Novel Gaussian mixture model based nonsingular terminal sliding mode control for spacecraft close-range proximity with complex shape obstacle

Author:

Wang Yi12ORCID,Yao Wen1ORCID,Chen Xiaoqian1,Ceriotti Matteo3,Bai Yuzhu4,Zhu Xiaozhou1ORCID

Affiliation:

1. National Innovation Institute of Defense Technology, Chinese Academy of Military Sciences, Beijing, China

2. Nanjing Research Institute of Electronics Technology, Nanjing, China

3. School of Engineering, University of Glasgow, Glasgow, UK

4. College of Aerospace and Engineering, National University of Defense Technology, Changsha, China

Abstract

This study is mainly focusing on the problem of spacecraft close-range proximity with obstacle avoidance in the presence of complex shape. A novel Gaussian mixture model–based nonsingular terminal sliding mode control (GMM-NTSMC) is proposed. This is achieved by developing GMM-based potential function with a switching surface of NTSMC. It is theoretically proved that the closed-loop system is globally stable. The main contribution of this study is that the GMM-based avoiding strategies, which include the GMM-based terminal sliding mode control (GMM-TSMC) and GMM-NTSMC, can solve the collision avoidance problem considering complex shape while the artificial potential function–based terminal sliding model control (APF-TSMC) fails. Moreover, the GMM-NTSMC and the GMM-TSMC require less energy with respect to the APF-TSMC. Furthermore, the GMM-NTSMC retains the advantage of the NTSMC and can avoid singularity problem while GMM-TSMC cannot. Finally, numerical simulations are performed to verify the effectiveness and superiority of the proposed GMM-NTSMC.

Funder

The China Postdoctoral Science Foundation

The National Science Foundation of China

The Major Program of National Nature Science Foundation of China

Publisher

SAGE Publications

Subject

Mechanical Engineering,Aerospace Engineering

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