Research Article
VTOL UAV Transition Maneuver Using Incremental Nonlinear Dynamic Inversion
Figure 1
UAV aerodynamic and power configurations.
| (a) Vectored thrust of power system |
| (b) UAV power system |
| (c) Vectored thrust of lift fan |
| (d) Lift fan |
| (e) Vectored thrust of engine |
| (f) Thrust vector engine |