Combined low-thrust propulsion and invariant manifold trajectories to capture NEOs in the Sun-Earth circular restricted three-body problem.

MLA

Mingotti, G., et al. “Combined Low-Thrust Propulsion and Invariant Manifold Trajectories to Capture NEOs in the Sun-Earth Circular Restricted Three-Body Problem.” Celestial Mechanics & Dynamical Astronomy, vol. 120, no. 3, Nov. 2014, pp. 309–36. EBSCOhost, https://doi.org/10.1007/s10569-014-9589-9.

APA

Mingotti, G., Sánchez, J., & McInnes, C. (2014). Combined low-thrust propulsion and invariant manifold trajectories to capture NEOs in the Sun-Earth circular restricted three-body problem. Celestial Mechanics & Dynamical Astronomy, 120(3), 309–336. https://doi.org/10.1007/s10569-014-9589-9

Chicago

Mingotti, G., J. Sánchez, and C. McInnes. 2014. “Combined Low-Thrust Propulsion and Invariant Manifold Trajectories to Capture NEOs in the Sun-Earth Circular Restricted Three-Body Problem.” Celestial Mechanics & Dynamical Astronomy 120 (3): 309–36. doi:10.1007/s10569-014-9589-9.