Affiliation:
1. School of Mechanical Engineering, Nanjing University of Science & Technology, Nanjing 210094, China
2. Key Laboratory of Special Engine Technology, Ministry of Education, Nanjing University of Science and Technology, Nanjing 210094, China
Abstract
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.
Funder
key laboratory of space intelligent control technology stability
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