Correction: Fault-Tolerant Model Predictive Control for Spacecraft Formations via Nonlinear Regression

Correction NoticeThe results section includes updated figures comparing the performance of the proposed system with another controller of similar design as a baseline.For all cases, we are comparing the performance of the controller to a previously proposed Nonsingular Terminal Sliding Mode Controller (NTSMC) [7].In the baseline case, we see performance increase in our system over NTSMC, showing our proposed systems optimality under a standard operating condition.The fault cases either show similar baseline or improvements in all proposed plots, depending on the severity of faults.An acknowledgement about AI usage is also included to clarify the involvement of AI in this work as only a revision tool for grammar and formatting and not as a technical tool for system design.Fig. 4 Case 1: 1km Offset with no faults