@inproceedings{773a4ef5e5fb438ca3ab9f4bf49bf213,
title = "Time-fuel optimal trajectory based attitude maneuver control for flexible spacecraft",
abstract = "This paper investigates the attitude maneuver control for flexible spacecraft, in which the torque saturation and unknown parameter uncertainties are considered. Firstly, a timefuel optimal trajectory is developed such that a PD controller based on the trajectory is proposed. Then, in order to suppress the vibration of flexible appendages, a structure filter is designed for the first order elastic mode. Simulation results show that the high-precise attitude control and vibration suppression are achieved successfully. Considering the inertia parameter errors, the effectiveness of the developed optimal trajectory is demonstrated.",
keywords = "Attitude maneuver, Flexible spacecraft, Structure filter, Weightedtime-fuel optimal control",
author = "Pengyu Wang and Zongming Liu and Chuanjiang Li and Yanchao Sun and Chao Zhang",
note = "Publisher Copyright: {\textcopyright} 2016 IEEE.; 6th International Conference on Instrumentation and Measurement, Computer, Communication and Control, IMCCC 2016 ; Conference date: 21-07-2016 Through 23-07-2016",
year = "2016",
month = dec,
day = "5",
doi = "10.1109/IMCCC.2016.227",
language = "英语",
series = "Proceedings - 2016 6th International Conference on Instrumentation and Measurement, Computer, Communication and Control, IMCCC 2016",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "197--201",
editor = "Junbao Li",
booktitle = "Proceedings - 2016 6th International Conference on Instrumentation and Measurement, Computer, Communication and Control, IMCCC 2016",
address = "美国",
}