Simplício, P., Acquatella, P., & Bennani, S. (2025). Design and Analysis of a Launcher Flight Control System Based on Incremental Nonlinear Dynamic Inversion. Aerospace, 12(4), 296. https://doi.org/10.3390/aerospace12040296
Citace podle Chicago (17th ed.)Simplício, Pedro, Paul Acquatella, a Samir Bennani. "Design and Analysis of a Launcher Flight Control System Based on Incremental Nonlinear Dynamic Inversion." Aerospace 12, no. 4 (2025): 296. https://doi.org/10.3390/aerospace12040296.
Citace podle MLA (9th ed.)Simplício, Pedro, et al. "Design and Analysis of a Launcher Flight Control System Based on Incremental Nonlinear Dynamic Inversion." Aerospace, vol. 12, no. 4, 2025, p. 296, https://doi.org/10.3390/aerospace12040296.
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