TY - JOUR
T1 - Advance of dynamics and control of the satellite with large mesh deployable antenna
AU - Liu, Likun
AU - Zhou, Zhicheng
AU - Zheng, Gangtie
AU - Tian, Qiang
PY - 2014/4
Y1 - 2014/4
N2 - With the development of mobile communication technology, the large deployable parabolic mesh reflectors are wildly used to improve the antenna gain. Considering the large inertia, long-period deployment, and low stiffness properties, these antennae have a great influence on the dynamics and control of the satellites. Firstly, the structural characteristics and its influences on the dynamic and control of the whole-satellite were introduced for the large mesh deployable antenna. Secondly, the dynamic and control problems were discussed, such as dynamic modeling of the deployed antenna, verification method of the deployed dynamic model, multi-body dynamics of the deploying antenna, deploying-process attitude control, and pointing control of the antenna, and so on. Finally, the prospects of the dynamics and control of the satellite with large deployable antenna were presented.
AB - With the development of mobile communication technology, the large deployable parabolic mesh reflectors are wildly used to improve the antenna gain. Considering the large inertia, long-period deployment, and low stiffness properties, these antennae have a great influence on the dynamics and control of the satellites. Firstly, the structural characteristics and its influences on the dynamic and control of the whole-satellite were introduced for the large mesh deployable antenna. Secondly, the dynamic and control problems were discussed, such as dynamic modeling of the deployed antenna, verification method of the deployed dynamic model, multi-body dynamics of the deploying antenna, deploying-process attitude control, and pointing control of the antenna, and so on. Finally, the prospects of the dynamics and control of the satellite with large deployable antenna were presented.
KW - Attitude control
KW - Dynamics
KW - Large deployable mesh antenna
KW - Satellite
UR - https://www.scopus.com/pages/publications/84900496199
U2 - 10.3780/j.issn.1000-758X.2014.02.001
DO - 10.3780/j.issn.1000-758X.2014.02.001
M3 - Review article
AN - SCOPUS:84900496199
SN - 1000-758X
VL - 34
SP - 1
EP - 12
JO - Chinese Space Science and Technology
JF - Chinese Space Science and Technology
IS - 2
ER -