CN107450395A - Unmanned plane Information locating acquisition control system - Google Patents
Unmanned plane Information locating acquisition control system Download PDFInfo
- 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
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- unmanned plane
- information
- dsp processor
- control system
- processing system
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- 230000010365 information processing Effects 0.000 claims abstract description 20
- 238000004891 communication Methods 0.000 claims abstract description 10
- 238000012546 transfer Methods 0.000 claims abstract description 5
- 230000005540 biological transmission Effects 0.000 claims 5
- 230000005611 electricity Effects 0.000 claims 1
- 238000013461 design Methods 0.000 abstract description 2
- 238000011161 development Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000010200 validation analysis Methods 0.000 description 1
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B19/00—Programme-control systems
- G05B19/02—Programme-control systems electric
- G05B19/04—Programme control other than numerical control, i.e. in sequence controllers or logic controllers
- G05B19/042—Programme control other than numerical control, i.e. in sequence controllers or logic controllers using digital processors
- G05B19/0423—Input/output
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B2219/00—Program-control systems
- G05B2219/20—Pc systems
- G05B2219/25—Pc structure of the system
- G05B2219/25257—Microcontroller
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
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)
- 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. 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. 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. 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. 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.
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CN201710697781.8A CN107450395A (en) | 2017-08-15 | 2017-08-15 | Unmanned plane Information locating acquisition control system |
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CN201710697781.8A CN107450395A (en) | 2017-08-15 | 2017-08-15 | Unmanned plane Information locating acquisition control system |
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Cited By (1)
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 |