CN112363540A - Remote unmanned aerial vehicle operating system - Google Patents
Remote unmanned aerial vehicle operating system Download PDFInfo
- Publication number
- CN112363540A CN112363540A CN202011408312.8A CN202011408312A CN112363540A CN 112363540 A CN112363540 A CN 112363540A CN 202011408312 A CN202011408312 A CN 202011408312A CN 112363540 A CN112363540 A CN 112363540A
- Authority
- CN
- China
- Prior art keywords
- unmanned aerial
- module
- aerial vehicle
- processing unit
- central processing
- 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.)
- Pending
Links
Images
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/12—Target-seeking control
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
- G01S19/39—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/42—Determining position
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N23/00—Cameras or camera modules comprising electronic image sensors; Control thereof
- H04N23/50—Constructional details
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N7/00—Television systems
- H04N7/18—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast
Abstract
The invention relates to the technical field of unmanned aerial vehicles, in particular to a remote unmanned aerial vehicle operating system, which comprises a control room of a tower, wherein the control room of the tower is connected with an unmanned aerial vehicle; unmanned aerial vehicle is including: the system comprises a GPS positioning system, a video monitoring system, a take-off and landing control system, an electric power monitoring system, an emergency alarm system, a central processing unit and an automatic driving system. The unmanned aerial vehicle has the advantages that the unmanned aerial vehicle has stronger search and rescue functions on people, and the lives of people are further guaranteed.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to a remote unmanned aerial vehicle operating system.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer.
In order to be able to perfect a better unmanned aerial vehicle control system, a remote unmanned aerial vehicle operation system is provided for this purpose.
Disclosure of Invention
In view of the above problems in the prior art, an aspect of the present invention is to provide a remote drone operating system.
In order to achieve the purpose, the remote unmanned aerial vehicle operating system provided by the invention comprises a control room of a tower, wherein the control room of the tower is connected with an unmanned aerial vehicle; unmanned aerial vehicle is including: the system comprises a GPS positioning system, a video monitoring system, a take-off and landing control system, an electric power monitoring system, an emergency alarm system, a central processing unit and an automatic driving system; central processing unit is connected with GPS positioning system for receive information and transmission, central processing unit is connected with video monitor system for information processing and transmission, central processing unit is connected with the control system that takes off and land for the instruction of receiving institute, central processing unit is connected with electric power monitored control system for self-checking self electric quantity condition and transmission, central processing unit is connected with emergent alarm system for with self information processing transmission usefulness, central processing unit is connected with autopilot system for receive information, and control operation is used.
Preferably, the GPS positioning system includes: the rescue system comprises a rescue module, a distress signal receiving module and a signal enhancement module, wherein a GPS positioning system is connected with the rescue module, the GPS positioning system is connected with the distress signal receiving module, and the GPS positioning system is connected with the signal enhancement module.
Preferably, the emergency alarm system comprises: the emergency alarm system is connected with the fault detection module, and is connected with the obstacle identification module.
Preferably, the take-off and landing control system comprises: the launching and landing control system is connected with the launching and landing module.
Preferably, the power monitoring system includes: the power monitoring system is connected with the power detection module and the power monitoring system is connected with the power failure module. Preferably, the video monitoring system includes: the video monitoring system is connected with the image storage module, the video monitoring system is connected with the image acquisition module, and the video monitoring system is connected with the image identification module.
Compared with the prior art, the remote unmanned aerial vehicle operating system provided by the invention has the following beneficial effects:
the invention can better perfect the underground garage system, when in use, the unmanned aerial vehicle is taken out and started through the control room of the tower, then the emergency alarm system is used for self-checking to see whether the self condition of the unmanned aerial vehicle is normal, if all the conditions are normal, the unmanned aerial vehicle can be used, before the system is used, the system is firstly bound with the identity of a person on a trip task through the mobile client carried at any time and the unmanned aerial vehicle, then an independent signal channel can be established, the stability of the channel is improved through the signal enhancement module, after the person is in an emergency, the system can send a distress signal to the unmanned aerial vehicle through the mobile client carried at any time and process the signal to the central processing unit through the GPS positioning system, then the signal is transmitted to the control room of the tower through the unmanned aerial vehicle, after the control room of the tower obtains the distress signal, the unmanned aerial vehicle after the safety self-checking is controlled to start to the dangerous, make unmanned aerial vehicle accomplish descending that can be fine after the task, unmanned aerial vehicle can carry out the scope search through video detection system at the flight process, can discern the back and gather the control data of rescue through image recognition module, saves again, then flies back to the pylon to carry out personnel's position through the pylon control room and confirm, do rescue on next step again.
Drawings
Fig. 1 is a schematic structural diagram of an operating system of a remote unmanned aerial vehicle according to the present invention;
fig. 2 is a schematic structural diagram of an unmanned aerial vehicle in a remote unmanned aerial vehicle operating system according to the present invention;
fig. 3 is a schematic structural diagram of a video monitoring system in a remote unmanned aerial vehicle operating system according to the present invention.
Fig. 4 is a schematic structural diagram of a take-off and landing control system in a remote unmanned aerial vehicle operating system according to the present invention.
Fig. 5 is a schematic structural diagram of a cable monitoring system in a remote drone operating system according to the present invention.
Fig. 6 is a schematic structural diagram of an emergency alarm system in a remote unmanned aerial vehicle operating system according to the present invention.
Fig. 7 is a schematic structural diagram of a GPS positioning system in a remote drone operating system according to the present invention.
Fig. 8 is a schematic structural diagram of a control room of a tower in a remote unmanned aerial vehicle operating system according to the present invention.
Detailed Description
In order to make the objects, technical solutions and advantages of the embodiments of the present disclosure more clear, the technical solutions of the embodiments of the present disclosure will be described below clearly and completely with reference to the accompanying drawings of the embodiments of the present disclosure.
Referring to fig. 1-8, a remote unmanned aerial vehicle operating system includes a control tower room, which is connected with an unmanned aerial vehicle for information transmission; unmanned aerial vehicle is including: the system comprises a GPS positioning system, a video monitoring system, a take-off and landing control system, an electric power monitoring system, an emergency alarm system, a central processing unit and an automatic driving system; central processing unit is connected with GPS positioning system for receive information and transmission, central processing unit is connected with video monitor system for information processing and transmission, central processing unit is connected with the control system that takes off and land for the instruction of receiving institute, central processing unit is connected with electric power monitored control system for self-checking self electric quantity condition and transmission, central processing unit is connected with emergent alarm system for with self information processing transmission usefulness, central processing unit is connected with autopilot system for receive information, and control operation is used.
In an alternative embodiment, the GPS positioning system comprises: the rescue system comprises a rescue module, a distress signal receiving module and a signal enhancement module, wherein a GPS positioning system is connected with the rescue module, the GPS positioning system is connected with the distress signal receiving module, the GPS positioning system is connected with the signal enhancement module, people bind with the unmanned aerial vehicle through a mobile client side and then take place in emergency again, when no GPS is used for positioning, a unique signal channel is arranged between the unmanned aerial vehicle and the client side, and a distress signal is sent through personnel and then is positioned for help.
In an alternative embodiment, the emergency alert system includes: stabilize detection module, fault detection module and obstacle identification module, emergency alarm system is connected with stable detection module, emergency alarm system is connected with the fault detection module, emergency alarm system is connected with obstacle identification module, and the equipment self-checking of being convenient for prevents that unmanned aerial vehicle from breaking down.
In an optional embodiment, the take-off and landing control system comprises: the launching and landing control system is connected with the launching and landing module, so that the unmanned aerial vehicle can take off and land conveniently, and the unmanned aerial vehicle is prevented from failing to take off or land due to the fact that the unmanned aerial vehicle does not have a systematic taking off and landing system.
In an optional embodiment, the power monitoring system comprises: electric quantity detection module and outage module, electric power monitored control system is connected with electric quantity detection module, electric power monitored control system is connected with the outage module, and the people of being convenient for monitor unmanned aerial vehicle electric quantity state prevents that the electric quantity from not recalling inadequately, leads to unmanned aerial vehicle to damage. In an alternative embodiment, the video surveillance system includes: the video monitoring system is connected with the image acquisition module, the video monitoring system is connected with the image identification module, the unmanned aerial vehicle is convenient to record data and bring back when going out a task, and people can clearly know the situation at that time.
When the unmanned aerial vehicle emergency signal transmission system is used, the unmanned aerial vehicle is taken out and started through the control room of the tower, then self-checking is carried out through the emergency alarm system to see whether the self condition of the unmanned aerial vehicle is normal or not, the unmanned aerial vehicle can be used after all the conditions are normal, before the unmanned aerial vehicle is used, the unmanned aerial vehicle is firstly bound with a person on a trip task through a mobile client carried at any time and then an independent signal channel can be established, the stability of the channel is improved through the signal enhancement module, after the person is in an emergency condition, the person can send a distress signal to the unmanned aerial vehicle through the mobile client carried at any time, the distress signal is processed to the central processing unit through the GPS positioning system and then is transmitted to the control room of the tower through the unmanned aerial vehicle, after the help signal is obtained by the control room of the unmanned aerial vehicle after the safety self-checking, the unmanned aerial vehicle is required, unmanned aerial vehicle can carry out the scope search through video detection system at the flight process, can pass through the image recognition module with the control data of rescue and discern the back and gather, save again, then fly back to the pylon to carry out personnel's position through the control room of pylon and confirm, do rescue on next step again.
The above description is only an exemplary embodiment of the present invention, and is not intended to limit the present invention, the scope of which is defined by the claims. Various modifications and equivalents may be made by those skilled in the art within the spirit and scope of the present invention, and such modifications and equivalents should also be considered as falling within the scope of the present invention.
Claims (6)
1. The utility model provides a long-range unmanned aerial vehicle operating system, includes the control room of tower, its characterized in that: the control room of the tower is connected with an unmanned aerial vehicle;
unmanned aerial vehicle is including: the system comprises a GPS positioning system, a video monitoring system, a take-off and landing control system, an electric power monitoring system, an emergency alarm system, a central processing unit and an automatic driving system;
central processing unit is connected with GPS positioning system for receive information and transmission, central processing unit is connected with video monitor system for information processing and transmission, central processing unit is connected with the control system that takes off and land for the instruction of receiving institute, central processing unit is connected with electric power monitored control system for self-checking self electric quantity condition and transmission, central processing unit is connected with emergent alarm system for with self information processing transmission usefulness, central processing unit is connected with autopilot system for receive information, and control operation is used.
2. The remote drone operating system of claim 1, wherein: the GPS positioning system comprises: the rescue system comprises a rescue module, a distress signal receiving module and a signal enhancement module, wherein a GPS positioning system is connected with the rescue module, the GPS positioning system is connected with the distress signal receiving module, and the GPS positioning system is connected with the signal enhancement module.
3. The remote drone operating system of claim 1, wherein: the emergency alarm system comprises: the emergency alarm system is connected with the fault detection module, and is connected with the obstacle identification module.
4. The remote drone operating system of claim 1, wherein: the take-off and landing control system comprises: the launching and landing control system is connected with the launching and landing module.
5. The remote drone operating system of claim 1, wherein: the power monitoring system comprises: the power monitoring system is connected with the power detection module and the power monitoring system is connected with the power failure module.
6. The remote drone operating system of claim 1, wherein: the video monitoring system comprises: the video monitoring system is connected with the image storage module, the video monitoring system is connected with the image acquisition module, and the video monitoring system is connected with the image identification module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011408312.8A CN112363540A (en) | 2020-12-05 | 2020-12-05 | Remote unmanned aerial vehicle operating system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011408312.8A CN112363540A (en) | 2020-12-05 | 2020-12-05 | Remote unmanned aerial vehicle operating system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN112363540A true CN112363540A (en) | 2021-02-12 |
Family
ID=74535977
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202011408312.8A Pending CN112363540A (en) | 2020-12-05 | 2020-12-05 | Remote unmanned aerial vehicle operating system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN112363540A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104700576A (en) * | 2015-03-27 | 2015-06-10 | 徐州飞梦电子科技有限公司 | Quick water rescuing system and method |
| KR20170106533A (en) * | 2016-03-10 | 2017-09-21 | 만진항공건설 주식회사 | Rescue tube apparatus using unmanned aerial vehicle |
| CN206926823U (en) * | 2017-07-25 | 2018-01-26 | 武汉大学 | A kind of multi-functional unmanned plane device searched and rescued for field |
| CN107656545A (en) * | 2017-09-12 | 2018-02-02 | 武汉大学 | A kind of automatic obstacle avoiding searched and rescued towards unmanned plane field and air navigation aid |
| CN109358653A (en) * | 2018-09-03 | 2019-02-19 | 济源维恩科技开发有限公司 | Marine unmanned plane distributed intelligence search and rescue system |
| CN111431591A (en) * | 2020-05-26 | 2020-07-17 | 南京森林警察学院 | All-weather intelligent flight system of unmanned aerial vehicle |
-
2020
- 2020-12-05 CN CN202011408312.8A patent/CN112363540A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104700576A (en) * | 2015-03-27 | 2015-06-10 | 徐州飞梦电子科技有限公司 | Quick water rescuing system and method |
| KR20170106533A (en) * | 2016-03-10 | 2017-09-21 | 만진항공건설 주식회사 | Rescue tube apparatus using unmanned aerial vehicle |
| CN206926823U (en) * | 2017-07-25 | 2018-01-26 | 武汉大学 | A kind of multi-functional unmanned plane device searched and rescued for field |
| CN107656545A (en) * | 2017-09-12 | 2018-02-02 | 武汉大学 | A kind of automatic obstacle avoiding searched and rescued towards unmanned plane field and air navigation aid |
| CN109358653A (en) * | 2018-09-03 | 2019-02-19 | 济源维恩科技开发有限公司 | Marine unmanned plane distributed intelligence search and rescue system |
| CN111431591A (en) * | 2020-05-26 | 2020-07-17 | 南京森林警察学院 | All-weather intelligent flight system of unmanned aerial vehicle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN107074375B (en) | Fail-safe aircraft monitoring and tracking | |
| CN110071754B (en) | UAV measurement and control link interruption fault emergency processing method | |
| CN106919184B (en) | Double-unmanned-aerial-vehicle cooperative operation system and double-unmanned-aerial-vehicle cooperative operation method | |
| CN113156999B (en) | Cluster formation airplane abnormal fault level processing method, system and application | |
| US10988251B2 (en) | On-board emergency response system for a vehicle | |
| CN114531194A (en) | Wireless communication method and device, unmanned aerial vehicle and unmanned aerial vehicle control system | |
| CN110955260A (en) | Intelligent scheduling system and method for portable emergency medical equipment | |
| CN206515670U (en) | A kind of unmanned plane cloud monitoring system with black box function | |
| KR20150146040A (en) | Unmanned aerial vehicles for body-guard service | |
| CN106325300A (en) | Remote condition monitoring and controlling system of unmanned aerial vehicle based on GSM-4G communication | |
| CN112650279B (en) | Cloud flight management system and cloud flight management method for airplane | |
| EP3757708B1 (en) | Method and apparatus for using drone on moving object | |
| CN106774358A (en) | Unmanned plane intelligent battery and its control method, device and unmanned plane | |
| CN110621579A (en) | Multi-battery power supply control method and device and unmanned aerial vehicle | |
| US11869371B2 (en) | Unmanned aerial vehicle traffic management apparatus, takeoff and landing facility management apparatus, unmanned aerial vehicle traffic management method, and unmanned aerial vehicle system | |
| CN111580559A (en) | Loss prevention method and control system for unmanned aerial vehicle | |
| CN109477891A (en) | Unmanned plane detection method and detecting devices, the control method of server and server | |
| CN110660207A (en) | Remote control terminal system and monitoring method of remote control terminal | |
| CN112363540A (en) | Remote unmanned aerial vehicle operating system | |
| CN114694421B (en) | Low-altitude air pipe system based on digital chart | |
| CN110908406A (en) | Positioning device and method suitable for unmanned aerial vehicle falling | |
| CN102514717B (en) | Unmanned aerial vehicle recycling method and device | |
| KR20160074297A (en) | Method for Tracing and Recovering Crashed Multirotor Body | |
| JP6932456B2 (en) | Unmanned aerial vehicle and battery cartridge | |
| CN111506103A (en) | Unmanned aerial vehicle control system and forced landing method |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20210212 |