Station keeping of constellations using multiobjective strategies

DOI10.1155/2013/476451zbMath1299.90300OpenAlexW1974473136WikidataQ59027915 ScholiaQ59027915MaRDI QIDQ473700

Evandro Marconi Rocco, Marcelo Lopes de Oliveira e Souza, Antonio Fernando Bertachini De Almeida Prado

Publication date: 24 November 2014

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

Full work available at URL: https://doi.org/10.1155/2013/476451

Mathematics Subject Classification ID

Multi-objective and goal programming (90C29) Celestial mechanics (70F15)

Related Items (1)

Design of a linear time-invariant control system based on a multiobjective optimization approach

Cites Work

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• A first-order analytical theory for optimal low-thrust limited-power transfers between arbitrary elliptical coplanar orbits
• Multiobjective programming and planning
• Optimal multi-objective low-thrust spacecraft trajectories
• Low-thrust out-of-plane orbital station-keeping maneuvers for satellites
• Optimal two-impulse trajectories with moderate flight time for Earth-Moon missions
• Optimal multiple-impulse time-fixed rendezvous between circular orbits
• Optimal switching conditions for minimum fuel fixed time transfer between non coplanar elliptical orbits
• Optimal impulsive transfer with time constraint
• Optimal Multiple-Impulse Direct Ascent Fixed-Time Rendezvous
• Optimal Low Thrust Trajectories to the Moon
• Transfer orbits in the Earth-moon system using a regularized model
• Optimal four-impulse fixed-time rendezvous in the vicinity of a circular orbit.
• An efficient method for calculating optimal free-space n-impulse trajectories.
• Optimal two- and three-impulse fixed-time rendezvous in the vicinityof a circular orbit

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