CN207281593U - Unmanned aerial vehicle control system - Google Patents
Unmanned aerial vehicle control system Download PDFInfo
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- CN207281593U CN207281593U CN201721019651.0U CN201721019651U CN207281593U CN 207281593 U CN207281593 U CN 207281593U CN 201721019651 U CN201721019651 U CN 201721019651U CN 207281593 U CN207281593 U CN 207281593U
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- primary processor
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- aerial vehicle
- vehicle control
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Abstract
The utility model discloses a kind of unmanned aerial vehicle control system.Including being powered primary processor by power module in unmanned plane, primary processor connects posture heading system respectively, pressure-altitude sensor, GPS module, ultrasonic sensor, airborne sensory equipment, information storage module, ultrasonic distance measuring module and electron speed regulator, pressure-altitude sensor is all connected with being connected with primary processor after comparing with GPS module, information storage module is stored with no-fly area information, posture heading system is directly over instruction calls program and is connected with information storage module, ultrasonic distance measuring module is directly over instruction calls program and is connected with posture heading system, primary processor also connects capture apparatus by shoot control system, primary processor is connected by the information processing system of Techniques Used in Digital Microwave Transmission and earth station.After above-mentioned structure, hovering and location data are accurate, and communication speed is very fast, improves the stability of communication, reliably avoids the problem of unmanned plane can not be controlled.
Description
Technical field
The present invention relates to a kind of control technology of unmanned plane, specifically a kind of unmanned aerial vehicle control system.
Background technology
With the development of society, unmanned plane is gradually gained popularity in daily life and is widely applied to each
Field（Such as early warning of taking precautions against natural calamities, geographical mapping, meteorological observation, walking along the street navigation）, but existing unmanned aerial vehicle control system is due to control
Means processed are unreasonable, and also there are following defect, on the one hand, positioning accuracy is not high, and poor reliability of hovering, there are larger wind
Danger, another further aspect, signal is easily lost, and leads to not controlled, also has on the one hand, is easily accessible no-fly region and collision barrier
Hinder thing.
The content of the invention
The technical problem to be solved in the present invention is to provide a kind of accurate positioning, hovering reliability is high, signal stabilization and can
The unmanned aerial vehicle control system in no-fly region is avoided enter into completely.
In order to solve the above-mentioned technical problem, unmanned aerial vehicle control system of the invention, including in unmanned plane by electricity
Source module power supply primary processor, primary processor connect posture heading system, pressure-altitude sensor, GPS module, ultrasonic wave respectively
Sensor, airborne sensory equipment, information storage module, ultrasonic distance measuring module and electron speed regulator, pressure-altitude sensor
It is all connected with being connected with primary processor after comparing with GPS module, information storage module is stored with no-fly area information, posture boat
Instruction calls program is directly over to system to be connected with information storage module, ultrasonic distance measuring module is directly over instruction calls journey
Sequence is connected with posture heading system, and primary processor also connects capture apparatus by shoot control system, and primary processor is by numeral
The information processing system of microwave transmission and earth station communicates wirelessly connection.
The airborne sensory equipment airborne sensory equipment includes CCD digital cameras, light optical camera, infrared scanner,
Laser scanner, magnetic determining device.
The posture heading system includes three-axis gyroscope, three axis accelerometer and three axis magnetic compasses.
After above-mentioned structure, it is connected due to the pressure-altitude sensor of setting and by comparing with primary processor
Pressure-altitude sensor and GPS module, it is possible thereby to directly be measured by ultrasonic sensor with the distance on ground and by right
The coordinate of horizontal level is determined than the data message after processing so that hovering and location data are accurate, memory module and super
Sound ranging module is directly over instruction calls program and is connected with posture heading system, thus when running into no-fly region or obstacle
Can directly it be transmitted during thing into row information, communication speed is very fast, and avoid that control time delay brings rushes or collide and ask by mistake
Topic, primary processor communicate wirelessly connection by the information processing system of Techniques Used in Digital Microwave Transmission and earth station, and the face of optimizing connects
Terminal and transmission mode are received, the stability of communication is improved, reliably avoids the problem of unmanned plane can not be controlled, its synthesis is adopted
With technologies such as computer network communication and wireless communications, can be widely applied to traffic administration, big data statistics, early warning of taking precautions against natural calamities,
The various aspects such as geographical mapping, meteorological observation, walking along the street navigation and real-time monitoring.
Brief description of the drawings
Fig. 1 is the functional block diagram of unmanned aerial vehicle control system of the present invention.
Embodiment
With reference to the accompanying drawings and detailed description, the unmanned aerial vehicle control system of the present invention is described in further detail.
As shown in the figure, the unmanned aerial vehicle control system of the present invention, including being powered by power module in unmanned plane are led
Processor, it is characterised in that：The primary processor connects posture heading system, pressure-altitude sensor, GPS module, super respectively
Sonic sensor, airborne sensory equipment, information storage module, ultrasonic distance measuring module and electron speed regulator, pressure altitude pass
Sensor is all connected with being connected with primary processor after comparing with GPS module, and information storage module is stored with no-fly area information, appearance
State heading system is directly over instruction calls program and is connected with information storage module, can be according to nobody by information storage module
The positional information of machine judges whether unmanned plane enters no-fly region, if going out unmanned plane enters no-fly region, controls unmanned plane
Directly land, first no-fly region is judged during this, directly invoking program need not be again by the complicated fortune of master controller
The control of calculation, improves processing speed, and ultrasonic distance measuring module is directly over instruction calls program and is connected with posture heading system,
The distance between surrounding barrier can be detected by ultrasonic distance measuring module, it is got around obstacle when there is barrier
Thing flies, and equally first barrier is judged during this, and directly invoking program need not be again by the complicated fortune of master controller
The control of calculation, improves processing speed, and primary processor also connects capture apparatus by shoot control system, and primary processor passes through number
The information processing system of word microwave transmission and earth station communicates wirelessly connection.
Further, described airborne sensory equipment airborne sensory equipment include CCD digital cameras, light optical camera,
Infrared scanner, laser scanner, magnetic determining device, described posture heading system include three-axis gyroscope, three axis accelerometer with
And three axis magnetic compasses, wherein it is possible to be provided with primary processor with instruction calls program be directly connected to apart from threshold values, use
When, first pass through ultrasonic distance measuring module and detect unmanned plane apart from the distance between barrier, when ultrasonic distance measuring module detects
When unmanned plane during flying distance is less than setting apart from threshold values, you can pass through primary processor and control change of flight posture, get around obstacle
Thing, when unmanned plane during flying excessive velocities have little time avoiding obstacles by setting apart from threshold values, is then referred to by caller
Order directly gets around barrier, further increases the reliability of unmanned plane during flying.
Claims (3)
1. a kind of unmanned aerial vehicle control system, including being powered primary processor by power module in unmanned plane, its feature exists
In：The primary processor connects posture heading system, pressure-altitude sensor, GPS module, ultrasonic sensor, airborne respectively
Remote sensing equipment, information storage module, ultrasonic distance measuring module and electron speed regulator, the pressure-altitude sensor and GPS moulds
Block is all connected with being connected with primary processor after comparison, and the memory module is stored with no-fly area information, the posture course
System is directly over instruction calls program and is connected with information storage module, and the ultrasonic distance measuring module is directly over instruction calls
Program is connected with posture heading system, and the primary processor also connects capture apparatus, primary processor warp by shoot control system
The information processing system for crossing Techniques Used in Digital Microwave Transmission and earth station communicates wirelessly connection.
2. unmanned aerial vehicle control system described in accordance with the claim 1, it is characterised in that：The airborne sensory equipment aerial remote sensing is set
It is standby to include CCD digital cameras, light optical camera, infrared scanner, laser scanner, magnetic determining device.
3. according to the unmanned aerial vehicle control system described in claim 1 or 2, it is characterised in that：The posture heading system includes three
Axis gyroscope, three axis accelerometer and three axis magnetic compasses.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721019651.0U CN207281593U (en) | 2017-08-15 | 2017-08-15 | Unmanned aerial vehicle control system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721019651.0U CN207281593U (en) | 2017-08-15 | 2017-08-15 | Unmanned aerial vehicle control system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207281593U true CN207281593U (en) | 2018-04-27 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201721019651.0U Active CN207281593U (en) | 2017-08-15 | 2017-08-15 | Unmanned aerial vehicle control system |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107390707A (en) * | 2017-08-15 | 2017-11-24 | 江苏穿越金点信息科技股份有限公司 | Unmanned aerial vehicle control system |
-
2017
- 2017-08-15 CN CN201721019651.0U patent/CN207281593U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107390707A (en) * | 2017-08-15 | 2017-11-24 | 江苏穿越金点信息科技股份有限公司 | Unmanned aerial vehicle control system |
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