Loosely formation-displaced geostationary orbit optimization with complex hybrid sail propulsion

DOI10.1155/2018/3576187zbMath1398.90223OpenAlexW2806975213MaRDI QIDQ1785176

Yong Hao, Yuan Liu, Weiwei Liu

Publication date: 28 September 2018

Published in: Complexity (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1155/2018/3576187

zbMATH Keywords

spacecraft formationGauss pseudospectral algorithmgeostationary orbit optimizationhybrid sail propulsion

Mathematics Subject Classification ID

Applications of mathematical programming (90C90) Stochastic programming (90C15) Variable mass, rockets (70P05)

Cites Work

• Orbit period modulation for relative motion using continuous low thrust in the two-body and restricted three-body problems

Related Items (1)

Optimal spatial launch of a spacecraft into a geostationary orbit from and artificial satellite orbit

Uses Software

• PSOPT

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