TY - GEN
T1 - Cooperative circumnavigation of a host spacecraft by multiple microsatellites
AU - Li, Dongyu
AU - Li, Chuanjiang
AU - Ma, Guangfu
AU - Lv, Yueyong
AU - He, Wei
AU - Ge, Shuzhi Sam
N1 - Publisher Copyright:
© 2019 EUCA.
PY - 2019/6
Y1 - 2019/6
N2 - This paper addresses the trajectory analysis, mission design, and control law for multiple microsatellites to cooperatively circumnavigate a host spacecraft. The cooperative circumnavigation (CCN) problem is first defined to drive a group of microsatellites to a predefined planar ellipse concerning a host spacecraft while maintaining a geometric formation configuration. Nest, a CCN control law is proposed, where the artificial potential functions and the affine Laplacian matrix are applied to fulfill the requirements of a CCN mission. Finally, simulation results are given to show the feasibility of this approach.
AB - This paper addresses the trajectory analysis, mission design, and control law for multiple microsatellites to cooperatively circumnavigate a host spacecraft. The cooperative circumnavigation (CCN) problem is first defined to drive a group of microsatellites to a predefined planar ellipse concerning a host spacecraft while maintaining a geometric formation configuration. Nest, a CCN control law is proposed, where the artificial potential functions and the affine Laplacian matrix are applied to fulfill the requirements of a CCN mission. Finally, simulation results are given to show the feasibility of this approach.
UR - https://www.scopus.com/pages/publications/85071521227
U2 - 10.23919/ECC.2019.8796233
DO - 10.23919/ECC.2019.8796233
M3 - 会议稿件
AN - SCOPUS:85071521227
T3 - 2019 18th European Control Conference, ECC 2019
SP - 1068
EP - 1072
BT - 2019 18th European Control Conference, ECC 2019
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 18th European Control Conference, ECC 2019
Y2 - 25 June 2019 through 28 June 2019
ER -