3-DOF Position and Orientation Control of an Air Flotation Platform for Spacecraft Ground Microgravity Simulation by Using Double Closed-Loop Cascade PIDnn

Author:

Wang Siyue12ORCID,Gao Qing3ORCID,Liu Jinguo24ORCID,Feng Jingkai245ORCID,Liufu Jingshu26ORCID

Affiliation:

1. Shenyang Ligong University, Shenyang 110158, China

2. State Key Laboratory of Robotics, Shenyang Institute of Automation, Chinese Academy of Sciences, Shenyang 110016, China

3. Institute of Robotics and Intelligent Manufacturing & School of Science and Engineering, The Chinese University of Hong Kong, Shenzhen 518172, China

4. Institute of Robotics and Intelligent Manufacturing, Chinese Academy of Sciences, Shenyang 110169, China

5. University of Chinese Academy of Sciences, Beijing 100049, China

6. University of Science and Technology Liaoning, Anshan 110325, China

Abstract

Space assistant robots can help astronauts or their assistants perform certain tasks. A ground microgravity simulation environment is built for the space assistant robot AAR-2. The hardware requirements of the ground simulation by the 3-DOF microgravity air flotation platform. An algorithm is designed for this simulation system. By using momentum and RMSprop methods to improve the PID neural network, the challenging problem of strong coupling between system nonlinearity and variables is solved. Firstly, the paper introduces the hardware system and deduces the dynamic model of the system. Then, the algorithm is calculated and simulated. Through simulation, the effectiveness and feasibility of the algorithm are compared and proved. Finally, the control system is simulated by MATLAB/Simulink and compared with other advanced algorithms. The simulation results show that the designed neural network controller can quickly and accurately control the 3-DOF of freedom motion of AAR-2.

Funder

CAS Interdisciplinary Innovation Team

Publisher

Hindawi Limited

Subject

Aerospace Engineering

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