CNN) and Long Short-Term Memory (LSTM) model integrated with the Search and Rescue (SAR) optimization algorithm to react instantaneously to the broad range of failures such as actuator failure and failure due to the wind. Then the performances of the proposed CNNLSTM-SAR based fault estimation approach are compared and the results demonstrated that the proposed approach provide a smooth landing with minimum fault and error. (c) 2023 Published by Elsevier B.V.
引用
收藏
页数:12
相关论文
共 39 条
  • [1] Aleksandrovskaya L.N., 2019, RUSS AERONAUT, V62, P199
  • [2] An improved NSGA-II based control allocation optimisation for aircraft longitudinal automatic landing system
    Bian, Qi
    Nener, Brett
    Wang, Xinmin
    [J]. INTERNATIONAL JOURNAL OF CONTROL, 2019, 92 (04) : 705 - 716
  • [3] Air-to-Air Automatic Landing of Unmanned Aerial Vehicles: A Quasi Time-Optimal Hybrid Strategy
    Gozzini, Giovanni
    Invernizzi, Davide
    Panza, Simone
    Giurato, Mattia
    Lovera, Marco
    [J]. IEEE CONTROL SYSTEMS LETTERS, 2020, 4 (03): : 692 - 697
  • [4] Fixed-time control for automatic carrier landing with disturbance
    Guan, Zhiyuan
    Liu, Hu
    Zheng, Zewei
    Lungu, Mihai
    Ma, Yunpeng
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 108
  • [5] Mars entry fault-tolerant control via neural network and structure adaptive model inversion
    Huang, Yixin
    Li, Shuang
    Sun, Jun
    [J]. ADVANCES IN SPACE RESEARCH, 2019, 63 (01) : 557 - 571
  • [6] 3D Convolutional Neural Networks for Human Action Recognition
    Ji, Shuiwang
    Xu, Wei
    Yang, Ming
    Yu, Kai
    [J]. IEEE TRANSACTIONS ON PATTERN ANALYSIS AND MACHINE INTELLIGENCE, 2013, 35 (01) : 221 - 231
  • [7] Khanapuri Eshaan M., 2018, P INT C COGNITION RE, P63
  • [8] Krammer C, 2020, AIAA SCITECH 2020 FO, P1083
  • [9] Kugler Martin E., 2019, AIAA SCITECH 2019 FO, P0505
  • [10] Lin SY, 2019, TENCON IEEE REGION, P235, DOI [10.1109/TENCON.2019.8929401, 10.1109/tencon.2019.8929401]