CN207473339U - Unmanned plane Information locating acquisition control system - Google Patents
Unmanned plane Information locating acquisition control system Download PDFInfo
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- CN207473339U CN207473339U CN201721019179.0U CN201721019179U CN207473339U CN 207473339 U CN207473339 U CN 207473339U CN 201721019179 U CN201721019179 U CN 201721019179U CN 207473339 U CN207473339 U CN 207473339U
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Abstract
The utility model discloses a kind of unmanned plane Information locating acquisition control systems.It includes being powered dsp processor by power module, the vehicle-mounted GPS equipment being connect with in-vehicle processor；Dsp processor connects inertial sensor respectively, pressure-altitude sensor and electron speed regulator, the motor of electron speed regulator and unmanned plane connects, in-vehicle processor is connected 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 in the unmanned plane during flying nearest apart from density center to density center according to the data information received and pass through video camera scene be shot, the reason of 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.Reasonable in design after above-mentioned structure, communication transfer speed block, judging result is accurate, and human resources are greatly saved.
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, by the way that various data are carried out with the grand strategy that analysis is following each big city solution city route planning, the prior art
In, some modes for manually counting of generally use are to various data（Such as the analysis to current traffic）Summarized then
It being compared, such as prediction planning carries out traffic data by comparison result, existing this mode is relatively backward, single,
It needs to expend a large amount of manpower and materials and accuracy is inadequate.
Invention content
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, it is each including being mounted on
Being powered dsp processor by power module in frame unmanned plane, the vehicle being connect 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
The speed of unmanned plane motor is connect and can controlled with the motor of unmanned plane, and 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 and determine bus high density state and general
For data information transfer to the information processing system of overall control center, the information processing system of overall control center can be according to the number received
It is believed that breath makes in the unmanned plane during flying nearest apart from density center to density center and passes through video camera scene is shot,
The dsp processor image information of shooting can be fed directly to overall control center information processing system judge it is intensive
The reason of state.
The display terminal for being used to show information being connect with information processing system is additionally provided in the overall control center.
Described information processing system is connect 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 axis magnetic compasses and the GPS/ Big Dippeves and receives
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, judging result is accurate, and human resources are greatly saved.
Description of the drawings
Fig. 1 is the functional block diagram of unmanned plane Information locating acquisition control system of the present invention.
Specific 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 is described in detail.
As shown in the figure, the unmanned plane Information locating acquisition control system of the present invention, including being mounted in each frame unmanned plane
It is powered dsp processor by power module, the vehicle-mounted GPS equipment being connect with in-vehicle processor in each bus；DSP
Processor connects inertial sensor, pressure-altitude sensor and electron speed regulator respectively, certainly it is essential further include by
The motor of video camera, electron speed regulator and unmanned plane connects and can control the speed of unmanned plane motor, and 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 analyze and determine the intensive of bus according to the location information of vehicle-mounted GPS equipment
State and by data information transfer to the information processing system of overall control center, the information processing system of overall control center can be according to connecing
The data information received makes to be in the unmanned plane during flying nearest apart from density center to density center and passes through video camera to scene
Shot, wherein, due to the monitoring range of unmanned plane be it is limited, in actual use, while multi rack of going on a journey
Unmanned plane and every frame unmanned plane are responsible for different ranges, 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 of judgement high density state.
Wherein, it is whole that the display for being used to show information being connect with information processing system is additionally provided in described overall control center
End, described information processing system are connect 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 axis magnetic compasses and
GPS/ Beidou receivers, described inertial sensor are MEMS sensor.
Claims (5)
1. a kind of unmanned plane Information locating acquisition control system, it is characterised in that：Including be mounted in each frame unmanned plane by electricity
Source module power supply dsp processor, the vehicle-mounted GPS equipment being connect 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 connect 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 and determine bus high density state and general
For data information transfer to the information processing system of overall control center, the information processing system of the overall control center can be according to receiving
Data information make in the unmanned plane during flying nearest apart from density center to density center and pass through 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 of disconnected high density state.
2. unmanned plane Information locating acquisition control system described in accordance with the claim 1, it is characterised in that：In the overall control center
It is additionally provided with the display terminal for being used to show information being connect with information processing system.
3. according to the unmanned plane Information locating acquisition control system described in claims 1 or 2, it is characterised in that：At described information
Reason system is connect with operation control system by input equipment interface and can input the operation from input operation control system
Instruction.
4. unmanned plane Information locating acquisition control system described in accordance with the claim 3, it is characterised in that：The inertial sensor
Including three-axis gyroscope, three axis accelerometer, three axis magnetic compasses and GPS/ Beidou receivers.
5. according to the unmanned plane Information locating acquisition control system described in claim 4, it is characterised in that：The inertial sensor
For MEMS sensor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721019179.0U CN207473339U (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 |
|---|---|---|---|
| CN201721019179.0U CN207473339U (en) | 2017-08-15 | 2017-08-15 | Unmanned plane Information locating acquisition control system |
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| Publication Number | Publication Date |
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| CN207473339U true CN207473339U (en) | 2018-06-08 |
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| CN201721019179.0U Active CN207473339U (en) | 2017-08-15 | 2017-08-15 | Unmanned plane Information locating acquisition control system |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107450395A (en) * | 2017-08-15 | 2017-12-08 | 江苏穿越金点信息科技股份有限公司 | Unmanned plane Information locating acquisition control system |
| CN109324685A (en) * | 2017-08-01 | 2019-02-12 | 卡西欧计算机株式会社 | Information processing unit, information processing method and recording medium |
-
2017
- 2017-08-15 CN CN201721019179.0U patent/CN207473339U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109324685A (en) * | 2017-08-01 | 2019-02-12 | 卡西欧计算机株式会社 | Information processing unit, information processing method and recording medium |
| CN107450395A (en) * | 2017-08-15 | 2017-12-08 | 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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