Optimal aeroassisted return from high earth orbit with plane change

DOI10.1016/0094-5765(85)90003-7zbMath0599.70038OpenAlexW3084962616MaRDI QIDQ3735126

N. X. Vinh, John M. Hanson

Publication date: 1985

Published in: Acta Astronautica (Search for Journal in Brave)

Full work available at URL: http://hdl.handle.net/2027.42/25789

zbMATH Keywords

variational problemparametric optimization problemorbital transfer vehiclechange in orbital planecombined propulsive and atmospheric maneuverhigh earth orbitNecessary conditions for the optimal split of plane changeoptimal impulsive transferperformance index for optimizationsynergetic type of flighttotal characteristic velocity

Mathematics Subject Classification ID

Control of mechanical systems (70Q05) Orbital mechanics (70M20)

Related Items (2)

Planar heliocentric roto-translatory motion of a spacecraft with a solar sail of complex shape ⋮ Application of the Kalman filter to estimate the state of an aerobraking maneuver

This page was built for publication: Optimal aeroassisted return from high earth orbit with plane change