Astronomy and Astrophysics – Astronomy
Scientific paper
Nov 2004
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2004cemda..90..331s&link_type=abstract
Celestial Mechanics & Dynamical Astronomy, Volume 90, Issue 3-4, pp. 331-354
Astronomy and Astrophysics
Astronomy
1
Lambert Problem, Three-Body Problem, Hill Equations, Lagrange Points, Halo Orbit
Scientific paper
The goal of this paper is obtaining a solution of the Lambert problem in the restricted three-body problem described by the Hill equations. This solution is based on the use of pre determinate reference orbits of different types giving the first guess and defining the sought-for transfer type. A mathematical procedure giving the Lambert problem solution is described. This procedure provides step-by-step transformation of the reference orbit to the sought-for transfer orbit. Numerical examples of the procedure application to the transfers in the Sun Earth system are considered. These examples include transfer between two specified positions in a given time, a periodic orbit design, a halo orbit design, halo-to-halo transfers, LEO-to-halo transfer, analysis of a family of the halo-to-halo transfer orbits. The proposed method of the Lambert problem solution can be used for the two-point boundary value problem solution in any model of motion if a set of typical reference orbits can be found.
Prado Antonio F. Bertachini A.
Sukhanov Alexander
No associations
LandOfFree
Lambert problem solution in the hill model of motion does not yet have a rating. At this time, there are no reviews or comments for this scientific paper.
If you have personal experience with Lambert problem solution in the hill model of motion, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Lambert problem solution in the hill model of motion will most certainly appreciate the feedback.
Profile ID: LFWR-SCP-O-1010814