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Novel Gaussian mixture model based nonsingular terminal sliding mode control for spacecraft close-range proximity with complex shape obstacle
- Source :
- Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 236:517-526
- Publication Year :
- 2021
- Publisher :
- SAGE Publications, 2021.
-
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.
- Subjects :
- Physics
020301 aerospace & aeronautics
Spacecraft
business.industry
Mechanical Engineering
Aerospace Engineering
02 engineering and technology
Mixture model
Topology
01 natural sciences
law.invention
Close range
Invertible matrix
0203 mechanical engineering
Terminal (electronics)
law
Obstacle
0103 physical sciences
Nonsingular terminal sliding mode control
Obstacle avoidance
business
010303 astronomy & astrophysics
Subjects
Details
- ISSN :
- 20413025 and 09544100
- Volume :
- 236
- Database :
- OpenAIRE
- Journal :
- Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
- Accession number :
- edsair.doi.dedup.....25075e2b27cae72b726f22957ae7b5c6