Tu, L., Wang, Y., Yan, C., & Yang, Y. (2023). Optimal transfer orbit design of spacecraft with finite thrust based on Legendre pseudospectral method. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 237(8), 1791-1797. https://doi.org/10.1177/09544100221138164

TU, Lianghui, WANG, Yuhao, YAN, Chao und YANG, Yang, 2023. Optimal transfer orbit design of spacecraft with finite thrust based on Legendre pseudospectral method. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 15 Juni 2023. Vol. 237, no. 8, p. 1791-1797. DOI 10.1177/09544100221138164.

Tu, L., Y. Wang, C. Yan, und Y. Yang. „Optimal Transfer Orbit Design of Spacecraft With Finite Thrust Based on Legendre Pseudospectral Method.“. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Bd. 237, Nr. 8, Juni 2023, S. 1791-7, https://doi.org/10.1177/09544100221138164.

Tu, Lianghui/Wang, Yuhao/Yan, Chao/Yang, Yang: Optimal transfer orbit design of spacecraft with finite thrust based on Legendre pseudospectral method., Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 2023, 1791-1797.

Tu, L., Wang, Y., Yan, C. und Yang, Y. (2023), „Optimal transfer orbit design of spacecraft with finite thrust based on Legendre pseudospectral method.“, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Vol. 237 No. 8, S. 1791-1797.