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Unmanned aerial vehicle

Gao Peng, +1 more
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TLDR
In this article, an unmanned aerial vehicle (UAV) consisting of an upper body part, a middle body part and a lower body part is described, where the upper body is composed of at least one machine arm, each paddle is attached to the corresponding machine arm through a corresponding motor.
Abstract
The invention relates to an unmanned aerial vehicle which comprises an upper body part, a middle body part and a lower body part, wherein the upper body part is composed of at least one machine arm; at least one paddle is arranged on each machine arm; each paddle is connected to the corresponding machine arm through a corresponding motor; the middle body part is composed of a damping component; the lower body part is composed of a casing; and a controlling component which is connected with the motors are arranged in the casing and is used for controlling the motors to drive the corresponding paddles to rotate. The unmanned aerial vehicle is in a new unmanned aircraft layout manner, and breaks the conventional flight attitude of the unmanned aerial vehicle. According to the unmanned aerial vehicle, vibration generated by the upper body part can be greatly weakened and even to zero through the damping component of the middle body part, and thus flight is more balance.

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Patent

Aerial vehicle and control method thereof and computer readable storage medium

Jia Zehao, +1 more
TL;DR: In this paper, an unmanned aerial vehicle (UAV) comprises at least two processors and a gate module, where each processor of the UAV simultaneously outputs a drivingsignal after the aerial vehicle is started, and the gate module is used for receiving driving signals of the at least 2 processors and selecting a driving signal generated by a non-abnormal processor from the received driving signals and transmitting the driving signal to a motor of the AUV.
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References
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Patent

Hovering unmanned aerial vehicle

TL;DR: In this article, an HUAV has an arm assembly configured to support a propeller in such a way that propeller drag of the propeller is decoupled from yaw torque requirements associated with the hovering UAV.
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TL;DR: In this article, a multi-rotor unmanned aerial vehicle (UAV) for fast surveying and a surveying method of the UAV is described, which belongs to the technical field of aviation surveying, and can be used for determining the relation between the shooting height and the imaging proportion by analyzing camera lens parameters.
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Downwards foldable-type multi-rotor wing unmanned aerial vehicle

Zhang Zilin, +1 more
TL;DR: In this paper, a downwards foldable-type multi-rotor wing unmanned aerial vehicle (UAV) consisting of a power device (200), a camera shooting device (300), a cell system (400), a control circuit (600), a plurality of support arms (110), a central mounting seat (120), and a locking component (150), was presented.
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Multi-rotor unmanned aerial vehicle

TL;DR: In this paper, a multi-rotor unmanned aerial vehicle (UAV) consisting of a vehicle frame, a plurality of rotor sets and a power device is described, and a variable pitch device is fixed to each rotor set correspondingly to control the pitch of the rotors in the rotor set.
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Six unmanned aerial vehicle

Liao Qiuxiong
TL;DR: In this article, a six unmanned aerial vehicle in aviation UAV field, circuit control system on including fuselage, camera subassembly and locating the fuselage is described, the camera subassembles includes infrared thermal imaging camera and cloud platform camera, border toward the outer horn that forms more than the six roots of sensation that extends of fuselage base.