Attitude Adaptive Control Of Combined Spacecraft
- DOI
- 10.2991/jimec-17.2017.18How to use a DOI?
- Keywords
- combination of spacecraft; attitude; adaptive control.
- Abstract
Aiming at the attitude adaptive control of spacecraft after docking, an adaptive attitude control method is proposed.Firstly, the dynamic modeling and spatial disturbance torque modeling of the combined spacecraft are carried out using the modified Rodriguez parameters to describe the attitude of the combined spacecraft. Secondly, according to the equation of attitude motion, the characteristic equation of closed-loop control system is deduced, and an adaptive attitude controller is designed. Finally, Matlab/Simulink simulation tool simulates the analysis. The simulation results show the effectiveness of the proposed controller for attitude control of the combined spacecraft.
- Copyright
- © 2017, the Authors. Published by Atlantis Press.
- Open Access
- This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).
Cite this article
TY - CONF AU - Qian Wang AU - Xinhong Li AU - Guanghong He AU - Zhibin Zhang AU - Jiping An PY - 2017/10 DA - 2017/10 TI - Attitude Adaptive Control Of Combined Spacecraft BT - Proceedings of the 2017 2nd Joint International Information Technology, Mechanical and Electronic Engineering Conference (JIMEC 2017) PB - Atlantis Press SP - 85 EP - 89 SN - 2352-538X UR - https://doi.org/10.2991/jimec-17.2017.18 DO - 10.2991/jimec-17.2017.18 ID - Wang2017/10 ER -