@inproceedings{36a57e51eb444abcabdae60c72ba5898,
title = "Delayed output feedback control of the spacecraft rendezvous system with actuator delays",
abstract = "This study is concerned with the circular orbital spacecraft rendezvous by the delayed output feedback (DOF). Considering that the rendezvous system is subjected to actuator delay and the relative velocity is difficult to be measured actually in practice, the DOF controller is constructed by just using the present and past inputs and outputs to predict the future state, which is then used to form the predictor-based state feedback. Since the numerical approximation of the distributed delay terms contained in the DOF controller may lead to instability of the whole system, a filter is introduced in the control loop and an augmented system is used to design the filter gains. Numerical simulations are worked out to show the effectiveness of the proposed approach.",
keywords = "Actuator delay, Delayed output feedback, Filters, Numerical integration, Spacecraft rendezvous",
author = "Chuanchuan Xu and Weiwei Luo and Bin Zhou",
note = "Publisher Copyright: {\textcopyright} 2017 Technical Committee on Control Theory, CAA.; 36th Chinese Control Conference, CCC 2017 ; Conference date: 26-07-2017 Through 28-07-2017",
year = "2017",
month = sep,
day = "7",
doi = "10.23919/ChiCC.2017.8028317",
language = "英语",
series = "Chinese Control Conference, CCC",
publisher = "IEEE Computer Society",
pages = "6037--6042",
editor = "Tao Liu and Qianchuan Zhao",
booktitle = "Proceedings of the 36th Chinese Control Conference, CCC 2017",
address = "美国",
}