The Design concept of the TURAC in cruise ( a ) and hover ( b ) …
A successive linearization based model predictive control (SLMPC) method is proposed to control a vertical take-off and landing (VTOL) tail-sitter unmanned aerial vehicle (UAV) in hovering...
Design of a commercial hybrid VTOL UAV system - IEEE Xplore
The main topic of this project is designing, producing and testing the TURAC VTOL UAV that have the following features: • Vertical takeoff and landing, and hovering like helicopter • High cruise speed and fixed-wing • Multi-functional and designed for civil purpose • The project involves two different variants: • The TURAC A variant ...
Design of a commercial hybrid VTOL UAV system - ResearchGate
May 1, 2013 · The main topic of this project is designing, producing and testing the TURAC VTOL UAV that have the following features : Vertical takeoff and landing, and hovering like helicopter ; High cruise...
Design of a Commercial Hybrid VTOL UAV System
Apr 1, 2014 · In this paper, we review the preliminary design process of such a capable civilian UAV system, namely the TURAC VTOL UAV. TURAC UAV is aimed to have both vertical take-off and landing and Conventional Take-off and Landing (CTOL) capability.
A low cost prototyping approach for design analysis and flight …
TURAC - a VTOL Tilt Rotor UAV with these capabilities - is designed. Although mathematical and CFD analyses were performed iteratively in order to optimize the design, testing in real life conditions were needed to see the real performance of the TURAC UAV.
Design of a commercial hybrid VTOL UAV system - ResearchGate
Apr 1, 2014 · In this paper, we review the preliminary design process of such a capable civilian UAV system, namely the TURAC VTOL UAV. TURAC UAV is aimed to have both vertical take-off and landing and...
In this paper, we review the pre-liminary design process of such a capable civil-ian UAV system, namely the TURAC VTOL UAV. TURAC UAV is aimed to have both ver-tical take-off and landing and Conventional Take-off and Landing (CTOL) capability.
Design of a Commercial Hybrid VTOL UAV System - Semantic …
In this paper, we review the preliminary design process of such a capable civilian UAV system, namely the TURAC VTOL UAV. TURAC UAV is aimed to have both vertical take-off and landing and Conventional Take-off and Landing (CTOL) capability.
Dynamic modeling of a fixed-wing VTOL UAV - IEEE Xplore
This paper presents a transition-flight mathematical model of a civil tilt-rotor VTOL unmanned aerial vehicle (UAV) TURAC. Forces and moments acting on the UAV body are calculated using Newton's second law. Aerodynamic effects of free airstream and propeller airstream are …
Rapid Prototyping of a Fixed-Wing VTOL UAV for Design Testing
Feb 18, 2016 · Most civilian applications require UAVs to be low cost, portable, and easily packaged while also having Vertical Take-off and Landing (VTOL) capability. In light of this, the TURAC was designed, a VTOL Tilt Rotor UAV with these capabilities.
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