Keeping a Spacecraft on a Vertical Circular Collinear Lagrange Point Orbit
M Ghazy, B Newman - Journal of guidance, control, and dynamics, 2010 - arc.aiaa.org
IN PREVIOUS research [1], a circular orbit in a plane perpendicular to the line joining the
two primaries of a restricted three-body system is used as a nominal generating orbit for an …
two primaries of a restricted three-body system is used as a nominal generating orbit for an …