Research Article
Multiple Spacecraft Formation Flying Control around Artificial Equilibrium Point Using Propellantless Approach
Table 3
The control performance of control algorithms (take follower 1 as an example).
| | Controller | Terminal relative position errors max (,,) [m] | Terminal relative velocity errors max (,,)[m/s] | Average variation of angle [deg] | Average variation of charge product [C2] |
| | MFITSMC | (0.012,0.018,0.022) | | (0.0285,0.0101) | | | FTSMC | (0.15,0.118,0.038) | | (0.0244,0.0078) | | | PID | (0.95,0.78,0.42) | | (0.0084,0.0042) | |
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