@inproceedings{31795c76504d4631aff631e090828cc5,
title = "3-point inscribed angle guidance law",
abstract = "A planar three-point trajectory shaping guidance law against stationary targets was developed based upon the principle of constant inscribed angles in a circle. The guidance controller was designed through linearization. Linear and non-linear dynamic models were compared through simulation, and results are shown for various scenarios of applied desired impact angles. Utilization of this guidance law requires simply the inscribed angle in order to effectively shape the missile trajectory, allowing to impose impact angles. Application of the proposed strategy can enhance penetration capabilities, reduce a missile's warhead size, and reduce collateral damage.",
author = "Ronny Tsalik and Tal Shima",
year = "2013",
language = "الإنجليزيّة",
isbn = "9781627481144",
series = "53rd Israel Annual Conference on Aerospace Sciences 2013",
pages = "256--277",
booktitle = "53rd Israel Annual Conference on Aerospace Sciences 2013",
note = "53rd Israel Annual Conference on Aerospace Sciences 2013 ; Conference date: 06-03-2013 Through 07-03-2013",
}