2013 International Conference on Unmanned Aircraft Systems (ICUAS) 2013
DOI: 10.1109/icuas.2013.6564693
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Design of a commercial hybrid VTOL UAV system

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Cited by 47 publications
(42 citation statements)
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“…The UAV is divided in to two categories, one is fixed wing and second is rotor craft UAV's. However, rotor craft UAV's have an advantage it does not need a runway to execute a flight because of its Vertical Takeoff and Landing (VTOL) ability [2][3][4]. Furthermore, the rotor craft UAV's are also classified in to bi-rotor, tri-rotor, quad-rotor and hex-rotor crafts, having Multiple Input and Multiple Output (MIMO) underactuated systems.…”
Section: Introductionmentioning
confidence: 99%
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“…The UAV is divided in to two categories, one is fixed wing and second is rotor craft UAV's. However, rotor craft UAV's have an advantage it does not need a runway to execute a flight because of its Vertical Takeoff and Landing (VTOL) ability [2][3][4]. Furthermore, the rotor craft UAV's are also classified in to bi-rotor, tri-rotor, quad-rotor and hex-rotor crafts, having Multiple Input and Multiple Output (MIMO) underactuated systems.…”
Section: Introductionmentioning
confidence: 99%
“…The key contributions of this article are: (1) an adaptive sliding surface is proposed to remove the steady state error and for the rejections of model uncertainties (2) the designed ASMC uses linear and angular velocity subcomponents as an input providing practical inside of the real world scenario (3) in spite of the model uncertainties, close loop errors in the UAV system converges to zero, which is proved in the simulation and result section (4) stability of the system is proven by Lyapunov stability function.…”
Section: Introductionmentioning
confidence: 99%
“…With these advantages, the UAV can be the best tool for monitoring the green tide patches, especially at a regional scale. 48,49 Specifically, the UAV was successfully used on the salvage ship during the Ulva bloom disaster in 2016. As shown in Fig.…”
Section: Monitoring Green Tide Using Multi-source Data In the Yellow Seamentioning
confidence: 99%
“…As the speed of the aircraft increases, the proportion of the total lift of the wing is gradually increased, and the lift proportion of the rotor is gradually reduced until the helicopter mode is completed. Fixed-wing mode of conversion, the wing provides the required lift aircraft, the rotor to provide a pull to overcome the resistance of the aircraft flight process [4][5]. In this paper, the general theory of the modeling of the Tilt tri-rotor UAV is given by modeling the power system of the tilt tri-rotor UAV with the positive triangular layout, and the research of the unmanned aerial vehicle The theoretical basis.…”
Section: Introductionmentioning
confidence: 99%