CN202694152U - Unmanned aerial vehicle control system - Google Patents

Unmanned aerial vehicle control system Download PDF

Info

Publication number
CN202694152U
CN202694152U CN 201220234962 CN201220234962U CN202694152U CN 202694152 U CN202694152 U CN 202694152U CN 201220234962 CN201220234962 CN 201220234962 CN 201220234962 U CN201220234962 U CN 201220234962U CN 202694152 U CN202694152 U CN 202694152U
Authority
CN
China
Prior art keywords
state
emergency processing
aircraft
aerial vehicle
unmanned aerial
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
CN 201220234962
Other languages
Chinese (zh)
Inventor
方煜
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
XI'AN XIANGYU AVIATION TECHNOLOGY Co Ltd
Original Assignee
XI'AN XIANGYU AVIATION TECHNOLOGY Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by XI'AN XIANGYU AVIATION TECHNOLOGY Co Ltd filed Critical XI'AN XIANGYU AVIATION TECHNOLOGY Co Ltd
Priority to CN 201220234962 priority Critical patent/CN202694152U/en
Application granted granted Critical
Publication of CN202694152U publication Critical patent/CN202694152U/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Landscapes

  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

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 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 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 (4)

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.
CN 201220234962 2012-05-23 2012-05-23 Unmanned aerial vehicle control system Expired - Lifetime CN202694152U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201220234962 CN202694152U (en) 2012-05-23 2012-05-23 Unmanned aerial vehicle control system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201220234962 CN202694152U (en) 2012-05-23 2012-05-23 Unmanned aerial vehicle control system

Publications (1)

Publication Number Publication Date
CN202694152U true CN202694152U (en) 2013-01-23

Family

ID=47549740

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201220234962 Expired - Lifetime CN202694152U (en) 2012-05-23 2012-05-23 Unmanned aerial vehicle control system

Country Status (1)

Country Link
CN (1) CN202694152U (en)

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103974327A (en) * 2014-04-28 2014-08-06 华南理工大学 Small-size unmanned helicopter point-to-point data chain system and achieving method
CN104570872A (en) * 2015-01-07 2015-04-29 厦门翼正航空科技有限公司 Unmanned plane remoter monitoring and controlling method
CN104571131A (en) * 2015-01-20 2015-04-29 西安电子科技大学宁波信息技术研究院 Unmanned aerial vehicle formation distributed collaboration system and anti-interference method thereof
CN104615143A (en) * 2015-01-23 2015-05-13 广州快飞计算机科技有限公司 Unmanned aerial vehicle scheduling method
CN105573335A (en) * 2016-03-18 2016-05-11 王正作 Unmanned-plane aerial photography control system
CN105700545A (en) * 2015-11-05 2016-06-22 赵子滨 UAV scheduling method based on UAV automation platform
WO2016154949A1 (en) * 2015-03-31 2016-10-06 SZ DJI Technology Co., Ltd. Authentication systems and methods for generating flight regulations
CN106102110A (en) * 2016-06-21 2016-11-09 北京小米移动软件有限公司 The method of switching control power and control terminal
CN107209489A (en) * 2015-12-10 2017-09-26 深圳市大疆创新科技有限公司 Unmanned plane and its method for monitoring state, condition monitoring system, state monitoring device
CN111766895A (en) * 2020-05-29 2020-10-13 苏州云思翼电子科技有限公司 Unmanned aerial vehicle inspection system and method for photovoltaic power station
CN111831487A (en) * 2019-04-15 2020-10-27 丰鸟航空科技有限公司 Data source output method, device, system and storage medium
CN112214030A (en) * 2020-09-11 2021-01-12 中国航空工业集团公司成都飞机设计研究所 One-station-control dual-computer display control method for unmanned aerial vehicle
US11094202B2 (en) 2015-03-31 2021-08-17 SZ DJI Technology Co., Ltd. Systems and methods for geo-fencing device communications

Cited By (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103974327A (en) * 2014-04-28 2014-08-06 华南理工大学 Small-size unmanned helicopter point-to-point data chain system and achieving method
CN104570872A (en) * 2015-01-07 2015-04-29 厦门翼正航空科技有限公司 Unmanned plane remoter monitoring and controlling method
CN104571131A (en) * 2015-01-20 2015-04-29 西安电子科技大学宁波信息技术研究院 Unmanned aerial vehicle formation distributed collaboration system and anti-interference method thereof
CN104615143B (en) * 2015-01-23 2017-05-24 广州快飞计算机科技有限公司 Unmanned aerial vehicle scheduling method
CN104615143A (en) * 2015-01-23 2015-05-13 广州快飞计算机科技有限公司 Unmanned aerial vehicle scheduling method
US9805372B2 (en) 2015-03-31 2017-10-31 SZ DJI Technology Co., Ltd Authentication systems and methods for generating flight regulations
US11094202B2 (en) 2015-03-31 2021-08-17 SZ DJI Technology Co., Ltd. Systems and methods for geo-fencing device communications
US11961093B2 (en) 2015-03-31 2024-04-16 SZ DJI Technology Co., Ltd. Authentication systems and methods for generating flight regulations
US9792613B2 (en) 2015-03-31 2017-10-17 SZ DJI Technology Co., Ltd Authentication systems and methods for generating flight regulations
US9805607B2 (en) 2015-03-31 2017-10-31 SZ DJI Technology Co., Ltd. Authentication systems and methods for generating flight regulations
US9870566B2 (en) 2015-03-31 2018-01-16 SZ DJI Technology Co., Ltd Authentication systems and methods for generating flight regulations
WO2016154949A1 (en) * 2015-03-31 2016-10-06 SZ DJI Technology Co., Ltd. Authentication systems and methods for generating flight regulations
US11367081B2 (en) 2015-03-31 2022-06-21 SZ DJI Technology Co., Ltd. Authentication systems and methods for generating flight regulations
US11120456B2 (en) 2015-03-31 2021-09-14 SZ DJI Technology Co., Ltd. Authentication systems and methods for generating flight regulations
CN105700545A (en) * 2015-11-05 2016-06-22 赵子滨 UAV scheduling method based on UAV automation platform
CN107209489A (en) * 2015-12-10 2017-09-26 深圳市大疆创新科技有限公司 Unmanned plane and its method for monitoring state, condition monitoring system, state monitoring device
CN107209489B (en) * 2015-12-10 2019-07-09 深圳市大疆创新科技有限公司 Unmanned plane and its method for monitoring state, condition monitoring system, state monitoring device
CN105573335A (en) * 2016-03-18 2016-05-11 王正作 Unmanned-plane aerial photography control system
US10134269B2 (en) 2016-06-21 2018-11-20 Beijing Xiaomi Mobile Software Co., Ltd. Control switching method and control terminal, and storage medium
CN106102110A (en) * 2016-06-21 2016-11-09 北京小米移动软件有限公司 The method of switching control power and control terminal
CN111831487A (en) * 2019-04-15 2020-10-27 丰鸟航空科技有限公司 Data source output method, device, system and storage medium
CN111766895A (en) * 2020-05-29 2020-10-13 苏州云思翼电子科技有限公司 Unmanned aerial vehicle inspection system and method for photovoltaic power station
CN112214030A (en) * 2020-09-11 2021-01-12 中国航空工业集团公司成都飞机设计研究所 One-station-control dual-computer display control method for unmanned aerial vehicle
CN112214030B (en) * 2020-09-11 2023-03-14 中国航空工业集团公司成都飞机设计研究所 One-station-control dual-computer display control method for unmanned aerial vehicle

Similar Documents

Publication Publication Date Title
CN202694152U (en) Unmanned aerial vehicle control system
CN202093395U (en) Earth station remote control device for unmanned vehicle
CN201000576Y (en) Flight control system for unmanned plane
CN103714719B (en) Based on the Flight navigational system of Beidou satellite navigation
CN105551287B (en) Dispatch system in airport station level ground
CN202533754U (en) Ground monitoring system for unmanned vehicle physical simulated test platform
CN110166535B (en) Intelligent traffic communication system
CN204595221U (en) A kind of common aero vehicle airborne communication navigational system
CN202282078U (en) Airplane flight real time control system
CN105573336A (en) Portable ground station capable of supporting multiple unmanned aerial vehicles
CN105676249A (en) Navigation airplane communication navigation monitoring system and method based on 4G/3G/BDS
CN206515700U (en) A kind of UAV Flight Control System based on smart mobile phone
CN205050404U (en) Flight simulation training system based on model airplane
CN204669614U (en) A kind ofly to be connected based on iBeacon the system that mobile phone applies with unmanned air vehicle technique
CN109496303A (en) The methods of exhibiting and device and unmanned plane monitoring system of monitored data
CN106470141A (en) A kind of dynamo-electric method for interchanging data based on GJB289A bus
KR101082874B1 (en) Multi-flight simulation system
CN202226055U (en) Dual-autopilot flight controller for unmanned aerial vehicle
CN207191460U (en) A kind of portable intelligent Airborne Terminal and aircraft
CN203759493U (en) Integration monitoring system based on AFDX bus
CN205384745U (en) Airport station level ground dispatch system and on -vehicle positioner
RU2014150021A (en) DEVICE AND METHOD FOR FACILITATING RECONFIGURATION OF AIRCRAFT, AIRCRAFT INCLUDING SUCH DEVICE, AND RELATED COMPUTER SOFTWARE
CN112634662A (en) Electronic fence, control system, method, medium, unmanned aerial vehicle formation and terminal
CN102142913B (en) Aviation channel simulator and simulation method
CN202231751U (en) Complicated electromagnetic environment simulation platform achieving distributed simulation parameter acquisition

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CX01 Expiry of patent term

Granted publication date: 20130123

CX01 Expiry of patent term