@inproceedings{e43cd3a4ef8d4dcb8d6cfa0eabcc3aaf,
title = "Nonlinear attractive sets under optimal feedback control in the hill three-body problem",
abstract = "Trajectory design combining low-thrust and the three-body problem is a challenging area for study. This paper investigates the combination of optimal feedback control with the dynamical structure of the three-body problem. For the nonlinear system, the attractive set of an equilibrium point or a periodic orbit under optimal control is described by the Hamilton-Jacobi-Bellman partial differential equation. We obtain the solution to the Hamilton-Jacobi-Bellman equation by solving the truncation problem successively.",
author = "Mai Bando and Scheeres, {Daniel J.}",
year = "2016",
doi = "10.2514/6.2016-5436",
language = "English",
isbn = "9781624104459",
series = "AIAA/AAS Astrodynamics Specialist Conference, 2016",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "AIAA/AAS Astrodynamics Specialist Conference, 2016",
note = "AIAA/AAS Astrodynamics Specialist Conference, 2016 ; Conference date: 13-09-2016 Through 16-09-2016",
}