CN202694152U

Movatterモバイル変換

Info

Publication number: CN202694152U
Application number: CN 201220234962
Authority: CN
Inventors: 方煜
Original assignee: XI'AN XIANGYU AVIATION TECHNOLOGY Co Ltd
Current assignee: XI'AN XIANGYU AVIATION TECHNOLOGY Co Ltd
Priority date: 2012-05-23
Filing date: 2012-05-23
Publication date: 2013-01-23
Anticipated expiration: 2022-05-23

Abstract

The utility model discloses an unmanned aerial vehicle control system, comprising at least one ground surface base station, wherein the ground surface base station comprises an unmanned aerial vehicle main control device, an aircraft switching device and a flying state display module, a data server and an emergency processing computer, wherein the unmanned aerial vehicle main control device is connected with the aircraft switching device and the data server; the data server is further connected with the emergency processing computer and the flying state display module; the flying state display module receives a state data packet sent by the data server and displays a corresponding aircraft state; the emergency processing computer stands by at any time; when an emergency condition happens, a corresponding serial port is converted to the emergency processing computer by serial port converting equipment and an emergency process control command is sent; and the ground surface base station is arranged on a mobile vehicle and can be used for monitoring telemetering data, planning a route and carrying out real-time fly control.

Description

Unmanned aerial vehicle control system

Technical field

The utility model relates to control field, is specifically related to unmanned aerial vehicle control system.

Background technology

Along with advancing by leaps and bounds of national economic development, monitoring is more and more important, duty cycle is shorter and shorter, existing miniature or Mini-Unmanned Aerial Vehicles still can not be finished dynamic emergency monitoring and periodic monitoring, main cause is to control the navigator fix of control system and the ground monitoring system of unmanned plane, program control navigation can not in time be fed back and transmission, can't practical requirement.

Summary of the invention

In order to overcome the shortcoming of above-mentioned prior art, the purpose of this utility model is unmanned aerial vehicle control system, can be used for the telemetry monitoring to unmanned plane, routeing, and real-time flight control.

To achieve these goals, the technical solution of the utility model is:

Unmanned aerial vehicle control system, comprise at least one ground base station is set, described ground base station comprises the unmanned plane master control set, aircraft switching device shifter and state of flight display module, data server, the emergency processing computing machine, described unmanned plane master control set links to each other with data server with the aircraft switching device shifter, described data server also connects client and state of flight display module, with the emergency processing computing machine that has the aircraft switching device shifter to link to each other, described emergency processing computing machine also is connected with the state of flight display module.

The state data packets that described state of flight display module receive data server sends, and show corresponding flight state.

Described emergency processing computing machine stands ready, and when being in an emergency, by the aircraft switching device shifter corresponding serial ports is switched to the emergency processing computing machine, sends the emergency processing control command.

Described ground base station is arranged on the moving vehicle.

Described aircraft serial data is as data source, and the flow direction by aircraft switching device shifter control data source when case of emergency appears in certain unmanned plane, switches to the emergency processing computing machine and carries out emergency processing; Under the normal flight state, data server receives the aircraft serial data, and sends data by network to the client that has connected.

The beneficial effects of the utility model:

This system has adopted advanced aerial networking mode, utilizes two frequencies simultaneously aerial aircraft to be controlled, and can be mainly used in the telemetry monitoring to unmanned plane, routeing, and real-time flight control.

Described control system works in two states: unmanned plane master mode and state of flight pattern.

Described unmanned plane master mode mainly is to carry out the real-time control of routeing, aerial mission, and the state of flight pattern mainly is state of flight and the information warning that shows unmanned plane by display.

Description of drawings

Fig. 1 is fundamental diagram of the present utility model.

Embodiment

Below in conjunction with the drawings and specific embodiments the utility model is elaborated.

With reference to accompanying drawing, unmanned aerial vehicle control system, comprise at least one ground base station is set, described ground base station comprises the unmanned plane master control set, aircraft switching device shifter and state of flight display module, data server, the emergency processing computing machine, described unmanned plane master control set links to each other with data server with the aircraft switching device shifter, described data server also connects client and state of flight display module, with the emergency processing computing machine that has the aircraft switching device shifter to link to each other, described emergency processing computing machine also is connected with the state of flight display module.

The state data packets that described state of flight display module receive data server sends, and show corresponding flight state, can specify when needing to switch to corresponding aircraft, thereby control the state of a plurality of aircraft.

Described ground base station is arranged on the moving vehicle.

Described aircraft switching device shifter switches to the current selected aircraft, shows the flight planning of current selected aircraft, and can change this flight planning, and other each flight plan do not show, the aircraft sign show corresponding state of flight (air speed, highly); And aerial mission controlled in real time;

The state data packets that described state of flight display module receive data server sends, and show corresponding flight state; Show and comprise aircraft electrical origin system parameter; Flight attitude (level meter and numerical value); Speed, highly (scale and numerical value); GPS information; The flight state indication; The transmitter state shows.

Claims

1. unmanned aerial vehicle control system, comprise at least one ground base station is set, described ground base station comprises the unmanned plane master control set, aircraft switching device shifter and state of flight display module, data server, the emergency processing computing machine, described unmanned plane master control set links to each other with data server with the aircraft switching device shifter, described data server also connects client and state of flight display module, with the emergency processing computing machine that has the aircraft switching device shifter to link to each other, described emergency processing computing machine also is connected with the state of flight display module.

2. unmanned aerial vehicle control system according to claim 1, it is characterized in that, the state data packets that described state of flight display module receive data server sends, and show corresponding flight state, can specify when needing and switch to corresponding aircraft, thereby show the state of a plurality of aircraft.

3. unmanned aerial vehicle control system according to claim 1, it is characterized in that described emergency processing computing machine stands ready, when being in an emergency, by the aircraft switching device shifter corresponding serial ports is switched to the emergency processing computing machine, send the emergency processing control command.

4. unmanned aerial vehicle control system according to claim 1 is characterized in that, described ground base station is arranged on the moving vehicle.