CN106060079A - Unmanned aerial vehicle authentication system and method - Google Patents
Unmanned aerial vehicle authentication system and method Download PDFInfo
- Publication number
- CN106060079A CN106060079A CN201610544022.3A CN201610544022A CN106060079A CN 106060079 A CN106060079 A CN 106060079A CN 201610544022 A CN201610544022 A CN 201610544022A CN 106060079 A CN106060079 A CN 106060079A
- Authority
- CN
- China
- Prior art keywords
- unit
- certification
- unmanned plane
- authentication
- parts
- 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
Links
- 238000000034 method Methods 0.000 title claims abstract description 28
- 230000005611 electricity Effects 0.000 claims description 27
- 238000012790 confirmation Methods 0.000 claims description 21
- 238000012795 verification Methods 0.000 claims description 10
- 238000004891 communication Methods 0.000 claims description 5
- 230000005540 biological transmission Effects 0.000 claims description 3
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical group C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 abstract 4
- 238000010586 diagram Methods 0.000 description 8
- 238000005516 engineering process Methods 0.000 description 5
- 238000005183 dynamical system Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 230000004044 response Effects 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 239000000306 component Substances 0.000 description 1
- 239000008358 core component Substances 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000024703 flight behavior Effects 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L63/00—Network architectures or network communication protocols for network security
- H04L63/08—Network architectures or network communication protocols for network security for authentication of entities
- H04L63/0869—Network architectures or network communication protocols for network security for authentication of entities for achieving mutual authentication
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/0011—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot associated with a remote control arrangement
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
-
- G—PHYSICS
- G08—SIGNALLING
- G08C—TRANSMISSION SYSTEMS FOR MEASURED VALUES, CONTROL OR SIMILAR SIGNALS
- G08C17/00—Arrangements for transmitting signals characterised by the use of a wireless electrical link
- G08C17/02—Arrangements for transmitting signals characterised by the use of a wireless electrical link using a radio link
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L63/00—Network architectures or network communication protocols for network security
- H04L63/08—Network architectures or network communication protocols for network security for authentication of entities
- H04L63/0876—Network architectures or network communication protocols for network security for authentication of entities based on the identity of the terminal or configuration, e.g. MAC address, hardware or software configuration or device fingerprint
Abstract
The invention discloses an unmanned aerial vehicle authentication system and an unmanned aerial vehicle authentication method. The system comprises a recognition unit, a flight control unit and an authentication unit, wherein the recognition unit is configured to recognize the identity of a user; a flight control unit is configured to receive an authentication code of each component of an unmanned aerial vehicle, and upload the authentication codes to an authentication unit; the authentication unit is configured to find the corresponding authentication code of each piece of authentication information, check the authentication information and the corresponding authentication code, and send a check result to the flight control unit; and the flight control unit is also used for receiving the check result, and controlling the unmanned serial vehicle to execute a flight command when the check result shows that configuration of each component of the unmanned serial vehicle is legal. According to the method, the authentication information and the corresponding authentication code of each component are checked, so that authentication control is performed on each component, and use security of the unmanned serial vehicle is improved.
Description
Technical field
The disclosure relates generally to unmanned air vehicle technique field, is specifically related to unmanned plane manipulation field, particularly relates to a kind of unmanned
Machine Verification System；
The disclosure further relates to unmanned plane authentication method.
Background technology
UAV, is called for short unmanned plane, is to utilize radio robot and the presetting apparatus provided for oneself to handle
The most manned aircraft.
Along with the gradually refinement of unmanned plane during flying management and control regulations, the management and control to the flight of unmanned plane becomes most important.Existing
Some model plane, civilian and plant protection and other kinds of unmanned plane are reequiped through non-producer again, directly can be controlled by individual
Flight.
Program encryption has been done just for kernel control module by unmanned plane enterprise now, makees battery and recognize powering on when
Card, and other core components can not be done certification control.After aircraft is lost, individual can disassemble voluntarily and again assemble
, there is the biggest uncontrollable risk in one brand-new aircraft.
Summary of the invention
In view of drawbacks described above of the prior art or deficiency, it is desirable to providing a kind of can be carried out all parts of unmanned plane
Certification management and control, improves Verification System and the authentication method of the safety that unmanned plane uses.
First aspect, it is provided that a kind of unmanned plane Verification System, described system includes: recognition unit, is configured to adopting
After collection arrives the identity information of user's input, being identified the identity of user, after identifying successfully, authentication ' unit issues certification request
And the unique mark exciting the authentication information prestored in authentication ' unit, described authentication information to be all parts of the unmanned plane prestored
Information and/or the identity information of all parts；Fly to control unit, be configured to receive described certification and ask and collect each of unmanned plane
The certification coding of individual parts, uploads described certification and is encoded to authentication ' unit, carries unmanned plane each in described certification coding
The unique identification information of parts and/or the identity information of all parts；And authentication ' unit, it is configured to find and each certification
The certification coding that information is corresponding, and authentication information and corresponding certification encoded and check, to determine each of unmanned plane
The configuration of parts is the most legal, and controls unit transmission control instruction to described flying；The described control unit that flies is additionally operable to receive described control
System instruction, and perform unmanned plane during flying operation according to described control instruction or stop unmanned plane during flying operation.
Preferably, all parts of unmanned plane by chip with described fly control unit communication so that described in fly control unit obtain
Take the certification coding of all parts.
Preferably, the parts of unmanned plane include following at least one: battery, electricity are adjusted, motor and electromotor.
Preferably, described motor is adjusted by described electricity and is connected with the described control unit that flies, and described electricity is stealthily substituted and included confirmation unit, institute
State confirmation unit to be configured to obtain the certification coding of motor the certification of motor being encoded and prestore in described confirmation unit
The authentication information of motor is checked, and encodes and the authentication information phase of motor that prestores in described confirmation unit in the certification of motor
The certification of the certification coding and electricity tune of uploading motor during to correspondence is encoded to described authentication ' unit.
Preferably, described recognition unit is also configured to after the identity information collecting user's input first, and storage is used
The identity information at family, to carry out system of real name registration to unmanned plane；Described recognition unit is also configured to again collecting user
After the identity information of input, identity information user inputted is checked with the information of system of real name registration in recognition unit, with
Identify user identity.
Second aspect, it is provided that a kind of unmanned plane authentication method, described method includes: in the identity collecting user's input
After information, the identity of user is identified by recognition unit, and after identifying successfully, authentication ' unit issues certification and asks and excite certification
The authentication information prestored in unit, described authentication information be all parts of the unmanned plane prestored unique identification information and/or
The identity information of all parts；The certification flying to control all parts that unit reception certification is asked and collected unmanned plane encodes, and uploads
Described certification is encoded to authentication ' unit, described certification coding carries all parts of unmanned plane unique identification information and/
Or the identity information of all parts；Authentication ' unit finds the certification coding corresponding with each authentication information, and by authentication information
Check with corresponding certification coding, the most legal to determine the configuration of all parts of unmanned plane, and fly control list to described
Unit sends control instruction；Fly to control unit described in and and receive described control instruction, and perform unmanned plane according to described control instruction
Flight operation or stopping unmanned plane during flying operation.
Preferably, described in fly to control the chip communication of all parts of unit and unmanned plane, and obtain from corresponding described chip
Take the certification coding of all parts.
Preferably, the parts of unmanned plane include following at least one: battery, electricity are adjusted, motor and electromotor.
Preferably, described motor is adjusted by described electricity and is connected with the described control unit that flies, and described electricity is stealthily substituted and included confirmation unit, institute
State confirmation unit obtain the certification coding of motor and the certification of motor encoded and the recognizing of motor that prestore in described confirmation unit
Card information is checked, when the certification of motor encodes corresponding with the authentication information of the motor prestored in described confirmation unit,
The certification of the certification coding and electricity tune of uploading motor is encoded to described authentication ' unit.
Preferably, after the identity information collecting user's input first, the identity letter of described recognition unit storage user
Breath, to carry out system of real name registration to unmanned plane；After the identity information again collecting user's input, described recognition unit is also joined
The information of system of real name registration in identity information user inputted with recognition unit of putting is checked, to identify user's body
Part.
The application is by checking the authentication information of all parts, therefore to all parts with corresponding certification coding
It is authenticated management and control, improves the safety that unmanned plane uses.
Accompanying drawing explanation
By the detailed description that non-limiting example is made made with reference to the following drawings of reading, other of the application
Feature, purpose and advantage will become more apparent upon:
Fig. 1 shows the block diagram of the unmanned plane Verification System according to the embodiment of the present application；And
Fig. 2 shows the exemplary process diagram of the unmanned plane authentication method according to the embodiment of the present application.
Detailed description of the invention
With embodiment, the application is described in further detail below in conjunction with the accompanying drawings.It is understood that this place is retouched
The specific embodiment stated is used only for explaining related invention, rather than the restriction to this invention.It also should be noted that, in order to
It is easy to describe, accompanying drawing illustrate only and invent relevant part.
It should be noted that in the case of not conflicting, the embodiment in the application and the feature in embodiment can phases
Combination mutually.Describe the application below with reference to the accompanying drawings and in conjunction with the embodiments in detail.
Refer to Fig. 1, it illustrates the block diagram of unmanned plane Verification System according to the embodiment of the present application.
As it is shown in figure 1, unmanned plane Verification System can include recognition unit, fly to control unit and authentication ' unit.Wherein, control is flown
Unit is connected with all parts of unmanned plane, and authentication ' unit is connected with flying to control unit and recognition unit.Collecting user's input
Identity information after, recognition unit for receive user input identity information, recognition unit can be to the identity information of user
Check, to identify user identity.Wherein, user can be inputted used by modes such as handheld terminal or mobile phone A PP softwares
The identity information at family.Fly to control unit to be connected with authentication ' unit by wireless or wired form.
After identifying successfully, authentication ' unit issues certification and asks and excite the authentication information prestored in authentication ' unit, its
In, authentication information is unique identification information and/or each portion of all parts of the unmanned plane being previously stored in authentication ' unit
The identity information of part.Identification information can include numbering or coding or bar code or Quick Response Code.Fly to control unit to receive and recognize
After card request, can collect the certification coding of all parts of unmanned plane, wherein, each parts of unmanned plane have respective
Certification encodes, and when receiving certification request, is uploaded to fly to control unit by each certification coding.The certification coding of each parts
In carry the unique identification information of corresponding component and/or the identity information of all parts.Wherein, identification information can include compiling
Number or coding or bar code or Quick Response Code.Authentication ' unit is for each authentication information found and be stored in authentication ' unit
Corresponding or identical certification coding, and authentication information is checked with corresponding certification coding.So, all parts is worked as
Authentication information respectively with corresponding certification coding can one_to_one corresponding and when checking correct, determine all parts of unmanned plane
Configuration be legal, and to fly control unit send control instruction, fly control unit receive control instruction, unmanned plane is performed flight
Operation.When authentication information and the certification coding of all parts can not one_to_one corresponding or when checking incorrect, explanation can not
Corresponding or to check incorrect parts be illegal parts, i.e. these parts are to be not belonging to the parts of this unmanned plane or damage
Bad.Fly to control unit and send this illegal control instruction, fly to control unit and receive control instruction, perform unmanned plane to stop flight behaviour
Make.So, by the authentication information of all parts is checked with corresponding certification coding, all parts can be carried out
Certification management and control, it is to avoid will not belong to the problem that the parts assembly of same unmanned plane uses together, can also detect simultaneously
Whether the parts of unmanned plane have the problem of damage, improve the safety that unmanned plane uses.Preferably, user is collected first
After the identity information of input, identity information can be stored by recognition unit, thus completes the registration of the system of real name to unmanned plane.It
After, after the identity information again collecting user's input, recognition unit by the verification identity information that again inputs of user and
The information of system of real name registration, to identify user identity.
Further, all parts of unmanned plane can be provided with chip, and in chip, storage has recognizing of unmanned plane all parts
Card coding.Fly to control unit to be communicated with unmanned plane all parts by chip, thus obtain the certification coding of all parts.Its
In, chip is in the case of being disassembled, it is impossible to the enough communication realized and fly to control unit.Such as: chip periphery can be provided with little electricity
Pond, thus maintain the state that chip is kept powered on, and after once the parts of unmanned plane are removed, chip leaves baby battery, makes
Becoming chip power-down, the certification coding of storage inside is lost immediately；Or chip and parts are connected to fly to control unit by flexible cord, disassemble
After cause certification coding cannot be transferred to fly control unit；Or can be by above two mode connected applications.
Yet further, the parts of unmanned plane can include battery, electricity tune, motor and electromotor etc..Wherein, motor is permissible
It is connected with flying control unit by electricity tune.Electricity includes validating that unit in adjusting, confirmation unit encode for the certification obtaining motor and incite somebody to action
The authentication information of the motor prestored in the certification coding of motor and confirmation unit is checked.Certification at motor encodes and confirms
When the authentication information of the motor prestored in unit is corresponding, the certification of the certification coding and electricity tune of uploading motor is encoded to certification list
Unit；The certification of the certification coding and electricity tune that otherwise will not upload motor is encoded to authentication ' unit.
In the technology of technique scheme, when flying to control unit to unmanned plane execution flight directive, all parts just can be just
Often run, such as: electricity is adjusted and just can be controlled electric machine rotation, exports power；Battery could export big electric current for dynamical system.Otherwise,
Battery can only export with small area analysis, maintains the operation flying to control unit, or once output electric current exceedes setting value, and battery is cut automatically
Break and export and shut down.
Refer to Fig. 2, it illustrates the exemplary process diagram of unmanned plane authentication method according to the embodiment of the present application.
Unmanned plane authentication method according to the application, on the basis of technique scheme, as in figure 2 it is shown, method includes:
Step S10, after the identity information collecting user's input, the identity of recognition unit identification user.Identify successfully
Rear authentication ' unit issues certification and asks and excite the authentication information prestored in authentication ' unit, and authentication information is the unmanned plane prestored
The unique identification information of all parts and/or the identity information of all parts.
Step S20, the certification flying to control all parts that unit reception certification is asked and collected unmanned plane encodes, and uploads certification
It is encoded to authentication ' unit.Certification coding carries the unique identification information of all parts of unmanned plane and/or all parts
Identity information.
Step S30, the certification coding that authentication ' unit searching is corresponding with each authentication information, and by authentication information with corresponding
Certification coding check.
Step S40, authentication ' unit confirms that the configuration of all parts of unmanned plane is the most legal, and sends control to flying control unit
System instruction.
Step S50, flies to control unit and receives control instruction, and it is legal to be in the configuration that checked result is unmanned plane all parts
Time, perform unmanned plane during flying operation according to control instruction；
Step S60, flies to control unit and receives checked result, exist in the configuration that checked result is unmanned plane all parts and do not conform to
During method, perform to stop flight operation according to control instruction.
Preferably, before step S10, can be with setting steps S100.Step S100, is collecting what user inputted first
After identity information, recognition unit storage identity information, unmanned plane is carried out system of real name registration.Afterwards, then carry out step S10, i.e.
After collecting the identity information that user inputs again, the identity information that user is inputted by recognition unit and real name in recognition unit
The information of system registration is checked, to identify user identity.
So, by the authentication information of all parts is checked, therefore to all parts with corresponding certification coding
It is authenticated management and control, it is to avoid will not belong to the problem that the parts assembly of same unmanned plane uses together, the most all right
Whether the parts detecting unmanned plane have the problem of damage, improve the safety that unmanned plane uses.
Further, all parts of unmanned plane can be provided with chip, and in chip, storage has recognizing of unmanned plane all parts
Card coding.In performing step S20, fly to control unit and communicated with unmanned plane all parts by chip, thus from chip
Obtain the certification coding of all parts.
Yet further, in all parts of unmanned plane, motor can be connected with flying control unit by electricity tune.During electricity is adjusted
Including validating that unit, when flying in performing step S20 controls the certification coding that unit receives motor, confirmation unit obtains motor
The authentication information of the motor prestored in the certification coding of motor and confirmation unit is also checked by certification coding.Recognizing at motor
When card coding is corresponding with the authentication information of the motor prestored in confirmation unit, upload the certification coding of motor and the electric certification adjusted
It is encoded to authentication ' unit；The certification of the certification coding and electricity tune that otherwise will not upload motor is encoded to authentication ' unit.
In the technology of technique scheme, when flying to control unit to unmanned plane execution flight directive, all parts just can be just
Often run, such as: electricity is adjusted and just can be controlled electric machine rotation, exports power；Battery could export big electric current for dynamical system.Otherwise,
Battery can only export with small area analysis, maintains the operation flying to control unit, or once output electric current exceedes setting value, and battery is cut automatically
Break and export and shut down.
Although it should be noted that, describe the operation of the inventive method in the accompanying drawings with particular order, but, this does not requires that
Or hint must perform these operations according to this particular order, or having to carry out the most shown operation could realize the phase
The result hoped.On the contrary, the step described in flow chart can change execution sequence.Additionally or alternatively, it is convenient to omit some
Multiple steps are merged into a step and are performed by step, and/or a step is decomposed into the execution of multiple step.
Flow chart in accompanying drawing and block diagram, it is illustrated that according to system, method and the computer journey of various embodiments of the invention
Architectural framework in the cards, function and the operation of sequence product.In this, each square frame in flow chart or block diagram can generation
One module of table, program segment or a part for code, a part for described module, program segment or code comprises one or more
For realizing the executable instruction of the logic function of regulation.It should also be noted that some as replace realization in, institute in square frame
The function of mark can also occur to be different from the order marked in accompanying drawing.Such as, the square frame that two succeedingly represent is actual
On can perform substantially in parallel, they can also perform sometimes in the opposite order, and this is depending on involved function.Also want
It is noted that the combination of the square frame in each square frame in block diagram and/or flow chart and block diagram and/or flow chart, Ke Yiyong
The special hardware based system of the function or operation that perform regulation realizes, or can refer to computer with specialized hardware
The combination of order realizes.
It is described in the embodiment of the present application involved unit or module can realize by the way of software, it is also possible to
Realize by the way of hardware.Described unit or module can also be arranged within a processor.These unit or module
Title is not intended that under certain conditions to this unit or the restriction of module itself.
As on the other hand, present invention also provides a kind of computer-readable recording medium, this computer-readable storage medium
Matter can be the computer-readable recording medium described in above-described embodiment included in device；Can also be individualism, not
The computer-readable recording medium being fitted in equipment.Computer-readable recording medium storage has one or more than one journey
Sequence, described program is used for performing to be described in the formula input method of the application by one or more than one processor.
Above description is only the preferred embodiment of the application and the explanation to institute's application technology principle.People in the art
Member should be appreciated that invention scope involved in the application, however it is not limited to the technology of the particular combination of above-mentioned technical characteristic
Scheme, also should contain in the case of without departing from described inventive concept simultaneously, above-mentioned technical characteristic or its equivalent feature carry out
Combination in any and other technical scheme of being formed.Such as features described above has similar merit with (but not limited to) disclosed herein
The technical scheme that the technical characteristic of energy is replaced mutually and formed.
Claims (10)
1. a unmanned plane Verification System, it is characterised in that described system includes:
Recognition unit, is configured to, after the identity information collecting user's input, be identified the identity of user, be identified as
After merit, authentication ' unit issues certification and asks and excite the authentication information prestored in authentication ' unit, and described authentication information is the nothing prestored
The unique identification information of man-machine all parts and/or the identity information of all parts；
Flying to control unit, the certification being configured to receive all parts that described certification is asked and collected unmanned plane encodes, and uploads institute
State certification and be encoded to authentication ' unit, described certification coding carries all parts of unmanned plane unique identification information and/or
The identity information of all parts；And
Authentication ' unit, is configured to find the certification coding corresponding with each authentication information, and by authentication information with corresponding
Certification coding is checked, the most legal to determine the configuration of all parts of unmanned plane, and controls unit transmission control to described flying
System instruction；
Described fly to control unit and be additionally operable to receive described control instruction, and according to described control instruction perform unmanned plane during flying operation or
Person stops unmanned plane during flying operation.
System the most according to claim 1, it is characterised in that all parts of unmanned plane flies control list by chip with described
Unit communication so that described in fly control unit obtain all parts certification coding.
System the most according to claim 2, it is characterised in that the parts of unmanned plane include following at least one: battery, electricity
Tune, motor and electromotor.
System the most according to claim 3, it is characterised in that described motor is adjusted by described electricity and controlled unit even with described flying
Connecing, described electricity is stealthily substituted and is included confirmation unit, and described confirmation unit is configured to obtain the certification coding of motor and by the certification of motor
The authentication information of motor prestored in coding and described confirmation unit is checked, and the certification at motor encodes and described confirmation form
When the authentication information of the motor prestored in unit is corresponding, the certification of the certification coding and electricity tune of uploading motor is encoded to described certification
Unit.
5. according to the system described in claim 1-4 any one claim, it is characterised in that described recognition unit also configures that use
In after the identity information collecting user's input first, the identity information of storage user, to carry out system of real name note to unmanned plane
Volume；Described recognition unit is also configured to after the identity information again collecting user's input, identity letter user inputted
Cease and check, to identify user identity with the information of system of real name registration in recognition unit.
6. a unmanned plane authentication method, it is characterised in that described method includes:
After the identity information collecting user's input, the identity of user is identified by recognition unit, certification after identifying successfully
Unit issues certification and asks and excite the authentication information prestored in authentication ' unit, and described authentication information is each of the unmanned plane that prestores
The unique identification information of individual parts and/or the identity information of all parts；
The certification flying to control all parts that unit reception certification is asked and collected unmanned plane encodes, and uploads described certification and is encoded to recognize
Card unit, carries unique identification information and/or the identity of all parts of all parts of unmanned plane in described certification coding
Information；
Authentication ' unit finds the certification coding corresponding with each authentication information, and is coded into corresponding certification by authentication information
Row verification, the most legal to determine the configuration of all parts of unmanned plane, and control unit transmission control instruction to described flying；And
Described flying controls the unit described control instruction of reception, and performs unmanned plane during flying operation or stopping according to described control instruction
Unmanned plane during flying operates.
Method the most according to claim 6, it is characterised in that described in fly to control the chip of all parts of unit and unmanned plane
Communication, and the certification coding of all parts is obtained from corresponding described chip.
Method the most according to claim 7, it is characterised in that the parts of unmanned plane include following at least one: battery, electricity
Tune, motor and electromotor.
Method the most according to claim 8, it is characterised in that described motor is adjusted by described electricity and controlled unit even with described flying
Connecing, described electricity is stealthily substituted and is included confirmation unit, and described confirmation unit obtains the certification coding of motor and the certification of motor encoded and institute
The authentication information stating the motor prestored in confirmation unit is checked, and the certification at motor encodes and prestores in described confirmation unit
The authentication information of motor corresponding time, upload the certification coding of motor and certification that electricity is adjusted be encoded to described authentication ' unit.
10. according to the method described in claim 6-9 any one claim, it is characterised in that collecting first, user is defeated
After the identity information entered, the identity information of described recognition unit storage user, to carry out system of real name registration to unmanned plane；Again
After collecting the identity information of user's input, the identity information that described recognition unit is also configured to input user is single with identification
In unit, the information of system of real name registration is checked, to identify user identity.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610544022.3A CN106060079A (en) | 2016-07-11 | 2016-07-11 | Unmanned aerial vehicle authentication system and method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610544022.3A CN106060079A (en) | 2016-07-11 | 2016-07-11 | Unmanned aerial vehicle authentication system and method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106060079A true CN106060079A (en) | 2016-10-26 |
Family
ID=57186744
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610544022.3A Pending CN106060079A (en) | 2016-07-11 | 2016-07-11 | Unmanned aerial vehicle authentication system and method |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106060079A (en) |
Cited By (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106598037A (en) * | 2016-12-13 | 2017-04-26 | 天津成周科技有限公司 | UAV identity recognition system based on electronic information UAV control |
| CN106714166A (en) * | 2016-12-23 | 2017-05-24 | 成都赫尔墨斯科技有限公司 | Anti-UAV method based on user authentication |
| CN107087440A (en) * | 2016-12-27 | 2017-08-22 | 深圳市大疆创新科技有限公司 | Information processing method and system, and unmanned plane control method and equipment |
| CN107426153A (en) * | 2017-04-13 | 2017-12-01 | 北京福瑞航行科技有限公司 | A kind of unmanned plane telecommunication network authentication mechanism and authentication method based on APP control terminals |
| CN107563183A (en) * | 2017-07-28 | 2018-01-09 | 翔升（上海）电子技术有限公司 | Unmanned aerial vehicle (UAV) control method, apparatus, equipment and computer-readable recording medium |
| WO2018121735A1 (en) * | 2016-12-31 | 2018-07-05 | 深圳市优必选科技有限公司 | Method and device for preventing loss of servo information |
| CN108377191A (en) * | 2018-02-24 | 2018-08-07 | 深圳市道通智能航空技术有限公司 | Battery discriminating method, unmanned plane and battery |
| CN108496332A (en) * | 2017-08-22 | 2018-09-04 | 深圳市大疆创新科技有限公司 | Auth method, equipment, machine readable storage medium and system |
| CN108496379A (en) * | 2017-05-23 | 2018-09-04 | 深圳市大疆创新科技有限公司 | Unmanned plane Activiation method, terminal, unmanned plane and machine readable storage medium |
| CN108702356A (en) * | 2017-05-19 | 2018-10-23 | 深圳市大疆创新科技有限公司 | Auth method, equipment, machine readable storage medium and system |
| CN109062253A (en) * | 2018-08-29 | 2018-12-21 | 广东电网有限责任公司 | Unmanned plane and unmanned plane management method |
| CN109076064A (en) * | 2017-10-31 | 2018-12-21 | 深圳市大疆创新科技有限公司 | Unmanned plane real name registration process method and system, server, terminal, management equipment |
| CN109116863A (en) * | 2018-08-24 | 2019-01-01 | 北京京东尚科信息技术有限公司 | Unmanned plane dispatching method, device, system, electronic equipment and readable medium |
| CN110012429A (en) * | 2018-01-05 | 2019-07-12 | 中国移动通信有限公司研究院 | Unmanned plane terminal identification method and network side equipment |
| CN110392049A (en) * | 2019-07-10 | 2019-10-29 | 同济大学 | Airborne unmanned plane identification module and real name identification method |
| CN110460811A (en) * | 2019-07-31 | 2019-11-15 | 视联动力信息技术股份有限公司 | A kind of multimedia data processing method and system based on view networking |
| CN110622466A (en) * | 2018-03-23 | 2019-12-27 | 深圳市大疆创新科技有限公司 | Control method, equipment and system |
| CN111460427A (en) * | 2020-02-26 | 2020-07-28 | 上海钧正网络科技有限公司 | Binding method and device of power supply equipment, storage medium and equipment |
| CN113033737A (en) * | 2017-10-09 | 2021-06-25 | 深圳市大疆创新科技有限公司 | Registration information processing method and system, terminal device and control device |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102396251A (en) * | 2009-04-15 | 2012-03-28 | 交互数字专利控股公司 | Validation and/or authentication of device for communication with network |
| US20140379173A1 (en) * | 2011-11-15 | 2014-12-25 | Insitu, Inc. | Controlled range and payload for unmanned vehicles, and associated systems and methods |
| CN105025014A (en) * | 2015-06-18 | 2015-11-04 | 顺丰科技有限公司 | Unmanned aerial vehicle commissioning method, system and device |
| US20160099969A1 (en) * | 2014-10-06 | 2016-04-07 | The Boeing Company | Enforcing policy compliance on a device |
-
2016
- 2016-07-11 CN CN201610544022.3A patent/CN106060079A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102396251A (en) * | 2009-04-15 | 2012-03-28 | 交互数字专利控股公司 | Validation and/or authentication of device for communication with network |
| US20140379173A1 (en) * | 2011-11-15 | 2014-12-25 | Insitu, Inc. | Controlled range and payload for unmanned vehicles, and associated systems and methods |
| US20160099969A1 (en) * | 2014-10-06 | 2016-04-07 | The Boeing Company | Enforcing policy compliance on a device |
| CN105025014A (en) * | 2015-06-18 | 2015-11-04 | 顺丰科技有限公司 | Unmanned aerial vehicle commissioning method, system and device |
Non-Patent Citations (1)
| Title |
|---|
| 陈娟等: "基于TPM的CPK信息安全认证研究", 《现代电子技术》 * |
Cited By (26)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106598037A (en) * | 2016-12-13 | 2017-04-26 | 天津成周科技有限公司 | UAV identity recognition system based on electronic information UAV control |
| CN106714166A (en) * | 2016-12-23 | 2017-05-24 | 成都赫尔墨斯科技有限公司 | Anti-UAV method based on user authentication |
| CN107087440A (en) * | 2016-12-27 | 2017-08-22 | 深圳市大疆创新科技有限公司 | Information processing method and system, and unmanned plane control method and equipment |
| CN107087440B (en) * | 2016-12-27 | 2019-04-19 | 深圳市大疆创新科技有限公司 | The control method and equipment of information processing method and system and unmanned plane |
| CN109302428A (en) * | 2016-12-27 | 2019-02-01 | 深圳市大疆创新科技有限公司 | The control method and equipment of unmanned plane |
| WO2018121735A1 (en) * | 2016-12-31 | 2018-07-05 | 深圳市优必选科技有限公司 | Method and device for preventing loss of servo information |
| CN107426153A (en) * | 2017-04-13 | 2017-12-01 | 北京福瑞航行科技有限公司 | A kind of unmanned plane telecommunication network authentication mechanism and authentication method based on APP control terminals |
| CN108702356A (en) * | 2017-05-19 | 2018-10-23 | 深圳市大疆创新科技有限公司 | Auth method, equipment, machine readable storage medium and system |
| WO2018209683A1 (en) * | 2017-05-19 | 2018-11-22 | 深圳市大疆创新科技有限公司 | Identify authentication method and device, machine readable storage medium, and system |
| CN108496379B (en) * | 2017-05-23 | 2021-08-31 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle activation method, terminal, unmanned aerial vehicle and machine-readable storage medium |
| CN108496379A (en) * | 2017-05-23 | 2018-09-04 | 深圳市大疆创新科技有限公司 | Unmanned plane Activiation method, terminal, unmanned plane and machine readable storage medium |
| CN107563183A (en) * | 2017-07-28 | 2018-01-09 | 翔升（上海）电子技术有限公司 | Unmanned aerial vehicle (UAV) control method, apparatus, equipment and computer-readable recording medium |
| CN108496332A (en) * | 2017-08-22 | 2018-09-04 | 深圳市大疆创新科技有限公司 | Auth method, equipment, machine readable storage medium and system |
| CN113033737A (en) * | 2017-10-09 | 2021-06-25 | 深圳市大疆创新科技有限公司 | Registration information processing method and system, terminal device and control device |
| CN109076064A (en) * | 2017-10-31 | 2018-12-21 | 深圳市大疆创新科技有限公司 | Unmanned plane real name registration process method and system, server, terminal, management equipment |
| CN110012429B (en) * | 2018-01-05 | 2021-01-15 | 中国移动通信有限公司研究院 | Unmanned aerial vehicle terminal identification method and network side equipment |
| CN110012429A (en) * | 2018-01-05 | 2019-07-12 | 中国移动通信有限公司研究院 | Unmanned plane terminal identification method and network side equipment |
| CN108377191A (en) * | 2018-02-24 | 2018-08-07 | 深圳市道通智能航空技术有限公司 | Battery discriminating method, unmanned plane and battery |
| WO2019161674A1 (en) * | 2018-02-24 | 2019-08-29 | 深圳市道通智能航空技术有限公司 | Battery recognition method, unmanned aerial vehicle and battery |
| CN110622466A (en) * | 2018-03-23 | 2019-12-27 | 深圳市大疆创新科技有限公司 | Control method, equipment and system |
| CN110622466B (en) * | 2018-03-23 | 2023-05-16 | 深圳市大疆创新科技有限公司 | Control method, equipment and system |
| CN109116863A (en) * | 2018-08-24 | 2019-01-01 | 北京京东尚科信息技术有限公司 | Unmanned plane dispatching method, device, system, electronic equipment and readable medium |
| CN109062253A (en) * | 2018-08-29 | 2018-12-21 | 广东电网有限责任公司 | Unmanned plane and unmanned plane management method |
| CN110392049A (en) * | 2019-07-10 | 2019-10-29 | 同济大学 | Airborne unmanned plane identification module and real name identification method |
| CN110460811A (en) * | 2019-07-31 | 2019-11-15 | 视联动力信息技术股份有限公司 | A kind of multimedia data processing method and system based on view networking |
| CN111460427A (en) * | 2020-02-26 | 2020-07-28 | 上海钧正网络科技有限公司 | Binding method and device of power supply equipment, storage medium and equipment |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106060079A (en) | Unmanned aerial vehicle authentication system and method | |
| US20180160285A1 (en) | Information processing system for mobile object, server for managing mobile object, information communication terminal and mobile object | |
| CN107087440B (en) | The control method and equipment of information processing method and system and unmanned plane | |
| CN106774415A (en) | Unmanned plane, unmanned plane battery change method, device and UAS | |
| US11655046B2 (en) | Safety management system for aircraft | |
| CN109034425A (en) | Substation secondary device maintenance safety managing and control system and method based on Internet of Things | |
| CN107038462B (en) | Equipment control operation method and system | |
| CN107105051A (en) | A kind of off-line type aircraft monitoring method and supervising device based on cloud service | |
| CN107799171A (en) | Information processing method, apparatus and system, storage medium, equipment and server | |
| CN110348755B (en) | Unmanned aerial vehicle full life cycle management system and method | |
| CN105450646A (en) | Local area network connection realization method for network refrigerator and user information security authentication method | |
| CN105128818A (en) | Multistage-identity-authentication car remote controlled key and work method thereof | |
| CN105740663A (en) | Portable password input equipment and control method thereof | |
| CN108037900B (en) | Remote and safe printing method and device of multifunctional printer | |
| CN107563183A (en) | Unmanned aerial vehicle (UAV) control method, apparatus, equipment and computer-readable recording medium | |
| US9652966B2 (en) | Jumpers and methods of making and using same | |
| CN106548323A (en) | The recommendation method and airspace management system of unmanned plane driver | |
| CN110561444B (en) | Airport robot service system and method and computer storage medium | |
| WO2017059174A1 (en) | System and method to control access to hazardous machines | |
| CN109086848A (en) | Clean the localization method and system of unmanned plane | |
| JP6523069B2 (en) | Autonomous moving body management device, autonomous moving body management system, autonomous moving body management method, and program | |
| CN111627138B (en) | Electrostatic discharge method and system, storage medium and electronic device | |
| CN112218523A (en) | Method for controlling operation of garden tool and battery pack | |
| CN105550755A (en) | Vehicle maintenance strategy execution method and system and electronic equipment | |
| US11227455B2 (en) | Distributed cloning tool assembly, system, and method for replication of vehicle access devices |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| TA01 | Transfer of patent application right | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20210722 Address after: 518063 5th floor, block B, building 1, software industry base, Yuehai street, Nanshan District, Shenzhen City, Guangdong Province Applicant after: Fengyi Technology (Shenzhen) Co.,Ltd. Address before: 518061 Intersection of Xuefu Road (south) and Baishi Road (east) in Nanshan District, Shenzhen City, Guangdong Province, 6-13 floors, Block B, Shenzhen Software Industry Base Applicant before: SF TECHNOLOGY Co.,Ltd. |
|
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20161026 |