A New Force Control Method by Combining Traditional PID Control with Radial Basis Function Neural Network for a Spacecraft Low-Gravity Simulation System
Author:
Affiliation:
1. School of Mechatronics Engineering, Harbin Institute of Technology, Harbin 150001, China
2. Aerospace System Engineering Shanghai, Shanghai 201109, China
Abstract
Funder
Aerospace System Engineering Shanghai
Publisher
MDPI AG
Subject
Aerospace Engineering
Link
https://www.mdpi.com/2226-4310/10/6/520/pdf
Reference18 articles.
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3. Micro/Low Gravity Simulation and Experiment Technology for Spacecraft;Qi;J. Astronaut.,2020
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