101. Issues and trends of transitioning from forward flight to hover for landing for a converted hybrid fixed wing VTOL UAS from autopilot perspective.
- Author
-
Zaludin, Zairil
- Subjects
- *
FLIGHT control systems , *AUTOMATIC control systems , *AUTOMATIC pilot (Airplanes) , *HYBRID systems , *AIR speed , *FLIGHT - Abstract
Hybrid UAVs have unique capabilities to take-off and land vertically. For these unique vehicles, there are several ways to achieve these phases of flight successfully. This paper proposes four strategies for a convertible hybrid unmanned aerial vehicle, to transition from forward flight to hover, and then land vertically. Strategy 1 and Strategy 2 suggest reducing forward airspeed gradually to zero while maintaining altitude by regulating the workload between the four motors and the main engine. The difference between these two strategies is the speed of reducing the forward airspeed to begin hovering. Strategy 3 proposes gradually losing altitude while reducing forward airspeed until transition airspeed is reached and hovering to commence. Strategy 4 suggests a way to drop the aircraft vertically by deep stalling in effort to lose altitude quickly but engage the four motors before the aircraft reach the ground. The paper concludes with a brief description of the role of the automatic flight control systems responsible for regulating this transition phase for convertible hybrid UAVs. [ABSTRACT FROM AUTHOR]
- Published
- 2024
- Full Text
- View/download PDF