Spacecraft Attitude Control on 300 MC Simulation Runs
0.0024Steady-State Error (deg)Linear MPC
Evaluation Results
| Method | Links | ||
|---|---|---|---|
| Linear MPC2025.08 | 0.0024 | 114.1 | |
| NVPSA2-LDLoss Type=Physics-informed / Hybrid loss2025.08 | 0.0464 | 42.8 | |
| Non-Linear MPC2025.08 | 0.1215 | 186.2 | |
| NVPSA2-DDLoss Type=Data-Driven2025.08 | 0.5865 | 65 |