Cite
Maneuver Attitude Control Method and In-Orbit Verification for Flexible Satellites with Single-Gimbal Control Moment Gyros.
MLA
YUAN Li, et al. “Maneuver Attitude Control Method and In-Orbit Verification for Flexible Satellites with Single-Gimbal Control Moment Gyros.” Journal of Astronautics / Yuhang Xuebao, vol. 39, no. 1, Jan. 2018, pp. 43–51. EBSCOhost, https://doi.org/10.3873/j.issn.1000-1328.2018.01.006.
APA
YUAN Li, LEI Yong-jun, YAO Ning, LIU Jie, & ZHU Qi. (2018). Maneuver Attitude Control Method and In-Orbit Verification for Flexible Satellites with Single-Gimbal Control Moment Gyros. Journal of Astronautics / Yuhang Xuebao, 39(1), 43–51. https://doi.org/10.3873/j.issn.1000-1328.2018.01.006
Chicago
YUAN Li, LEI Yong-jun, YAO Ning, LIU Jie, and ZHU Qi. 2018. “Maneuver Attitude Control Method and In-Orbit Verification for Flexible Satellites with Single-Gimbal Control Moment Gyros.” Journal of Astronautics / Yuhang Xuebao 39 (1): 43–51. doi:10.3873/j.issn.1000-1328.2018.01.006.