APA (7th ed.) Citation

YAMADA, K., HIGASHIYAMA, D., & SHOJI, Y. (2019). Optimal Attitude Control for Spacecraft Using Two Variable-Speed Control Moment Gyros. TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN, 17(3), 371-379. https://doi.org/10.2322/tastj.17.371

Chicago Style (17th ed.) Citation

YAMADA, Katsuhiko, Daiki HIGASHIYAMA, and Yasuhiro SHOJI. "Optimal Attitude Control for Spacecraft Using Two Variable-Speed Control Moment Gyros." TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN 17, no. 3 (2019): 371-379. https://doi.org/10.2322/tastj.17.371.

MLA (9th ed.) Citation

YAMADA, Katsuhiko, et al. "Optimal Attitude Control for Spacecraft Using Two Variable-Speed Control Moment Gyros." TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN, vol. 17, no. 3, 2019, pp. 371-379, https://doi.org/10.2322/tastj.17.371.