@inproceedings{f1525a87981c4c899fb13a8c61a83afa,
title = "Attitude control of under-actuated spacecraft with two reaction wheels by rotating the solar panels",
abstract = "This paper describes a novel attitude control strategy for an under-actuated spacecraft with two RWs (Reaction Wheels), using the active assistance of SRP (solar radiation pressure) torque. In this case, the magnitude and direction of the solar radiation pressure torque can be adjusted by changing the solar panel rotation angles. The model is linearized and the linear quadratic regulator (LQR) controller is designed to obtain the command control torque. The numerical solution is used to calculate the windsurfing angle to provide the expected torque along under-actuated axis. The simulation results prove the effectiveness of this control method.",
author = "Yingjie Li and Lei Jin",
note = "Publisher Copyright: {\textcopyright} 2018 KASHYAP.; 4th IAA Conference on Dynamics and Control of Space Systems, DYCOSS 2018 ; Conference date: 21-05-2018 Through 23-05-2018",
year = "2018",
language = "英语",
isbn = "9780877036531",
series = "Advances in the Astronautical Sciences",
publisher = "Univelt Inc.",
pages = "2247--2258",
editor = "Jeng-Shing Chern and Ya-Zhong Luo and Xiao-Qian Chen and Lei Chen",
booktitle = "Dynamics and Control of Space Systems",
}