Optimal Capture of Spinning Spacecraft via Deep Learning Vision and Guidance
This paper addresses the problem of robotic capture of an uncooperative spinning target spacecraft. To do so, a computationally lightweight and real-time implementable guidance, navigation, and control architecture that relies on deep learning as well as pseudospectral optimization is proposed and experimentally validated. Specifically, a convolutional neural-network-driven stereovision pose determination system is first combined with a deep-reinforcement-learning-based guidance algorithm and pose tracking controller to cancel the relative motion between a chaser platform and an uncooperative spinning target platform in real time. Then, real-time tracking of a pseudospectral-based optimal guidance law generated offline deploys a robotic arm while minimizing the overall attitude corrections required to keep the target in view. The integrated experiment carried out using Carleton University’s Spacecraft Proximity Operations Testbed (a state-of-the-art planar air bearing facility, introduced in this work) demonstrates the performance of the developed deep learning architecture.
Authors
- Steve Ulrich (ORCID: https://orcid.org/0000-0001-7465-8786)
- Kirk Hovell (ORCID: https://orcid.org/0000-0003-3519-2922)
- Alexander Crain (ORCID: https://orcid.org/0000-0003-4961-8437)
- Courtney Savytska
Institutions
- Carleton University (CA)
Publication Details
- Journal
- Journal of Spacecraft and Rockets
- Published
- 2025-05-26
- DOI
- https://doi.org/10.2514/1.a36277
- Citations
- 3
- Primary Topic
- Space Satellite Systems and Control
- Type
- article
- Field-Weighted Citation Impact
- 14.98
Funders
- Canadian Space Agency
- Natural Sciences and Engineering Research Council of Canada
- Ontario Ministry of Research and Innovation