Abstract
AbstractThe use of solar radiation pressure for station-keeping at a sub-L2 Sun-Earth/Moon collinear libration point is presented. Numerical halo and Lissajous reference trajectories are generated for the sub-L2 libration point. Owing to the instability of these orbits, active station-keeping is required to prevent spacecraft escape after orbit insertion. The control inputs for solar sail control include area variation and solar sail pitch and roll angle variations. A nonlinear higher order control method is developed to utilize solar radiation pressure to minimize the trajectory tracking error. The stability of the proposed controllers is established using the Lyapunov theory. The performance of the proposed controllers is tested through numerical simulation of the governing nonlinear equations of motion and is applied for station-keeping in the elliptical restricted three-body problem. It is shown that underactuated control is able to keep the spacecraft motion bounded, but the tracking error remains hi...
Published Version
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a call