@inproceedings{9b3560f0b64d442fa83cbcb34e09bac4,
title = "Design of modified backstepping attitude controller",
abstract = "In this paper, a three-axis nonlinear two step attitude controller design composed of control law module and control allocation module is presented for the attitude control of hypersonic vehicle in the re-entry phase. The modified backstepping control law integrated backstepping technique and extended state observers (ESOs). In order to facilitate the backstepping design, a command filter was introduced. To deal with the large and fast-varying uncertainties, linear extended state observers were designed to estimate and compensate for the uncertainties in real time. Simulations performed using six-degree-of-freedom nonlinear dynamics in MATLAB show that design using the proposed modified backstepping attitude controller has better tracking performance and is more robust to uncertainties with fewer control demands than traditional backstepping design.",
keywords = "Control systems, Design, Parameters, Vehicles",
author = "Jingjing Li and Zhang Ren",
year = "2010",
doi = "10.1061/41096(366)165",
language = "英语",
isbn = "9780784410967",
series = "Proceedings of the 12th International Conference on Engineering, Science, Construction, and Operations in Challenging Environments - Earth and Space 2010",
pages = "1834--1841",
booktitle = "Earth and Space 2010",
note = "12th International Conference on Engineering, Science, Construction, and Operations in Challenging Environments - Earth and Space 2010 ; Conference date: 14-03-2010 Through 17-03-2010",
}