Fixed-wing UAV Recovery Reliably by Moving Platforms based on Differential Games

Wang, Jinkui; Lou, Wenzhong; Zhao, Yuecen; Liu, Weitong

doi:10.1109/icus48101.2019.8996044

Cited by 2 publications

(1 citation statement)

References 5 publications

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“…1: fixed-wing drones, rotary-wing type drones and airship. Fixed-wing drones have the advantage of being fast and large in payload because the main wing is fixed to the body and flying using the lift, but they cannot stop and take off and land in the air like hovering [4]. A rotary-wing type drone is equipped with multiple propellers (rotor blades), which changes the rotational speed of the propeller, so the payload is small, and it is not resistant to disturbances such as wind.…”

Section: Introductionmentioning

confidence: 99%

Development of a Coanda-Drone with Built-in Propellers

ZHAO,

ZHANG,

LIM

2024

IEICE Trans. Inf. & Syst.

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In this study, a Coanda-drone with length, width, and height of 121.6, 121.6, and 191[mm] was designed, and its total mass was 1166.7[g]. Using four propulsion devices, it could produce a maximum of 5428[g] thrust. Its structure is very different from conventional drones because in this study it combines the design of the jet engine of a jet fixed-wing drone with the fuselage structure layout of a rotary-wing drone. The advantage of jet drone's high propulsion is kept so that it can output greater thrust under the same variation of PWM waveform output. In this study, the propulsion device performs high-speed jetting, and the airflow around the propulsion device will also be jetted downward along the direction of the airflow.

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Section: Introductionmentioning

confidence: 99%