Tail-Sitter Vertical Takeoff and Landing Unmanned Aerial Vehicle: Transitional Flight Analysis

Abstract

A new design for a tail-sitter vertical takeoff and landing unmanned aerial vehicle was proposed. A nonlinear mathematical model of the vehicle dynamics was constructed by combining simple estimation methods. The flight characteristics were revealed through a trim analysis and an optimized transitional flight path analysis by using the mathematical model. The trim analysis revealed the existence of a flight path constraint to avoid stall; the vehicle could not descend in low-speed flight without high-lift devices such as flaps and slats. These devices improved the descentperformance. Inparticular, slatsprovidedasubstantialimprovement; theyenabled adescent rateof2 m=s. In the optimized transitional flight path analysis, a level outbound transition without high-lift devices was achieved althoughatrimmedlevel flightatlowspeed,aswasshowninthetrimanalysis,wasnotpossible;thiswasbecausethe outboundtransition wasanaccelerative flight.Onthe contrary,without high-lift devices, the vehicle could notavoid climbing to avoid stall during inbound transitions. The slats provided a satisfactory improvement during the transition and enabled a level inbound transition. These results showed the necessity of leading-edge slats for the proposed tail-sitter vertical takeoff and landing unmanned aerial vehicle.