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A New Force Control Method by Combining Traditional PID Control with Radial Basis Function Neural Network for a Spacecraft Low-Gravity Simulation System

  • Jian Cao*
  • , Yang Zhang*
  • , Chuanyu Ju
  • , Xinyi Xue
  • , Jiyuan Zhang
  • *Corresponding author for this work
  • School of Mechatronics Engineering, Harbin Institute of Technology
  • Aerospace System Engineering Shanghai

Research output: Contribution to journalArticlepeer-review

Abstract

With the continuous development of the space industry, the demand for low-gravity simulation experiments on the ground for spacecraft is increasing, to overcome the gravity compensation of spacecraft on the ground tests. This paper presents a new low-gravity simulation system based on the suspension method. We used a traditional PID control method with Radial Basis Function (RBF) neural network to solve its constant-tension control problem. The ant colony algorithm was used to find the initial parameters of the neural network in the solution space. A self-adjusting control strategy of PID controller parameters was realized. The results show that the tension control error of the low-gravity simulation system is as small as 0.2%, which fully meets the requirements of the system’s technical indicators. This work provides auspicious theoretical and technical support for developing a low-gravity simulation system.

Original languageEnglish
Article number520
JournalAerospace
Volume10
Issue number6
DOIs
StatePublished - Jun 2023
Externally publishedYes

Keywords

  • PID adaptive
  • RBF neural network
  • constant-tension control
  • low-gravity simulation

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