Research Article
Development of Real-Time Maneuver Library Generation Technique for Implementing Tactical Maneuvers of Fixed-Wing Aircraft
Table 3
Parameter description for Figure
3.
| | Final value of the exit phase | | Final time of the exit phase | | Iteration number | | Boundary condition at final time | | Gradient of error | | Tuning parameter for | | Perturbation value for | | Tolerance of error |
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