Cite
Unconstrained Direct Optimization of Spacecraft Trajectories Using Many Embedded Lambert Problems.
MLA
Ottesen, David, and Ryan P. Russell. “Unconstrained Direct Optimization of Spacecraft Trajectories Using Many Embedded Lambert Problems.” Journal of Optimization Theory & Applications, vol. 191, no. 2/3, Dec. 2021, pp. 634–74. EBSCOhost, https://doi.org/10.1007/s10957-021-01884-1.
APA
Ottesen, D., & Russell, R. P. (2021). Unconstrained Direct Optimization of Spacecraft Trajectories Using Many Embedded Lambert Problems. Journal of Optimization Theory & Applications, 191(2/3), 634–674. https://doi.org/10.1007/s10957-021-01884-1
Chicago
Ottesen, David, and Ryan P. Russell. 2021. “Unconstrained Direct Optimization of Spacecraft Trajectories Using Many Embedded Lambert Problems.” Journal of Optimization Theory & Applications 191 (2/3): 634–74. doi:10.1007/s10957-021-01884-1.