CN202694152U - Unmanned aerial vehicle control system - Google Patents
Unmanned aerial vehicle control system Download PDFInfo
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- 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
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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
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.
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CN 201220234962 CN202694152U (en) | 2012-05-23 | 2012-05-23 | Unmanned aerial vehicle control system |
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CN 201220234962 CN202694152U (en) | 2012-05-23 | 2012-05-23 | Unmanned aerial vehicle control system |
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Cited By (13)
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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 |
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2012
- 2012-05-23 CN CN 201220234962 patent/CN202694152U/en not_active Expired - Lifetime
Cited By (24)
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 |
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