@inproceedings{58fd9b7c1908405cb087f78df18cd2c1,
title = "2-Sliding mode implementation in aircraft pitch control",
abstract = "The main problem in controlling real aircraft is information lack, external disturbances and mathematical model inaccuracy. However, combining both high precision and robustness, standard sliding modes feature high-frequency control switching causing the so-called chattering effect. The controller considered in the present paper is based on 2-sliding modes and produces bounded control continuously depending on time. It removes the chattering effect, reveals significant adaptive properties and guarantees precise constraint fulfillment within a finite time. The general approach is demonstrated by a solution of a real-life pitch control problem. Results of computer simulation and of actual flight experiments are presented.",
keywords = "Aircraft Control, Sliding Mode, Tracking",
author = "A. Levant and A. Pridor and Ben-Asher, {J. Z.} and R. Gitizadeh and I. Yaesh",
note = "Publisher Copyright: {\textcopyright} 1999 EUCA.; null ; Conference date: 31-08-1999 Through 03-09-1999",
year = "2015",
month = mar,
day = "24",
doi = "10.23919/ecc.1999.7099928",
language = "אנגלית",
series = "European Control Conference, ECC 1999 - Conference Proceedings",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "3826--3831",
booktitle = "European Control Conference, ECC 1999 - Conference Proceedings",
address = "ארצות הברית",
}