Cite
Suboptimal attitude tracking control law and eigenvalue analysis for a near-space hypersonic vehicle based on Koopman operator and stable manifold method.
MLA
Mi, Peichao, et al. “Suboptimal Attitude Tracking Control Law and Eigenvalue Analysis for a Near-Space Hypersonic Vehicle Based on Koopman Operator and Stable Manifold Method.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, vol. 237, no. 6, May 2023, pp. 1417–34. EBSCOhost, https://doi.org/10.1177/09544100221125963.
APA
Mi, P., Wu, Q., & Wang, Y. (2023). Suboptimal attitude tracking control law and eigenvalue analysis for a near-space hypersonic vehicle based on Koopman operator and stable manifold method. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 237(6), 1417–1434. https://doi.org/10.1177/09544100221125963
Chicago
Mi, Peichao, Qingxian Wu, and Yuhui Wang. 2023. “Suboptimal Attitude Tracking Control Law and Eigenvalue Analysis for a Near-Space Hypersonic Vehicle Based on Koopman Operator and Stable Manifold Method.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 237 (6): 1417–34. doi:10.1177/09544100221125963.