Modeling, Simulation and Control of a Spacecraft: Automated Rendezvous under Positional Constraints
The aim of this research paper is to propose a framework to model, simulate and control the motion of a small spacecraft in the proximity of a space station. In particular, rendezvous in the presence of physical obstacles is tackled by a virtual potential theory within a modern manifold calculus set...
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| Autori principali: | , , , |
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| Natura: | Artigo |
| Lingua: | Inglês |
| Pubblicazione: |
MDPI AG
2024-03-01
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| Serie: | Aerospace |
| Soggetti: | |
| Accesso online: | https://www.mdpi.com/2226-4310/11/3/245 |
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