TY - JOUR
T1 - Observer-based control for the platform of a tethered space robot
AU - ZHAI, Guang
AU - ZHENG, Heming
AU - ZHANG, Bo
N1 - Publisher Copyright:
© 2018 Chinese Society of Aeronautics and Astronautics
PY - 2018/8
Y1 - 2018/8
N2 - This paper addresses the attitude control problem of a space tethered robot platform in the presence of unknown external disturbance caused by a connecting elastic tether. The tether-generated unknown disturbance leads to tremendous challenges for attitude control of the platform. In this work, the perturbed attitude dynamics of the platform are derived with a consideration of the libration of the elastic tether, and then with the purpose of compensating the unknown disturbance, major attention is dedicated to develop a nonlinear disturbance observer based on gyros measurements, after which, an adaptive attitude scheme is proposed by combining the disturbance observer with a sliding mode controller. Finally, benefits from the observer based on an adaptive controller are validated by series of numerical simulations.
AB - This paper addresses the attitude control problem of a space tethered robot platform in the presence of unknown external disturbance caused by a connecting elastic tether. The tether-generated unknown disturbance leads to tremendous challenges for attitude control of the platform. In this work, the perturbed attitude dynamics of the platform are derived with a consideration of the libration of the elastic tether, and then with the purpose of compensating the unknown disturbance, major attention is dedicated to develop a nonlinear disturbance observer based on gyros measurements, after which, an adaptive attitude scheme is proposed by combining the disturbance observer with a sliding mode controller. Finally, benefits from the observer based on an adaptive controller are validated by series of numerical simulations.
KW - Adaptive control
KW - Attitude dynamics
KW - Disturbance observer
KW - Sliding mode control
KW - Tethered space robot
UR - https://www.scopus.com/pages/publications/85045075660
U2 - 10.1016/j.cja.2018.01.012
DO - 10.1016/j.cja.2018.01.012
M3 - Article
AN - SCOPUS:85045075660
SN - 1000-9361
VL - 31
SP - 1786
EP - 1796
JO - Chinese Journal of Aeronautics
JF - Chinese Journal of Aeronautics
IS - 8
ER -