Commonalities between robust hybrid incremental nonlinear dynamic inversion and proportional-integral-derivative flight control law design.

MLA

Pollack, T. S. C., et al. “Commonalities between Robust Hybrid Incremental Nonlinear Dynamic Inversion and Proportional-Integral-Derivative Flight Control Law Design.” Aerospace Science & Technology, vol. 152, Sept. 2024, p. N.PAG. EBSCOhost, https://doi.org/10.1016/j.ast.2024.109377.

APA

Pollack, T. S. C., Theodoulis, S. T., & van Kampen, E. (2024). Commonalities between robust hybrid incremental nonlinear dynamic inversion and proportional-integral-derivative flight control law design. Aerospace Science & Technology, 152, N.PAG. https://doi.org/10.1016/j.ast.2024.109377

Chicago

Pollack, T.S.C., S.T. Theodoulis, and E. van Kampen. 2024. “Commonalities between Robust Hybrid Incremental Nonlinear Dynamic Inversion and Proportional-Integral-Derivative Flight Control Law Design.” Aerospace Science & Technology 152 (September): N.PAG. doi:10.1016/j.ast.2024.109377.