@inproceedings{1f8134da550944bbaa1d7f279e5fc77c,
title = "Robust deflection strategies of Near Earth asteroids under uncertainties",
abstract = "In this paper, an approach to optimize deflection mission of Near Earth asteroids under uncertainty is proposed based on control theoretical framework. By using the nonlinear mapping from initial deviation to the final deviation, the performance index J which is expressed as a function of the distance of the Earth in the Earth's closest approach time is minimized for the worst case initial condition. We also formulate the robust orbital transfer problem of kinetic impactor spacecraft where the initial state estimation error exists.",
author = "Mai Bando and Yuki Akiyama and Shinji Hokamoto",
year = "2014",
month = jan,
day = "1",
language = "English",
series = "Advances in the Astronautical Sciences",
publisher = "Univelt Inc.",
pages = "1165--1181",
editor = "Mackison, {Donald L.} and Ossama Abdelkhalik and Wilson, {Roby S.} and Renato Zanetti",
booktitle = "Advances In The Astronautical Sciences",
address = "United States",
note = "24th AAS/AIAA Space Flight Mechanics Meeting, 2014 ; Conference date: 26-01-2014 Through 30-01-2014",
}