APA (7th ed.) Citation

Xu, S., Sun, G., & Sun, W. (2017). Fuzzy logic based fault-tolerant attitude control for nonlinear flexible spacecraft with sampled-data input. Journal of the Franklin Institute, 354(5), 2125-2156. https://doi.org/10.1016/j.jfranklin.2017.01.010

Chicago Style (17th ed.) Citation

Xu, Shidong, Guanghui Sun, and Weichao Sun. "Fuzzy Logic Based Fault-tolerant Attitude Control for Nonlinear Flexible Spacecraft with Sampled-data Input." Journal of the Franklin Institute 354, no. 5 (2017): 2125-2156. https://doi.org/10.1016/j.jfranklin.2017.01.010.

MLA (9th ed.) Citation

Xu, Shidong, et al. "Fuzzy Logic Based Fault-tolerant Attitude Control for Nonlinear Flexible Spacecraft with Sampled-data Input." Journal of the Franklin Institute, vol. 354, no. 5, 2017, pp. 2125-2156, https://doi.org/10.1016/j.jfranklin.2017.01.010.