A first-order analytical theory for optimal low-thrust limited-power transfers between arbitrary elliptical coplanar orbits

DOI10.1155/2008/525930zbMath1354.70053OpenAlexW2125393071WikidataQ58646197 ScholiaQ58646197MaRDI QIDQ955981

Francisco das Chagas Carvalho, Sandro da Silva Fernandes

Publication date: 24 November 2008

Published in: Mathematical Problems in Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1155/2008/525930

Mathematics Subject Classification ID

Applications of optimal control and differential games (49N90) Control of mechanical systems (70Q05) Celestial mechanics (70F15) Orbital mechanics (70M20) Optimality conditions for problems involving ordinary differential equations (49K15)

Related Items (6)

Optimal low-thrust transfers between coplanar orbits with small eccentricities ⋮ A numerical study for optimal low-thrust limited power transfers between coplanar orbits with small eccentricities ⋮ A numerical study of low-thrust limited power trajectories between coplanar circular orbits in an inverse-square force field ⋮ Searching for orbits with minimum fuel consumption for station-keeping maneuvers: an application to lunisolar perturbations ⋮ Station keeping of constellations using multiobjective strategies ⋮ Application of a genetic algorithm in orbital maneuvers

Cites Work

• Notes on Hori method for canonical systems
• Optimum low-thrust rendezvous and station keeping
• An asymptotic solution for optimum power limited orbit transfer.
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