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Fuzzy Sliding Mode for Spacecraft Formation Control in Eccentric Orbits

The problem of relative motion control for spacecraft formation flying in eccentric orbits is considered in this paper. Due to the presence of nonlinear dynamics and external disturbances, a robust fuzzy sliding mode controller is developed. The slopes of sliding surfaces of the conventional sliding...

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Bibliografski detalji
Glavni autori: A. Imani, M. Bahrami
Format: Artigo
Jezik:Persa
Izdano: Aerospace Research Institute 2014-04-01
Serija:فصلنامه علوم و فناوری فضایی
Teme:
Online pristup:https://jsst.ias.ir/article_14497_6b16ff082a514d99af2efbb9900787f1.pdf
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