Cite
Closed-Form Impact-Angle-Control Guidance of Nose-Dive Missiles for Maximum Terminal Speed
MLA
Han-Lim Choi, et al. “Closed-Form Impact-Angle-Control Guidance of Nose-Dive Missiles for Maximum Terminal Speed.” International Journal of Aeronautical and Space Sciences, vol. 22, Apr. 2021, pp. 1428–39. EBSCOhost, https://doi.org/10.1007/s42405-021-00361-3.
APA
Han-Lim Choi, In-Soo Jeon, & Iksoo Kim. (2021). Closed-Form Impact-Angle-Control Guidance of Nose-Dive Missiles for Maximum Terminal Speed. International Journal of Aeronautical and Space Sciences, 22, 1428–1439. https://doi.org/10.1007/s42405-021-00361-3
Chicago
Han-Lim Choi, In-Soo Jeon, and Iksoo Kim. 2021. “Closed-Form Impact-Angle-Control Guidance of Nose-Dive Missiles for Maximum Terminal Speed.” International Journal of Aeronautical and Space Sciences 22 (April): 1428–39. doi:10.1007/s42405-021-00361-3.