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

Author:

Cao Jian1,Zhang Yang2,Ju Chuanyu1,Xue Xinyi1,Zhang Jiyuan1

Affiliation:

1. School of Mechatronics Engineering, Harbin Institute of Technology, Harbin 150001, China

2. Aerospace System Engineering Shanghai, Shanghai 201109, China

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.

Funder

Aerospace System Engineering Shanghai

Publisher

MDPI AG

Subject

Aerospace Engineering

Reference18 articles.

1. Suspended micro-low gravity environment simulation technology: Status quo and prospect;Gao;Acta Astronaut. Et Astronaut. Sin.,2021

2. Zhang, H., Li, C., You, J., Zhang, X., Wang, Y., Chen, L., Fu, Q., Zhang, B., and Wang, Y. (2022). The Investigation of Plume-Regolith Interaction and Dust Dispersal during Chang’E-5 Descent Stage. Aerospace, 9.

3. Micro/Low Gravity Simulation and Experiment Technology for Spacecraft;Qi;J. Astronaut.,2020

4. ESA Parabolic Flights, Drop Tower and Centrifuge Opportunities for University Students;Callens;Microgravity Sci. Technol.,2010

5. The new Drop Tower catapult system;Kaczmarczik;Acta Astronaut.,2006

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