@inproceedings{969d2736f8d1437a86fb60f1f44d672d,
title = "The adaptive entry guidance based on 3D obtainable space concept",
abstract = "A three-dimension obtainable space concept for entry guidance subjected to path constraints is developed in this paper. The key characteristics of this method is that it can transform the path constraints of heating rate and dynamic pressure into control variable constraints which are bank angle and attack angle, obtaining a three-dimensional control variables space. The transformation can substantially simplify the entry guidance and trajectory design especially online design. The proportional terminal guidance law is introduced in the entry guidance which could fulfill the integrated design of entry guidance and terminal guidance through applying the 3D obtainable space concept.",
author = "Erlong Su and Jianjun Luo and Baichun Gong",
year = "2014",
language = "英语",
series = "Advances in the Astronautical Sciences",
publisher = "Univelt Inc.",
pages = "719--730",
editor = "Mackison, {Donald L.} and Ossama Abdelkhalik and Wilson, {Roby S.} and Renato Zanetti",
booktitle = "Advances In The Astronautical Sciences",
note = "24th AAS/AIAA Space Flight Mechanics Meeting, 2014 ; Conference date: 26-01-2014 Through 30-01-2014",
}