Unmanned Aerial Vehicle control system based on honeycomb mobile communication

A technology for cellular mobile communication and unmanned aerial vehicles, applied in the field of control systems of unmanned aerial vehicles, can solve problems such as flight accidents, transmission speed drops, unpredictable connectivity of time delay bandwidth, etc., achieve strong anti-interference ability, communication antenna Simple and effective in reducing procurement costs

Inactive Publication Date: 2007-03-14
AIR FORCE UNIV PLA
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  • Abstract
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  • Application Information

AI Technical Summary

Problems solved by technology

The digital transmission rate of the second-generation system is only 9.6Kbps, and the transmission speed will drop significantly under mobile conditions
However, due to the characteristics of variable time delay, variable bandwidth, and unpredictable connectivity when using cellular mobile communication for data communication, it cannot fully meet the requirements for real-time control of aircraft.
For example, when GPRS (General Packet Radio Service) has a typical bandwidth of 40kb / s, the data transmission has a delay of 200ms. If the speed of the aircraft is 100km / h, the aircraft has already flown 5.6m when the control command arrives. The delay will lead to serious flight accidents, and because there is no feedback information, the aircraft cannot actually fly beyond the visual range

Method used

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  • Unmanned Aerial Vehicle control system based on honeycomb mobile communication
  • Unmanned Aerial Vehicle control system based on honeycomb mobile communication
  • Unmanned Aerial Vehicle control system based on honeycomb mobile communication

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Embodiment Construction

[0022] Below in conjunction with accompanying drawing and embodiment the present invention will be described in further detail:

[0023] As shown in Figure 1, a kind of unmanned aerial vehicle control system based on cellular mobile communication comprises the following devices: the autopilot Xn that is arranged in the unmanned aerial vehicle Fn controls the autonomous flight of the unmanned aerial vehicle Fn by the preset mission , a ground console 1 that presets flight tasks for the unmanned aerial vehicle Fn and displays the actual flight status of the unmanned aerial vehicle Fn; the unmanned aerial vehicle Fn can have F1, F2, ... FnN frames, and the number of N is no more than 6 , the corresponding autopilot Xn also has X1, X2, ..., XnN cover; Described each set of autopilot X1, X2, ..., Xn and the ground console 1 respectively have a SIM card 26 storing a cellular mobile communication number and SIM card 8; between the autopilot Xn and the ground console 1, the cellular m...

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Abstract

This invention discloses one beehive mobile communication aviation control system, which comprises the following parts: automatic driver device to control aviation as set task control; earth control bench and beehive mobile communication system to set fly task and display aviation status; the said aviator has several planes with each set with automatic driver device to own one SIM card of mobile communication codes; the automatic driver and earth control bench realize double data communication linkage through earth base station and beehive mobile network.

Description

technical field [0001] The invention relates to a control system of an unmanned aerial vehicle, in particular to a control system of an unmanned aerial vehicle based on cellular mobile communication. Background technique [0002] In addition to military uses, unmanned aerial vehicles are also widely used in civilian applications, such as collecting atmospheric samples, mapping, resource surveys, disaster investigations, and anti-drug reconnaissance. Unmanned aerial vehicles include unmanned aircraft, helicopters and airships, etc., and are generally composed of power devices and power systems, automatic control devices and actuators, wireless communication and navigation systems, mission systems and remote control systems, and most of them also require ground control. system. Except for large unmanned aircraft using gas turbine engines, the flying speed of unmanned aerial vehicles is generally below 400km / h, the flying speed of helicopters is not more than 200km / h, and the ...

Claims

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Application Information

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IPC IPC(8): H04B7/185H04Q7/22A63H30/04
Inventor 陈卫程礼李康杨帆
Owner AIR FORCE UNIV PLA
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