Cite
Proportional-Integral-Type Event-Triggered Coupled Attitude and Orbit Tracking Control Using Dual Quaternions.
MLA
Li, Chunhui, et al. “Proportional-Integral-Type Event-Triggered Coupled Attitude and Orbit Tracking Control Using Dual Quaternions.” IEEE Transactions on Aerospace & Electronic Systems, vol. 58, no. 4, Aug. 2022, pp. 3021–36. EBSCOhost, https://doi.org/10.1109/TAES.2022.3143475.
APA
Li, C., Zou, H., Shi, D., Song, J., & Wang, J. (2022). Proportional-Integral-Type Event-Triggered Coupled Attitude and Orbit Tracking Control Using Dual Quaternions. IEEE Transactions on Aerospace & Electronic Systems, 58(4), 3021–3036. https://doi.org/10.1109/TAES.2022.3143475
Chicago
Li, Chunhui, Hengguang Zou, Dawei Shi, Jiliang Song, and Junzheng Wang. 2022. “Proportional-Integral-Type Event-Triggered Coupled Attitude and Orbit Tracking Control Using Dual Quaternions.” IEEE Transactions on Aerospace & Electronic Systems 58 (4): 3021–36. doi:10.1109/TAES.2022.3143475.