Periodic Model Predictive Control for Tracking Halo Orbits in the Elliptic Restricted Three-Body Problem
R Quartullo, A Garulli… - IEEE Transactions on …, 2023 - ieeexplore.ieee.org
A periodic model predictive control (MPC) scheme is proposed for tracking halo orbits. The
problem is formulated and solved in the elliptic restricted three-body problem (ER3BP) …
problem is formulated and solved in the elliptic restricted three-body problem (ER3BP) …
Artificial Triangular Points by Lorentz Force in the Restricted Three‐Body Problem
The restricted three body problem was outlined. The acceleration due to planetary magnetic
field, in terms of space craft's orbital elements, was analysed. The conditions for calculating …
field, in terms of space craft's orbital elements, was analysed. The conditions for calculating …
Halo Orbit Maintenance around Point of the Sun-Earth System Using Optimal Control and Lyapunov Stability Theory
V Ramteke, SR Kumar - Journal of Aerospace Engineering, 2022 - ascelibrary.org
This paper addresses the maintenance of a halo orbit around the L 1 point of the Sun-Earth
system in a circular restricted three-body problem. To this effect, a trajectory tracking …
system in a circular restricted three-body problem. To this effect, a trajectory tracking …