Cite
Orbit Correction Strategy of LEO Vehicle Based on Linearized Orbital Motion Equation.
MLA
WANG Tao, et al. “Orbit Correction Strategy of LEO Vehicle Based on Linearized Orbital Motion Equation.” Chinese Space Science & Technology / Zhongguo Kongjian Kexue Jishu, vol. 34, no. 2, Apr. 2014, pp. 22–35. EBSCOhost, https://doi.org/10.3780/j.issn.1000-758X.2014.02.003.
APA
WANG Tao, ZHANG Hongbo, & TANG Guojian. (2014). Orbit Correction Strategy of LEO Vehicle Based on Linearized Orbital Motion Equation. Chinese Space Science & Technology / Zhongguo Kongjian Kexue Jishu, 34(2), 22–35. https://doi.org/10.3780/j.issn.1000-758X.2014.02.003
Chicago
WANG Tao, ZHANG Hongbo, and TANG Guojian. 2014. “Orbit Correction Strategy of LEO Vehicle Based on Linearized Orbital Motion Equation.” Chinese Space Science & Technology / Zhongguo Kongjian Kexue Jishu 34 (2): 22–35. doi:10.3780/j.issn.1000-758X.2014.02.003.