@inproceedings{bea9252039f84ad18deed65909c57046,
title = "Full-state autopilot-guidance design under a linear quadratic differential game formulation",
abstract = "Full-state single-loop and full-state two-loop autopilot-guidance designs are derived using a linear quadratic differential game formulation. To keep all the states at reasonable values throughout the end-game, a cost function that includes appropriate running cost terms on some of the states is proposed. It is proven that the two designs may be identical under a linear quadratic differential game formulation and the proposed cost function. The theorem and guidance laws are illustrated using an interceptor missile having forward and aft controls.",
author = "Maital Levy and Tal Shima and Shaul Gutman",
note = "Publisher Copyright: {\textcopyright} IFAC.; 19th IFAC World Congress on International Federation of Automatic Control, IFAC 2014 ; Conference date: 24-08-2014 Through 29-08-2014",
year = "2014",
doi = "https://doi.org/10.3182/20140824-6-za-1003.01240",
language = "الإنجليزيّة",
series = "IFAC Proceedings Volumes (IFAC-PapersOnline)",
pages = "3942--3947",
editor = "Edward Boje and Xiaohua Xia",
booktitle = "19th IFAC World Congress IFAC 2014, Proceedings",
}