@inproceedings{531fd29a0c5c40b4b742adf9fc1464da,
title = "A variable structure attitude control system design based on finite time stability",
abstract = "A variable structure attitude control system design method that guarantees the finite-time stability is proposed for hypersonic vehicle attitude control. According to the characteristics of the hypersonic vehicle longitudinal attitude model, it is considered to comprise attack angle control loop and angular rate control loop. The attack angle controller and pitch angular rate controller based on variable structure control are designed respectively which ensure the finite-time stability. The finite-time stability of the whole attitude control system has been proved.The simulation results illustrated that the proposed attitude controller has good rapidity and robustness.",
keywords = "Attitude control, Finite time stability, Hypersonic vehicle, Variable structure control",
author = "Jiang, \{Rui Min\} and Jun Zhou and Guo, \{Jian Guo\}",
year = "2014",
doi = "10.4028/www.scientific.net/AMM.446-447.1141",
language = "英语",
isbn = "9783037859087",
series = "Applied Mechanics and Materials",
pages = "1141--1145",
booktitle = "Advanced Research in Material Science and Mechanical Engineering",
note = "2013 2nd International Conference on Mechanics and Control Engineering, ICMCE 2013 ; Conference date: 01-09-2013 Through 02-09-2013",
}