Citáce podľa APA (7th ed.)

Li, A., Liu, M., & Shi, Y. (2020). Adaptive sliding mode attitude tracking control for flexible spacecraft systems based on the Takagi-Sugeno fuzzy modelling method. Acta Astronautica, 175, 570-581. https://doi.org/10.1016/j.actaastro.2020.05.041

Citácia podle Chicago (17th ed.)

Li, Ang, Ming Liu, a Yan Shi. "Adaptive Sliding Mode Attitude Tracking Control for Flexible Spacecraft Systems Based on the Takagi-Sugeno Fuzzy Modelling Method." Acta Astronautica 175 (2020): 570-581. https://doi.org/10.1016/j.actaastro.2020.05.041.

Citácia podľa MLA (8th ed.)

Li, Ang, et al. "Adaptive Sliding Mode Attitude Tracking Control for Flexible Spacecraft Systems Based on the Takagi-Sugeno Fuzzy Modelling Method." Acta Astronautica, vol. 175, 2020, pp. 570-581, https://doi.org/10.1016/j.actaastro.2020.05.041.

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