Low-thrust out-of-plane orbital station-keeping maneuvers for satellites

DOI10.1155/2012/532708zbMath1264.70033OpenAlexW2006250634WikidataQ58912023 ScholiaQ58912023MaRDI QIDQ1954884

Antonio Fernando Bertachini De Almeida Prado, Vivian Martins Gomes

Publication date: 11 June 2013

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

Full work available at URL: https://doi.org/10.1155/2012/532708

Mathematics Subject Classification ID

Numerical mathematical programming methods (65K05) Numerical methods based on necessary conditions (49M05) Celestial mechanics (70F15)

Related Items (4)

Application of the Kalman filter to estimate the state of an aerobraking maneuver ⋮ Searching for orbits with minimum fuel consumption for station-keeping maneuvers: an application to lunisolar perturbations ⋮ Station keeping of constellations using multiobjective strategies ⋮ An analytical description of the three-dimensional swing-by

Cites Work

• Unnamed Item
• Optimum Orbital Transfer by Impulses
• Optimal impulsive transfer with time constraint
• An analytic approach to two-fixed-impulse transfers between Keplerian orbits
• An efficient method for calculating optimal free-space n-impulse trajectories.
• THE FUNDAMENTAL GROUP OF TWO SPACES WITH A COMMON POINT

This page was built for publication: Low-thrust out-of-plane orbital station-keeping maneuvers for satellites