CN107450395A - Unmanned plane Information locating acquisition control system - Google Patents

Unmanned plane Information locating acquisition control system Download PDF

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Publication number
CN107450395A
CN107450395A CN201710697781.8A CN201710697781A CN107450395A CN 107450395 A CN107450395 A CN 107450395A CN 201710697781 A CN201710697781 A CN 201710697781A CN 107450395 A CN107450395 A CN 107450395A
Authority
CN
China
Prior art keywords
unmanned plane
information
dsp processor
control system
processing system
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
Application number
CN201710697781.8A
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Chinese (zh)
Inventor
张兵
卫军
李建平
马俪齐
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.)
Jiangsu Crossing Point Information Polytron Technologies Inc
Original Assignee
Jiangsu Crossing Point Information Polytron Technologies Inc
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 Jiangsu Crossing Point Information Polytron Technologies Inc filed Critical Jiangsu Crossing Point Information Polytron Technologies Inc
Priority to CN201710697781.8A priority Critical patent/CN107450395A/en
Publication of CN107450395A publication Critical patent/CN107450395A/en
Pending legal-status Critical Current

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Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05BCONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B19/00Programme-control systems
    • G05B19/02Programme-control systems electric
    • G05B19/04Programme control other than numerical control, i.e. in sequence controllers or logic controllers
    • G05B19/042Programme control other than numerical control, i.e. in sequence controllers or logic controllers using digital processors
    • G05B19/0423Input/output
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05BCONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B2219/00Program-control systems
    • G05B2219/20Pc systems
    • G05B2219/25Pc structure of the system
    • G05B2219/25257Microcontroller

Abstract

The invention discloses a kind of unmanned plane Information locating acquisition control system.It includes being powered DSP Processor by power module, the vehicle-mounted GPS equipment being connected with in-vehicle processor;DSP Processor connects inertial sensor respectively, pressure-altitude sensor and electron speed regulator, the motor connection of electron speed regulator and unmanned plane, in-vehicle processor connects with DSP Processor communication, DSP Processor is connected by the information processing system of data radio station and overall control center, information processing system can make to shoot scene to density center and by video camera in the unmanned plane during flying nearest apart from density center according to the data message received, the reason for information processing system that the image information of shooting can be fed directly to overall control center by the DSP Processor carries out judgement high density state.After above-mentioned structure, its is reasonable in design, and communication transfer speed block, judged result is accurate, greatlys save human resources.

Description

Unmanned plane Information locating acquisition control system
Technical field
The present invention relates to a kind of unmanned aerial vehicle control system, specifically a kind of unmanned plane Information locating acquisition control system System.
Background technology
With the development of society, people to urban area bus routes planning carry out effectively analysis have become one it is important Task, it is that following each big city solves the grand strategy of city route planning, prior art by the way that various data are carried out with analysis In, some modes for manually counting of generally use are to various data(Such as the analysis to current traffic)Collected then It is compared, such as planning is predicted to traffic data by comparison result, existing this mode is relatively backward, single, Need to expend a large amount of manpower and materials and the degree of accuracy is inadequate.
The content of the invention
The technical problem to be solved in the present invention is to provide a kind of communication speed is fast, analysis result is accurate and it is few to expend resource Unmanned plane Information locating acquisition control system.
In order to solve the above-mentioned technical problem, unmanned plane Information locating acquisition control system of the invention, including installed in each Being powered DSP Processor by power module in frame unmanned plane, the car being connected with in-vehicle processor in each bus Carry GPS device;DSP Processor connects inertial sensor, pressure-altitude sensor and electron speed regulator, electron speed regulator respectively With that the motor connection of unmanned plane and can control the speed of unmanned plane motor, in-vehicle processor passes through wireless communication networks and DSP Processor communication connects and location information can be transferred to DSP Processor, and DSP Processor passes through data radio station and overall control center Information processing system connection and can according to the location information of vehicle-mounted GPS equipment analyze judge bus high density state and general Information processing system of the data information transfer to overall control center, the information processing system of overall control center can be according to the number received It is believed that breath makes to shoot scene to density center and by video camera in the unmanned plane during flying nearest apart from density center, The DSP Processor image information of shooting can be fed directly to overall control center information processing system judge it is intensive The reason for state.
The display terminal for display information being connected with information processing system is additionally provided with the overall control center.
Described information processing system is connected with operation control system by input equipment interface and can inputted from input The operational order of operation control system.
The inertial sensor includes three-axis gyroscope, three axis accelerometer, three axle magnetic compasses and the GPS/ Big Dippeves and received Machine.
The inertial sensor is MEMS sensor.
After above-mentioned structure, by carrying out positioning candid photograph, master control to bus dense degree with reference to unmanned air vehicle technique Center can be counted according to the degree of crowding in certain time, and field personnel checks this time according to statistical information The photo of interior candid photograph, be that personnel's flow is excessive according to the degree of crowding for capturing validation of information scene or other forms vehicle in itself It is crowded in addition be whether accidental burst road conditions thereby determined that whether need to bus exercise route planned again, Its is reasonable in design, and communication transfer speed block, judged result is accurate, greatlys save human resources.
Brief description of the drawings
Fig. 1 is the theory diagram of unmanned plane Information locating acquisition control system of the present invention.
Embodiment
With reference to the accompanying drawings and detailed description, the unmanned plane Information locating acquisition control system of the present invention is made into one Step describes in detail.
As illustrated, the unmanned plane Information locating acquisition control system of the present invention, including in each frame unmanned plane Powered DSP Processor by power module, the vehicle-mounted GPS equipment being connected with in-vehicle processor in each bus;DSP Processor connects inertial sensor, pressure-altitude sensor and electron speed regulator respectively, it is certainly essential also include by The motor connection of video camera, electron speed regulator and unmanned plane and the speed that can control unmanned plane motor, vehicle-mounted GPS equipment can Bus position is transferred to in-vehicle processor, in-vehicle processor connects by wireless communication networks and DSP Processor communication Connect and location information can be transferred to DSP Processor, thus improve positioning accuracy, DSP Processor by data radio station with The information processing system connection of overall control center simultaneously can judge the intensive of bus according to the analysis of the location information of vehicle-mounted GPS equipment State and by information processing system of the data information transfer to overall control center, the information processing system of overall control center can be according to connecing The data message received makes in the unmanned plane during flying nearest apart from density center to density center and by video camera to scene Shot, wherein, due to the monitoring range of unmanned plane be it is limited, therefore, in actual use, while multi rack of going on a journey Unmanned plane and every frame unmanned plane are responsible for different scopes, and the image information of shooting can be fed directly to always by DSP Processor The information processing system at control center carries out the reason for judgement high density state.
Wherein, it is whole that the display for display information being connected with information processing system is additionally provided with described overall control center End, described information processing system are connected with operation control system by input equipment interface and can inputted from input operation The operational order of control system, described inertial sensor include three-axis gyroscope, three axis accelerometer, three axle magnetic compasses and GPS/ Beidou receivers, described inertial sensor are MEMS sensor.

Claims (5)

  1. A kind of 1. unmanned plane information gathering transmission control system, it is characterised in that:Including in each frame unmanned plane by electricity Source module power supply DSP Processor, the vehicle-mounted GPS equipment being connected with in-vehicle processor in each bus;The DSP Processor connects inertial sensor, pressure-altitude sensor and electron speed regulator, the electron speed regulator and unmanned plane respectively Motor connection and the speed of unmanned plane motor can be controlled, the in-vehicle processor is by wireless communication networks and DSP processing Device communication connects and location information can be transferred to DSP Processor, and the DSP Processor passes through data radio station and overall control center Information processing system connection and can according to the location information of vehicle-mounted GPS equipment analyze judge bus high density state and general Information processing system of the data information transfer to overall control center, the information processing system of the overall control center can be according to receiving Data message make in the unmanned plane during flying nearest apart from density center to density center and by video camera to scene progress Shooting, the information processing system that the image information of shooting can be fed directly to overall control center by the DSP Processor are sentenced The reason for disconnected high density state.
  2. 2. according to the unmanned plane information gathering transmission control system described in claim 1, it is characterised in that:In the overall control center It is additionally provided with the display terminal for display information being connected with information processing system.
  3. 3. according to the unmanned plane information gathering transmission control system described in claim 1 or 2, it is characterised in that:At described information Reason system is connected with operation control system by input equipment interface and can input the operation from input operation control system Instruction.
  4. 4. according to described in claim 3 according to the unmanned plane information gathering transmission control system described in claim 1, its feature It is:The inertial sensor includes three-axis gyroscope, three axis accelerometer, three axle magnetic compasses and GPS/ Beidou receivers.
  5. 5. according to described in claim 4 according to the unmanned plane information gathering transmission control system described in claim 1, its feature It is:The inertial sensor is MEMS sensor.
CN201710697781.8A 2017-08-15 2017-08-15 Unmanned plane Information locating acquisition control system Pending CN107450395A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710697781.8A CN107450395A (en) 2017-08-15 2017-08-15 Unmanned plane Information locating acquisition control system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710697781.8A CN107450395A (en) 2017-08-15 2017-08-15 Unmanned plane Information locating acquisition control system

Publications (1)

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CN107450395A true CN107450395A (en) 2017-12-08

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CN (1) CN107450395A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108033008A (en) * 2017-12-15 2018-05-15 佛山市神风航空科技有限公司 One kind is herded with bionic mechanical bird and its flight control method

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CN205485626U (en) * 2015-12-31 2016-08-17 江苏首控制造技术有限公司 Multi freedom inertial sensor four -axis unmanned aerial vehicle self -contained navigation flight controller
CN106054928A (en) * 2016-05-18 2016-10-26 中国计量大学 All-region fire generation determination method based on unmanned plane network
CN106652456A (en) * 2017-01-20 2017-05-10 上海琛岫自控科技有限公司 Unmanned aerial vehicle detection system used for road section congestion alarming
CN207473339U (en) * 2017-08-15 2018-06-08 江苏穿越金点信息科技股份有限公司 Unmanned plane Information locating acquisition control system

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Publication number Priority date Publication date Assignee Title
CN202632538U (en) * 2012-04-19 2012-12-26 江苏穿越金点信息科技有限公司 Bus GPS positioning station reporting integrated display system
CN104240508A (en) * 2014-09-20 2014-12-24 无锡北斗星通信息科技有限公司 Unmanned plane detection system for road segment congestion alarming
CN104269054A (en) * 2014-09-20 2015-01-07 无锡北斗星通信息科技有限公司 Road segment traffic index estimation system based on unmanned aerial vehicle measurement
CN104980708A (en) * 2015-06-30 2015-10-14 江苏首控制造技术有限公司 Hand-held-terminal-contained remote direct-broadcasting monitoring system of unmanned plane
CN105468010A (en) * 2015-12-31 2016-04-06 江苏首控制造技术有限公司 Multi-degree of freedom inertial sensor four-axis unmanned aerial vehicle autonomous navigation flight controller
CN205485626U (en) * 2015-12-31 2016-08-17 江苏首控制造技术有限公司 Multi freedom inertial sensor four -axis unmanned aerial vehicle self -contained navigation flight controller
CN105516684A (en) * 2016-01-15 2016-04-20 南彦勃 Patrol inspection method for power transmission line of power grid
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CN207473339U (en) * 2017-08-15 2018-06-08 江苏穿越金点信息科技股份有限公司 Unmanned plane Information locating acquisition control system

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108033008A (en) * 2017-12-15 2018-05-15 佛山市神风航空科技有限公司 One kind is herded with bionic mechanical bird and its flight control method

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Application publication date: 20171208