Research Article
Multiaircraft Optimal 4D Trajectory Planning Using Logical Constraints
Table 3
Boundary conditions for Experiment 2.
| Symbol | Unit | Aircraft 1 | Aircraft 2 | Aircraft 3 |
| | m | 7400 | 7400 | 7400 | | m | 3350 | 3350 | 3350 | | deg | 39.000 | 39.000 | 38.701 | | deg | 40.575 | 40.575 | 40.848 | | deg | -5.327 | -3.325 | -4.320 | | deg | -3.430 | -5.215 | -4.320 | | m/s | 130 | 130 | 130 | | m/s | 110 | 110 | 110 | | deg | 0 | 0 | 0 | | deg | 0 | 0 | 0 | | deg | 356 | 294 | 294 | | kg | 65000 | 65000 | 65000 |
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