@inproceedings{f103181a26f54463be5f943907a2cf40,
title = "Spacecraft robust attitude control attitude control with saturation nonlinearity",
abstract = "The paper presents a robust nonlinear H∞ control design method for rigid spacecraft asymptotic attitude control with input saturation nonlinearity. The solution of the nonlinear H∞ control problem is known to related to the existence of solution to a Hamilton-Jacobi partially differential inequality (HJPDI). The papers proposes a candidate solution to the HJPDI for spacecraft attitude control that is subject to nonlinear dynamics and input saturation. The method is applied to the ROCSAT-3 attitude control problem to verify its effectiveness.",
author = "Show, {Long Life} and Juang, {Jyh Ching} and Jan, {Ying Wen} and Lin, {Chen Tsung}",
year = "2002",
month = jan,
day = "1",
language = "English",
isbn = "9781624101083",
series = "AIAA Guidance, Navigation, and Control Conference and Exhibit",
publisher = "American Institute of Aeronautics and Astronautics Inc.",
booktitle = "AIAA Guidance, Navigation, and Control Conference and Exhibit",
note = "AIAA Guidance, Navigation, and Control Conference and Exhibit 2002 ; Conference date: 05-08-2002 Through 08-08-2002",
}