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Multiple Spacecraft Formation Flying Control around Artificial Equilibrium Point Using Propellantless Approach
This paper demonstrates a detailed analysis of the feasibility for compact formation system around an L2-type artificial equilibrium point by means of continuous low-thrust propulsion in the hybrid form of solar sail and Coulomb force propulsion. Firstly, in view of non-ideal solar sail, the positio...
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| Main Authors: | , , , |
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| Formato: | Artigo |
| Idioma: | Inglês |
| Publicado em: |
Hindawi Limited
2022-01-01
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| Colecção: | International Journal of Aerospace Engineering |
| Acesso em linha: | http://dx.doi.org/10.1155/2022/8719645 |
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