The problem of minimum fuel transfer in a central gravity field for power-limited low thrust propulsion has been studied by several investigators. Orbital averaging was used by Edelbaum in the co-axial and co-planar cases, and by Marec and Vinh for the general transfer between elliptical orbits. The co-latus rectum transfer, which has a complete analytical solution, can be applied to the Pole Squatter. Typical results for the evolution of the orbit parameters and the variation of the thrust acceleration along the orbit are shown.
Low thrust power-limited transfer for a pole squatter
AIAA/AAS Astrodynamics Conference ; 1988 ; Minneapolis, MN, United States
01.01.1988
Aufsatz (Konferenz)
Keine Angabe
Englisch
Low thrust power-limited transfer for a pole squatter
AIAA | 1988
|Improving traffic safety in squatter areas
British Library Conference Proceedings | 1994
|Thrust Limited Coplanar Aeroassisted Orbital Transfer
AIAA | 2001
|Optimal Power-Limited Rendezvous with Thrust Saturation
Online Contents | 1995
|