Research on Space Operation Control of Air Float Satellite Simulator Based on Constraints Aware Particle Filtering-Nonlinear Model Predictive Control
This paper addresses the challenges of close proximity operations, such as rendezvous, docking, and fly-around maneuvers for micro/nano satellites, which require high control precision under the low power and limited computational capabilities of spacecraft. Firstly, a three-degree-of-freedom air float simulator platform is designed for ground-based experiments. Subsequently, model predictive controllers based on constraints aware of particle filtering (CAPF-NMPC) are developed for executing operations such as approach, fly-around, and docking maneuvers. The results validate the effectiveness of the experimental system, demonstrating position control accuracy less than 0.03 m and attitude control accuracy less than 3°, maintaining lower computational resource consumption. This study offers a practical solution for the onboard deployment of optimized control algorithms, highlighting significant value for further engineering applications.
Authors
- Chuangge Wang
- D.S. Chen (ORCID: https://orcid.org/0009-0003-0369-1986)
- Liao Wen-he (ORCID: https://orcid.org/0000-0002-2409-2398)
- Xu Lingfeng
Institutions
- Nanjing University of Science and Technology (CN)
Publication Details
- Journal
- Electronics
- Published
- 2024-09-08
- DOI
- https://doi.org/10.3390/electronics13173571
- Citations
- 1
- Primary Topic
- Space Satellite Systems and Control
- Type
- article
- Field-Weighted Citation Impact
- 1.30