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A multi-control system for unmanned aerial vehicles

A technology of drones and remote controllers, which is applied in the field of multi-control systems for drones, and can solve problems such as inconvenient operation, complex application terrain, and limited line of sight for operators

Active Publication Date: 2019-01-22
浙江翔龙航空科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, when the UAV is operating, especially when spraying medicine, rescue, or special operations, the operator must control the UAV through the remote control. Due to the complex application terrain and the limited line of sight of the operator, it is extremely difficult to operate the UAV. Inconvenient, and the drone's automation isn't working at its best

Method used

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  • A multi-control system for unmanned aerial vehicles
  • A multi-control system for unmanned aerial vehicles
  • A multi-control system for unmanned aerial vehicles

Examples

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Embodiment Construction

[0020] The present invention will be further described below in conjunction with accompanying drawing.

[0021] Such as Figure 1-3 As shown, a UAV multi-control system, including multiple remote controllers to control UAVs and UAVs jointly controlled,

[0022] The remote controller includes a charging module, a power module, a CPU main control module, a GPS positioning device, a wireless communication module, a channel information collection module and a status indication module, and a password pairing keyboard;

[0023] The drone includes a power unit, a CPU main control module, a GPS positioning device, a wireless communication module, an attitude information module, a pairing password setting keyboard, and a confirmation switch key.

[0024] A kind of unmanned aerial vehicle multi-control method: comprises the steps:

[0025] ((1) Pairing between the remote control and the drone: set a pairing password on the pairing password setting keyboard of the drone, and enter the ...

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PUM

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Abstract

The invention discloses a multi-control method for an unmanned aerial vehicle. A CPU main control module of a remote controller sends out a signal, which is transmitted to an unmanned aerial vehicle through a wireless communication module, and the unmanned aerial vehicle works according to instructions after receiving the signal through the wireless communication module. Both the remote controller and the drone have GPS positioning devices. The shared remote controller inputs the control password to realize pairing with the drone. They send and receive signals through the wireless communication module to realize the sharing of geographical coordinates. The drone uses the distance The algorithm judges or chooses to switch the remote control control independently according to the strength of the remote control signal, so as to realize the multi-control of the drone.

Description

technical field [0001] The invention relates to an unmanned aerial vehicle multi-control system. Background technique [0002] According to the application field, UAV can be divided into military and civilian. In terms of military use, UAVs are divided into reconnaissance aircraft and target aircraft. In terms of civilian use, drones + industry applications are the real rigid needs of drones; currently, they are used in aerial photography, agriculture, plant protection, selfies, express delivery, disaster rescue, wildlife observation, infectious disease monitoring, surveying and mapping, news reports, and power inspections. Applications in fields such as disaster relief, film and television shooting, and romance manufacturing have greatly expanded the use of drones themselves. Developed countries are also actively expanding industry applications and developing drone technology. However, when the UAV is operating, especially when spraying medicine, rescue, or special operat...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C39/02G08C17/02
CPCG05D1/0808G05D1/101G08C17/02B64C39/024B64U2101/00B64U2201/20
Inventor 孙晋生
Owner 浙江翔龙航空科技有限公司
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