2019
DOI: 10.1016/j.compag.2019.105036
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Numerical analysis and validation of spray distributions disturbed by quad-rotor drone wake at different flight speeds

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Cited by 76 publications
(42 citation statements)
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“…Since the drone arms are often the most common locations for lifting the aircraft by the ground crew, wearing proper personal protection equipment (PPE) is important. It is also important to note that mitigating the risk of airborne drift and operator exposures remains a top priority for aerial, and all application operations 14,24,25 . These data, although only from a single trial, are encouraging indications that minimal aircraft contamination and spray interference may be achievable.…”
Section: Resultsmentioning
confidence: 94%
See 1 more Smart Citation
“…Since the drone arms are often the most common locations for lifting the aircraft by the ground crew, wearing proper personal protection equipment (PPE) is important. It is also important to note that mitigating the risk of airborne drift and operator exposures remains a top priority for aerial, and all application operations 14,24,25 . These data, although only from a single trial, are encouraging indications that minimal aircraft contamination and spray interference may be achievable.…”
Section: Resultsmentioning
confidence: 94%
“…It is also important to note that mitigating the risk of airborne drift and operator exposures remains a top priority for aerial, and all application operations. 14,24,25 These data, although only from a single trial, are encouraging indications that minimal aircraft contamination and spray interference may be achievable.…”
Section: Active Ingredient Recovery On the Aircraftmentioning
confidence: 96%
“…Notice that pesticide droplets drift toward the opposite of UAV flight direction. For a M234-AT model quadrotor fitted with a pressure nozzle made by Lechler GmbH (Metzingen, Germany), the relationship between the drift and the distance behind the UAV, given that the nozzle position is 0.5 m, the distance between nozzles is 0.25 m, the flight height is 1.5 m, and the flight speed 6 m/s, can be expressed as [ 38 ]: where represents the percentage of the drift behind the UAV to the total drift, in percentage; represents the distance to the rear of the fuselage, in meters. Furthermore, Equation (8) can be rewritten as: …”
Section: System Modelmentioning
confidence: 99%
“…If hover extends for a significant fraction of the mission duration, hover efficiency becomes a key vehicle characteristic that must be carefully addressed. Since rotor wakes will produce the phenomena of distortion, winding and crushing due to the induction between wakes, which affects the aerodynamic performance of the quadrotor aircraft, therefore, appropriate rotor spacing should be selected wisely to reduce aerodynamic interference for the structural design of the quadrotor aircraft [6,7].…”
Section: Introductionmentioning
confidence: 99%