Research Article

Continuous-Thrust Station-Keeping of Cis-Lunar Orbits Using Optimal Sliding Mode Control with Practical Constraints

Figure 8

The station-keeping for the nominal orbits with the SRP as the perturbation.
(a) 2 : 1 DRO with LQR controller
(b) 2 : 1 DRO with OSMC controller
(c) 9 : 2 NRHO with LQR controller
(d) 9 : 2 NRHO with OSMC controller
(e) Halo (3) with LQR controller
(f) Halo (3) with OSMC controller