“…Several methods have been used so far by researchers ranging from location-based Target Point Approach (TPA), shape-similar trajectories, to finite-time Lyapunov exponents (FTLEs) in the form of the Cauchy Green Tensor (CGT) [17,18,25,27,28]. Studies performed on the effects of the Sun's gravity on the spacecraft as an additional perturbing force, through the Bi-Circular Restricted Four-Body Problem (BCR4BP) in the Sun-Earth-Moon system which presented significant positional deviation from a perfectly periodic halo orbit [6][7][8][9][10]. For Europa, due to the proximity to both Io and Ganymede, the Concentric Circular Restricted Four-Body Problem (CCR4BP) was a better approximation as all three moons are in resonance with each other [19,20].…”