Journal of Aeronautical Engineering

Journal of Aeronautical Engineering

Neural network-based control with disturbance estimation using Kalman filter for missile longitudinal channel autopilot

Document Type : Original Article

Authors
1 Faculty of Electrical and Computer, Malek-Ashtar University of Technology, Iran.
2 Faculty of Electrical & Computer Engineering , Malek ashtar University of Technology, Iran
10.22034/joae.2025.456173.1227
Abstract
In this paper, the design and simulation of the longitudinal channel missile autopilot based on the neural network and disturbance estimation using Kalman filter is presented. It is assumed that the dynamics of this disturbance is equal to zero and its value is constant over time. After the disturbance compensation, a neural network based controller is used for the longitudinal channel autopilot of the missile. One of the advantages of the proposed method is the use of the Kalman filter to estimate the disturbance, which is an optimal estimator. Also, the neural network is used as an autopilot and there is no need to design a controller.
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Subjects


Volume 27, Issue 1
May 2025
Pages 75-85

  • Receive Date 12 May 2024
  • Revise Date 10 September 2024
  • Accept Date 29 December 2024