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Landing fixing device for unmanned aerial vehicle and fixing method for landing fixing device

A technology of unmanned aerial vehicle and fixing device, applied in the field of unmanned aerial vehicle, can solve problems such as fixing of unmanned aerial vehicle, and achieve the effect of avoiding back and forth vibration

Active Publication Date: 2016-08-03
余江
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

However, this patent cannot allow the unmanned aerial vehicle to be automatically fixed after landing, and ground operators need to be powered on; moreover, this patent cannot flexibly respond to different winds and then adjust the size of the adsorption force so as to maintain an appropriate adsorption force and the unmanned aerial vehicle is fixed. Assure

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  • Landing fixing device for unmanned aerial vehicle and fixing method for landing fixing device
  • Landing fixing device for unmanned aerial vehicle and fixing method for landing fixing device
  • Landing fixing device for unmanned aerial vehicle and fixing method for landing fixing device

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Embodiment Construction

[0029] The following detailed description is merely exemplary in nature and not intended to limit application and uses. Furthermore, there is no intention to be bound by any expressed or implied theory presented in the preceding technical field, background, brief summary or the following detailed description.

[0030] Embodiments of the present invention describe a landing fixture for unmanned aerial vehicles, such as figure 1The schematic diagram of the landing fixture of the shown unmanned aerial vehicle according to an embodiment of the present invention, the landing fixture of the unmanned aerial vehicle includes the landing platform 1 for carrying the described unmanned aerial vehicle of landing and is arranged on the unmanned aerial vehicle The fixing device 2, the fixing device 2 includes a sensor 3, an excitation device 4 and an electromagnet core 5, the sensor 3 detects that the unmanned aerial vehicle is in a landing state and sends a landing signal to the excitation...

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Abstract

The invention provides a landing fixing device for an unmanned aerial vehicle and a fixing method for the landing fixing device. The landing fixing device for the unmanned aerial vehicle comprises a landing table (1) used for carrying the landing unmanned aerial vehicle and a fixing device body (2) arranged on the unmanned aerial vehicle. The fixing device body (2) comprises a sensor (3), an excitation device (4) and an electromagnet core (5). The sensor (3) detects that the unmanned aerial vehicle is in a landing state and sends a landing signal to the excitation device (4), and the excitation device (4) connected with the sensor (3) conducts excitation on the electromagnet core (5) on the basis of the landing signal, so that the unmanned aerial vehicle is attracted to the landing table (1) through the electromagnet core (5).

Description

technical field [0001] The invention belongs to the field of unmanned aerial vehicles, and in particular relates to a landing fixing device and a fixing method for an unmanned aerial vehicle. Background technique [0002] With the increasing intelligence of UAVs, UAVs can realize automatic control in various flight links such as take-off, navigation, and landing, and human intervention is less and less, making UAVs from the current one player Controlling the consumer model of always controlling a drone is changing to a commercial application model such as large-scale express delivery. However, in this large-scale commercial application model, each drone is no longer under human control all the time, and many Sometimes it is necessary to autonomously and automatically respond to some scenarios. For example, the aircraft may not be recovered immediately after landing. Considering the weight of the drone itself is relatively light, even a light wind on the ground may cause the...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C25/00B64F1/02
CPCB64C25/001B64F1/02
Inventor 余江
Owner 余江
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