PC-control-supporting multi-rotor-wing unmanned-aerial-vehicle control system

A multi-rotor unmanned and control system technology, applied in the field of aircraft communication control, can solve the problems of few safety protection functions, limited coverage of wireless remote control signals, and low scalability of controlling aircraft, so as to improve the incomplete information collection and display , Make up for the effect of limited flight radius

Active Publication Date: 2016-05-04
JINAN UNIVERSITY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In terms of the control system, most of the relevant multi-rotor unmanned aerial vehicles are controlled by wireless remote controllers, and this type of remote controller is very difficult for novices to get started, and it takes a certain amount of exercise to control the aircraft well.
And due to the limited signal coverage of the wireless remote control, the flight radius of the multi-rotor UAV is also limited.
In addition, due to the functional limitations of the remote control, the scalability of controlling the aircraft is also low
In short, the existing remote control-based control system is not only cumbersome to operate, has few safety protection functions, and limited flight radius, but also has single function, low scalability, and lack of humanized operation interface, which is not conducive to the further development of aircraft technology.

Method used

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  • PC-control-supporting multi-rotor-wing unmanned-aerial-vehicle control system

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Embodiment

[0042] This embodiment discloses a multi-rotor unmanned aerial vehicle control system that supports PC control, which not only greatly reduces the difficulty of operation, improves operational safety, and expands the flight control range, but also supports real-world control of multi-rotor aircraft through video transmission. . In addition, multicopter enhancements can be further enhanced by developing expansive plug-ins on the PC.

[0043] The basic structure of the control system is as follows figure 1 shown. It mainly includes the multi-rotor UAV platform, the PC-side ground control platform, and the communication system between the PC-side and the multi-rotor UAV. The combination of these three forms a multi-rotor UAV system that supports PC control.

[0044] Specifically, the content of the present invention includes the following three components:

[0045] (1) Multi-rotor unmanned aerial vehicle platform: build a multi-rotor unmanned aerial vehicle based on the existi...

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Abstract

The invention discloses a PC-control-supporting multi-rotor-wing unmanned-aerial-vehicle control system. A multi-rotor-wing unmanned-aerial-vehicle platform of the control system collects video information by constructing a multi-rotor-wing unmanned aerial vehicle; a PC-terminal ground control platform constructs a ground control platform at a PC terminal in a programming design mode to serve as a human-computer interaction interface for transmitting a control command to the multi-rotor-wing unmanned aerial vehicle; a PC-control-supporting multi-rotor-wing unmanned-aerial-vehicle communication system achieves the functions such as flight control command transmitting, flight state data transmitting and video returning data transmitting by carrying an ARM main control panel on the multi-rotor-wing unmanned aerial vehicle. By means of the PC-control-supporting multi-rotor-wing unmanned-aerial-vehicle control system, new control modes are expanded; meanwhile, the operative difficulty index is decreased, control accuracy is increased, the information collecting function and the information feedback function are expanded, the safety performance is improved, and the defects that present control based on a remote controller is high in operative difficulty index, inaccurate in control and indirect in information feedback are overcome.

Description

technical field [0001] The present invention relates to the technical field of aircraft communication control, in particular to a multi-rotor unmanned aerial vehicle control system supporting PC control, specifically to the communication system between PC and UAV, and the flight control technology and image return based on the communication system technology. Background technique [0002] Multi-rotor UAV is a flight platform composed of multiple sets of power systems. Compared with traditional aircraft, its unique structure and simple system architecture have obvious advantages: safety, low requirements for take-off and landing conditions, simple composition of mechanical components, and The machine is fully electronically stabilized. It can be widely used in agricultural medium and low-altitude sowing, spraying pesticides, public security monitoring, forest fire fighting, disaster monitoring, emergency communications, power applications, shipping applications, meteorologic...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B19/042G05D1/08
CPCG05B19/042G05D1/0808
Inventor 洪莹林楠方俊彬黄锐陈泽晗姚梓杰谢家璐陆潮东
Owner JINAN UNIVERSITY
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