Cite
Incremental model predictive control for satellite de-orbiting based on drag modulation.
MLA
La Marca, Tobia Armando, et al. “Incremental Model Predictive Control for Satellite De-Orbiting Based on Drag Modulation.” Acta Astronautica, vol. 215, Feb. 2024, pp. 708–24. EBSCOhost, https://doi.org/10.1016/j.actaastro.2023.12.046.
APA
La Marca, T. A., Nocerino, A., Opromolla, R., & Grassi, M. (2024). Incremental model predictive control for satellite de-orbiting based on drag modulation. Acta Astronautica, 215, 708–724. https://doi.org/10.1016/j.actaastro.2023.12.046
Chicago
La Marca, Tobia Armando, Alessia Nocerino, Roberto Opromolla, and Michele Grassi. 2024. “Incremental Model Predictive Control for Satellite De-Orbiting Based on Drag Modulation.” Acta Astronautica 215 (February): 708–24. doi:10.1016/j.actaastro.2023.12.046.