Method for calculating the perturbed trajectoryof a two-impulse flight between the halo orbit in the vicinity of the L2 point of the Sun — Earth systemand the near-lunar orbit
Published: 19.11.2020
Authors: Rui Zhou
Published in issue: #11(107)/2020
DOI: 10.18698/2308-6033-2020-11-2033
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control