CN106291638A - A kind of unmanned plane dual link tracing system of integrated black box - Google Patents
A kind of unmanned plane dual link tracing system of integrated black box Download PDFInfo
- Publication number
- CN106291638A CN106291638A CN201610671585.9A CN201610671585A CN106291638A CN 106291638 A CN106291638 A CN 106291638A CN 201610671585 A CN201610671585 A CN 201610671585A CN 106291638 A CN106291638 A CN 106291638A
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- CN
- China
- Prior art keywords
- dual link
- module
- microprocessor
- tracing system
- link tracing
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- 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.)
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Classifications
-
- 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
-
- 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
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04W—WIRELESS COMMUNICATION NETWORKS
- H04W4/00—Services specially adapted for wireless communication networks; Facilities therefor
- H04W4/02—Services making use of location information
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02D—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN INFORMATION AND COMMUNICATION TECHNOLOGIES [ICT], I.E. INFORMATION AND COMMUNICATION TECHNOLOGIES AIMING AT THE REDUCTION OF THEIR OWN ENERGY USE
- Y02D30/00—Reducing energy consumption in communication networks
- Y02D30/70—Reducing energy consumption in communication networks in wireless communication networks
Abstract
nullThe invention discloses the unmanned plane dual link tracing system of a kind of integrated black box，Including microprocessor、Memorizer、Flight controller、Electric power system、Dual link tracing system and ground display system，Wherein memorizer is bi-directionally connected with microprocessor，Described electric power system is connected with microprocessor，Flight controller is connected with electric power system，Described dual link tracing system is bi-directionally connected with microprocessor，Described ground display system is unidirectional with dual link tracing system to be connected，Described electric power system includes power supply protection circuit、Electric source monitoring circuit and battery/reserve battery，Described dual link tracing system includes Big Dipper module、Big Dipper short message module、Gsm module and data processing module，Achieve unmanned plane by dual link tracing system and have movable signal and the switching without the tracing system in the environment of movable signal，Ensure accuracy and the stability of work of unmanned plane location information，Described battery/reserve battery，Ensure that whole system the most normally works.
Description
Technical field
The invention belongs to unmanned plane positioning tracking technology field, specifically, the present invention relates to a kind of integrated black box
Unmanned plane dual link tracing system.
Background technology
Along with the development of unmanned air vehicle technique in recent years, the application of unmanned plane is constantly widened, military affairs from the beginning, instead
Probably field gradually extends to the every aspect of our life.Existing unmanned plane tracker location relies on movable signal, once unmanned
Machine flies into and covers or in the very weak environment of movable signal without movable signal, will be unable to terrestrial system feedback location information,
In addition, existing unmanned plane tracker does not possess flying quality storage function, once occurs that unmanned plane has an accident, and flying quality can
Can not get effectively preserving.
Summary of the invention
The present invention provides the unmanned plane dual link tracing system of a kind of integrated black box, it is therefore an objective to realizing unmanned plane is having shifting
Move signal and without the environment of movable signal realizes location information switching, it is ensured that working stability.
To achieve these goals, the technical scheme that the present invention takes is: the unmanned plane dual link of a kind of integrated black box
Tracing system, including microprocessor, memorizer, flight controller, electric power system, dual link tracing system and ground display system
System, wherein memorizer is bi-directionally connected with microprocessor, and described electric power system is connected with microprocessor, flight controller and power supply system
System connects, and described dual link tracing system is bi-directionally connected with microprocessor, described ground display system and dual link tracing system
Unidirectional connection.
Preferably, described electric power system includes power supply protection circuit, electric source monitoring circuit and battery/reserve battery, described
Power supply protection circuit is directly bi-directionally connected with microprocessor, and flight controller is bi-directionally connected with power supply protection circuit, described power supply
Observation circuit is the most unidirectional with power supply protection circuit to be connected, and another aspect is the most unidirectional with microprocessor to be connected, described battery/standby
Battery is unidirectional with microprocessor to be connected.
Preferably, described dual link tracing system includes at Big Dipper module, Big Dipper short message module, gsm module and data
Reason module, wherein Big Dipper module is bi-directionally connected with microprocessor, and Big Dipper short message module is unidirectional with Big Dipper module to be connected, at data
Module is unidirectional with Big Dipper short message module is connected for reason, and described gsm module is bi-directionally connected with microprocessor, data processing module and
The unidirectional connection of gsm module, described ground display system is unidirectional with the data processing module in dual link tracing system to be connected.
The present invention be for realize unmanned plane have movable signal and without the environment of movable signal in realize location information and cut
Change, it is ensured that working stability, unmanned plane tracing system done brand-new design, use above technical scheme to provide the benefit that:
In the case of having movable signal to cover, location information is mail to data processing module by gsm module, and the data after process are by ground
Display system shows, when in unmanned plane during flying to the environment covered without movable signal, location information is passed through north by microprocessor
Bucket module mails to Big Dipper short message module with the form of short message, location information is mail at data processing module the most again
Reason, the data after process are shown by ground display system, it is achieved that unmanned plane is having movable signal and the environment without movable signal
In the switching of tracing system, it is ensured that the accuracy of unmanned plane location information and the stability of work；The most within the system
Electric power system is provided with electric source monitoring circuit, when electric source monitoring circuit detects electric power system, powering-off state, microprocessor occurs
Process, start reserve battery, it is ensured that whole system the most normally works.
Accompanying drawing explanation
Fig. 1 is the control block diagram of this system.
Detailed description of the invention
Below against accompanying drawing, by the description to embodiment, the detailed description of the invention of the present invention is made further details of
Explanation, it is therefore an objective to help those skilled in the art that design, the technical scheme of the present invention are had more complete, accurate and deep reason
Solve, and contribute to its enforcement.
As it is shown in figure 1, the present invention is the unmanned plane dual link tracing system of a kind of integrated black box, it is unmanned for realizing
Machine have movable signal and without the environment of movable signal in realize the switching of location information, it is ensured that working stability.
Specifically, as it is shown in figure 1, include that microprocessor, memorizer, flight controller, electric power system, dual link are followed the trail of
System and ground display system, wherein memorizer is bi-directionally connected with microprocessor, and described electric power system is connected with microprocessor, flies
Line control unit is connected with electric power system, and described dual link tracing system is bi-directionally connected with microprocessor, described ground display system
Unidirectional with dual link tracing system it is connected；Described electric power system includes power supply protection circuit, electric source monitoring circuit and battery/standby
Battery, described power supply protection circuit is directly bi-directionally connected with microprocessor, and flight controller is bi-directionally connected with power supply protection circuit,
Described electric source monitoring circuit is the most unidirectional with power supply protection circuit to be connected, and another aspect is the most unidirectional with microprocessor to be connected, described
Battery/reserve battery is unidirectional with microprocessor to be connected；Described dual link tracing system includes Big Dipper module, Big Dipper short message mould
Block, gsm module and data processing module, wherein Big Dipper module is bi-directionally connected with microprocessor, Big Dipper short message module and the Big Dipper
The unidirectional connection of module, data processing module is unidirectional with Big Dipper short message module to be connected, described gsm module and the two-way company of microprocessor
Connecing, data processing module is unidirectional with gsm module to be connected, at the data in described ground display system and dual link tracing system
The reason unidirectional connection of module.
With specific embodiment, specific works mode is illustrated below:
When unmanned plane works, during normal work by battery through microprocessor to flight controller and whole tracing system
Power supply, flying quality is fed back to microprocessor by flight controller simultaneously, and then flying quality is stored in storage by microprocessor
In device, it is achieved the preservation of flying quality, described electric source monitoring circuit is the most unidirectional with power supply protection circuit to be connected, on the other hand
Unidirectional with microprocessor it is connected, when electric source monitoring circuit monitors system power supply by power supply protection circuit, power-down conditions occurs
Time, electric source monitoring circuit can pass through microprocessor, starts reserve battery, it is ensured that whole system the most normally works；
When unmanned plane flight in the case of having movable signal to cover, first general location information conveyance is to microprocessor, then for gsm module
Location data after microprocessor screens flow to gsm module again, and then location information is mail at data by gsm module again
Reason module, the data after process are shown by ground display system；When unmanned plane flight in the case of covering without movable signal,
Big Dipper module first general location information conveyance, to microprocessor, is then passed through the location data after microprocessor screening and flows to north again
Bucket module, then location information is mail to Big Dipper short message module with the form of short message by Big Dipper module again, the most again will location
Information mails to data processing module and processes, and the data after process are shown by ground display system, it is achieved that unmanned plane is having
Movable signal and the switching without the tracing system in the environment of movable signal, it is ensured that the accuracy of unmanned plane location information and work
Stability.
Above in association with accompanying drawing, the present invention is exemplarily described, it is clear that the present invention implements not by above-mentioned side
The restriction of formula, as long as have employed the improvement of the various unsubstantialities that method is conceived and technical scheme is carried out of the present invention；Or not
Improved, above-mentioned design and the technical scheme of the present invention are directly applied to other occasion, all in protection scope of the present invention
Within.
Claims (3)
1. the unmanned plane dual link tracing system of an integrated black box, it is characterised in that: include microprocessor, memorizer, fly
Line control unit, electric power system, dual link tracing system and ground display system, wherein memorizer is bi-directionally connected with microprocessor,
Described electric power system is connected with microprocessor, and flight controller is connected with electric power system, described dual link tracing system and Wei Chu
Reason device is bi-directionally connected, and described ground display system is unidirectional with dual link tracing system to be connected.
The unmanned plane dual link tracing system of a kind of integrated black box the most according to claim 1, it is characterised in that: described
Electric power system includes power supply protection circuit, electric source monitoring circuit and battery/reserve battery, and described power supply protection circuit is directly with micro-
Processor is bi-directionally connected, and flight controller is bi-directionally connected with power supply protection circuit, described electric source monitoring circuit one side and power supply
The unidirectional connection of protection circuit, another aspect is the most unidirectional with microprocessor to be connected, described battery/reserve battery and the unidirectional company of microprocessor
Connect.
The unmanned plane dual link tracing system of a kind of integrated black box the most according to claim 1, it is characterised in that: described
Dual link tracing system includes Big Dipper module, Big Dipper short message module, gsm module and data processing module, wherein Big Dipper module
Being bi-directionally connected with microprocessor, Big Dipper short message module is unidirectional with Big Dipper module to be connected, data processing module and Big Dipper short message
The unidirectional connection of module, described gsm module is bi-directionally connected with microprocessor, and data processing module is unidirectional with gsm module to be connected, described
Ground display system unidirectional with the data processing module in dual link tracing system be connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610671585.9A CN106291638A (en) | 2016-08-16 | 2016-08-16 | A kind of unmanned plane dual link tracing system of integrated black box |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201610671585.9A CN106291638A (en) | 2016-08-16 | 2016-08-16 | A kind of unmanned plane dual link tracing system of integrated black box |
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| CN106291638A true CN106291638A (en) | 2017-01-04 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610671585.9A Pending CN106291638A (en) | 2016-08-16 | 2016-08-16 | A kind of unmanned plane dual link tracing system of integrated black box |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107302394A (en) * | 2017-06-19 | 2017-10-27 | 四川腾盾科技有限公司 | A kind of unmanned aerial vehicle (UAV) control method based on Big Dipper short message |
| CN110944017A (en) * | 2019-12-25 | 2020-03-31 | 中电科航空电子有限公司 | Airborne position tracking equipment with bidirectional information transmission function |
| WO2022089381A1 (en) * | 2020-10-29 | 2022-05-05 | 泰斗微电子科技有限公司 | Dual-channel switching method, unmanned aerial vehicle, and control terminal |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107302394A (en) * | 2017-06-19 | 2017-10-27 | 四川腾盾科技有限公司 | A kind of unmanned aerial vehicle (UAV) control method based on Big Dipper short message |
| CN110944017A (en) * | 2019-12-25 | 2020-03-31 | 中电科航空电子有限公司 | Airborne position tracking equipment with bidirectional information transmission function |
| CN110944017B (en) * | 2019-12-25 | 2024-04-05 | 中电科航空电子有限公司 | Airborne position tracking equipment for bidirectional information transmission |
| WO2022089381A1 (en) * | 2020-10-29 | 2022-05-05 | 泰斗微电子科技有限公司 | Dual-channel switching method, unmanned aerial vehicle, and control terminal |
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Application publication date: 20170104 |