Optimal low-thrust transfers between coplanar orbits with small eccentricities

DOI10.1007/S40314-015-0249-9zbMath1348.70072OpenAlexW842275752MaRDI QIDQ338281

Rodolpho Vilhena de Moraes, Francisco das Chagas Carvalho, Sandro da Silva Fernandes

Publication date: 4 November 2016

Published in: Computational and Applied Mathematics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s40314-015-0249-9

zbMATH Keywords

optimal low-thrust transfersoptimal space trajectoriestransfers between coplanar orbits

Mathematics Subject Classification ID

Numerical methods for initial value problems involving ordinary differential equations (65L05) Orbital mechanics (70M20) Numerical methods of relaxation type (49M20)

Related Items (1)

A numerical study for optimal low-thrust limited power transfers between coplanar orbits with small eccentricities

Cites Work

• A first-order analytical theory for optimal low-thrust limited-power transfers between arbitrary elliptical coplanar orbits
• New challenges to trajectory design by the use of electric propulsion and other new means of wandering in the solar system
• Notes on Hori method for canonical systems
• Averaging and optimal control of elliptic keplerian orbits with low propulsion
• Optimal low-thrust orbital transfers in a central gravity field
• An asymptotic solution for optimum power limited orbit transfer.
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