CN103699826A - Identity authentication method and device for airborne information system - Google Patents
Identity authentication method and device for airborne information system Download PDFInfo
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- CN103699826A CN103699826A CN201310695609.0A CN201310695609A CN103699826A CN 103699826 A CN103699826 A CN 103699826A CN 201310695609 A CN201310695609 A CN 201310695609A CN 103699826 A CN103699826 A CN 103699826A
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F21/00—Security arrangements for protecting computers, components thereof, programs or data against unauthorised activity
- G06F21/30—Authentication, i.e. establishing the identity or authorisation of security principals
- G06F21/31—User authentication
- G06F21/32—User authentication using biometric data, e.g. fingerprints, iris scans or voiceprints
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F2221/00—Indexing scheme relating to security arrangements for protecting computers, components thereof, programs or data against unauthorised activity
- G06F2221/21—Indexing scheme relating to G06F21/00 and subgroups addressing additional information or applications relating to security arrangements for protecting computers, components thereof, programs or data against unauthorised activity
- G06F2221/2141—Access rights, e.g. capability lists, access control lists, access tables, access matrices
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Abstract
The invention discloses an identity authentication method for an airborne information system. The identity authentication method for the airborne information system comprises generating user configuration information which comprises every user identity and corresponding authority configuration in a ground terminal; enabling an aircraft terminal to receive guided user configuration information; receiving identity information which is input through users; opening authorities which are corresponding to the input identity information according to received identity information. The invention also discloses an identity authentication device for the airborne information system. The identity authentication method and the system for the airborne information system enable authentication of the users to be achieved onboard and improves airplane safety.
Description
Technical field
The present invention relates to a kind of identity identifying method for airborne infosystem and device.
Background technology
At present, airborne infosystem is brought into use from B787, A380 new architecture, the authentication application of under this airborne circumstance, the airborne application person of conducting interviews identity being differentiated there is no, and existing access rights control is to present corresponding accessible content according to user's autonomous selection, the type of authority is actual is to be decided by user behavior, and user behavior itself is uncontrolled, so in fact user's access is not carried out effectively accurately and controlled.Disabled user can normally access like this, and user can select unauthorized access by self arbitrarily, and the use of airborne application is completely not controlled.
Singularity due to airborne infosystem, in mobile system, identity is limited to the restriction that is subject to network, cannot share consolidated network with ground-based server aboard, and if user is not carried out to authentication and right assignment, easily cause some potential safety hazards of aircraft.Therefore, when user's identity is authenticated or limited, how can carry out conveniently, simple and direct carry out authentication, success is aviation field one urgent problem at present.
Summary of the invention
The technical matters that the present invention mainly solves is to provide a kind of identity identifying method for airborne infosystem and device, can solve the problem existing in background technology.
For solving the problems of the technologies described above, the technical scheme that the present invention adopts is: a kind of identity identifying method for airborne infosystem is provided, comprises: the user configuration information that generates each user identity and the configuration of corresponding authority in ground surface end; In aircraft termination, receive the user configuration information importing; Receive the identity information of user's input; According to the identity information receiving, open and the corresponding authority of identity information of inputting.
Wherein, the step that generates the user configuration information of each user identity and corresponding authority configuration in ground surface end comprises: the identity registration information that receives each user; The authority corresponding according to each user's who receives identity registration information configuration; According to the authority information of each identity registration information and configuration, generate the user configuration information of user identity and authority configuration; And derivation user configuration information.
Wherein, the identity information of described reception user input refers to the identity request information that receives user's input;
In the step of the corresponding authority information of identity information of opening and inputting according to the identity information receiving, comprising: the identity request information receiving is authenticated; The identity request information of authentication success is opened and the corresponding authority of this identity request information.
Wherein, in the step that the identity request information receiving is authenticated, comprising: in user configuration information, search the identity information matching with this identity request information; Judge whether to find the identity information matching with this identity request information; If find the identity information matching with this identity request information, search the authority configuration information matching with this identity information.
Wherein, described identity is the unique identification information for identifying user feature, and described identity comprises: username and password, user's palmmprint, iris, face, auricle, voice vocal print, fingerprint and/or the fingers/hand palm/hand back vein distribute.
For solving the problems of the technologies described above, another technical solution used in the present invention is: a kind of identification authentication system for airborne infosystem is provided, comprise: be positioned at the generation module of ground surface end, for generating the user configuration information of each user identity and the configuration of corresponding authority; Be positioned at the importing module of aircraft end, for receive the user configuration information importing in aircraft termination; Be positioned at the first receiver module of aircraft end, for receiving the identity information of user's input; And the authority opening module that is positioned at aircraft end, for opening and the corresponding authority of identity information of inputting according to the identity information receiving.
Wherein, described generation module comprises: the second receiver module, for receiving each user's identity registration information; Configuration module, each user's who receives for basis authority corresponding to identity registration information configuration; User configuration information generation module, for generating the user configuration information of user identity and authority configuration according to the authority information of each identity registration information and configuration; And derivation module, for deriving user configuration information.
Wherein, described the first receiver module, also for receiving the identity request information of user's input; Described authority opening module comprises: authentication module, authenticates for the identity request information to receiving; Authority is opened submodule, for the identity request information to authentication success, opens and the corresponding authority of this identity request information.
Wherein, described authentication module comprises: first searches module, for search the identity information matching with this identity request information at user configuration information; Judge module, for judging whether to find the identity information matching with identity request information; Second searches module, for obtaining finding after the identity information matching with this identity request information in judge module judgement, searches the authority configuration information matching with this identity information; Described authority is opened submodule, also for according to second search module searches to authority configuration information open corresponding authority.
Wherein, described identity is the unique identification information for identifying user feature, and described identity comprises: username and password, user's palmmprint, iris, face, auricle, voice vocal print, fingerprint and/or the fingers/hand palm/hand back vein distribute.
The invention has the beneficial effects as follows: the situation that is different from prior art, identity identifying method for airborne infosystem of the present invention and device, can be by create or generate the user configuration information that contains user identity and authority configuration in ground surface end, by ground user configuration information import in aircraft, so that can user be carried out the management of authority and authority is classified aboard, further make the user with some authority just can carry out operating accordingly with this authority, do not have the user of operating right can not operate some application software on aircraft or other devices, and then the security that has improved aircraft.
Accompanying drawing explanation
In order to be illustrated more clearly in the embodiment of the present invention or technical scheme of the prior art, to the accompanying drawing of required use in embodiment or description of the Prior Art be briefly described below, apparently, accompanying drawing in the following describes is only some embodiments of the present invention, for those of ordinary skills, do not paying under the prerequisite of creative work, can also obtain according to these accompanying drawings other accompanying drawing.
Fig. 1 is that the present invention is for the process flow diagram of identity identifying method one embodiment of airborne infosystem;
Fig. 2 is that the present invention generates the process flow diagram of user configuration information step for identity identifying method one embodiment of airborne infosystem;
To be the present invention open the process flow diagram of authority step for identity identifying method one embodiment of airborne infosystem to Fig. 3;
Fig. 4 is that the present invention is for the process flow diagram of the identity identifying method one embodiment identity request authenticating step of airborne infosystem;
Fig. 5 is that the present invention is for the block scheme of identification authentication system one embodiment of airborne infosystem;
Fig. 6 is that the present invention is for the block scheme of the identification authentication system one embodiment generation module of airborne infosystem;
Fig. 7 is that the present invention is for the block scheme of the identification authentication system one embodiment authority opening module of airborne infosystem;
Fig. 8 is that the present invention is for the block scheme of the identification authentication system one embodiment authentication module of airborne infosystem.
Embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is clearly and completely described, obviously, described embodiment is only the present invention's part embodiment, rather than whole embodiment.Embodiment based in the present invention, those of ordinary skills, not making the every other embodiment obtaining under creative work prerequisite, belong to the scope of protection of the invention.
Before embodiment is described, need to make an explanation to some necessary terms.For example:
If occur, use the terms such as " first ", " second " to describe various elements herein, but these elements should not limited by these terms.These terms are only used for distinguishing an element and another element.Therefore " first " element of, below discussing also can be called as " second " element and not depart from instruction of the present invention.It should be understood that, if while mentioning an element " connection " or " connection " to another element, can directly connect or directly be connected to another element or also can have intermediary element.On the contrary, when mentioning that an element " directly connects " or " directly connecting " arrives another element, there is not intermediary element.
The various terms that occur in this article are only not intended to as limitation of the invention for describing the object of concrete embodiment, unless context clearly point out in addition, otherwise singulative intention also comprises plural form.
When using in this manual term " to comprise " and/or when " including ", these terms have indicated the existence of described feature, integral body, step, operation, element and/or parts, but also do not get rid of the existence of above other features, integral body, step, operation, element, parts and/or its group and/or add.
About embodiment:
Refer to Fig. 1, Fig. 1 be the present invention for the identity identifying method of airborne infosystem, comprising:
S101, in ground surface end, generate the user configuration information of each user identity and corresponding authority configuration;
Described ground surface end can be server, computing machine etc., wherein, and the computing machine that indication computing machine is broad sense herein, make a general reference a kind of robot calculator device for supercomputing, it can carry out numerical evaluation, can carry out logical calculated again, also has store-memory function.To move according to program, automatically, the modernization intelligent electronic device of high speed processing mass data.Hardware system and software systems, consisted of, the computing machine that any software is not installed is called bare machine.For example desktop computer, notebook, PDA, mobile phone, panel computer etc. are all comprised in computing machine.
User includes but not limited to: aircraft maintainers, pilot, crew member etc.
Refer to Fig. 2, the described user configuration information that generates the configuration of each user identity and corresponding authority in ground surface end comprises following sub-step:
1011, receive each user's identity registration information;
Described identity refers to the unique identification information for identifying user feature, and for example identity can include but not limited to: username and password, user's palmmprint, iris, face, auricle, voice vocal print, fingerprint and/or the fingers/hand palm/hand back vein distribute etc.
User can pass through the input username and passwords such as physical button, touch-screen, Speech input with registered user's identity; Can pass through the special-purpose recognition device such as palmmprint, iris, face, auricle, voice vocal print, fingerprint, the distribution of the fingers/hand palm/hand back vein with identity of registered user etc.
1012, according to each user's who receives authority corresponding to identity registration information configuration;
Described authority can include but not limited to administrator right and domestic consumer's authority, for example can aircraft maintainers be set to administrator right, pilot is set to common authority; Administrator right be superior to common authority, the content that the user that authority is higher can check or operate is more, for example out-of-limit high user, also more to the authority of access, inquiry or the operation of relative application software on aircraft etc.; Out-of-limit low user reduces accordingly in the authority of some access, inquiry or operation.Described application software can be but be not limited to be that data load software (loading aboard the data of other equipment); Archive files produces application software etc.
1013, according to the authority information of each identity registration information and configuration, generate the user configuration information of user identity and authority configuration;
Described each identity registration information is associated with the authority information of configuration, and each log-on message closes bind by one and points to authority information, so that when follow-up input identity information, can find fast the authority information being associated with this identity information.
1014, derive user configuration information.
By automatic or manual derivation user configuration information, when derivation configuration information by manual, first receive the derivation command information of user's input, according to deriving command information, send derivation action command, according to deriving action command, user configuration information is derived.
This user configuration information can cause to a mobile storage means, then is directed in the corresponding system in aircraft by mobile storage means.
S102, the user configuration information importing in aircraft termination receipts;
This step can be automatic or manual import user configuration information, automatically importing can be when new equipment being detected, in search equipment, meet certain pre-conditioned file, when meeting certain when pre-conditioned, be that this document is set as user configuration information, send importing action command, user profile is directed in the system of aircraft end according to described importing action command;
When being manually importing, according to the importing order of user's input, send importing action command, user profile is fed in the system of aircraft end according to importing action command.
In the time of in first importing aircraft end, can load user configuration information by initial user.First loading after user configuration information, also can arrange one and be exclusively used in the keeper who manages aircraft end subscriber configuration information, with when user changes, user configuration information is reloaded.
The identity information of S103, reception user input;
Wherein, the identity information of described reception user input, refers to the identity request information that user inputs; When identity is username and password, identity request information is the login of username and password; When identity is palmmprint, vocal print etc., identity request information is the input log-on message of sound, palm.
S104, the corresponding authority of identity information of opening and inputting according to the identity information receiving.
Wherein, refer to Fig. 3, the identity information that described basis receives is opened with the corresponding authority of identity information of inputting and is comprised following sub-step:
S1041, the identity request information receiving is authenticated; Wherein, refer to Fig. 4, this step also comprises following sub-step:
S10411, in user configuration information, search the identity information matching with this identity request information;
When generating user configuration information, identity information is carried out associated with authority configuration information, in this step, as long as the identity request information of input can be mated with the identity information in user configuration information, can find by associated identity information permission match information.
S10412, judge whether to find the identity information matching with this identity request information; The identity information matching if find, enters S10413 step, and the identity information matching if do not find proceeds to S10414 step;
If S10413 finds the identity information matching with this identity request information, search the authority configuration information matching with this identity information.
S10414, end.End herein, if refer to, do not find the identity information matching, mean not this user's log-on message, do not have log-on message to represent that the user of this identity request does not have corresponding authority information, do not have corresponding authority not carry out follow-up any processing; Certainly, in certain embodiments, if do not have corresponding identity information and authority can point out step etc.
S1042, the unlatching of identity request information and the corresponding authority of this identity request information to authentication success.
Embodiment of the present invention, by create or generate the user configuration information that contains user identity and authority configuration in ground surface end, by ground user configuration information import in aircraft, so that can user be carried out the management of authority and authority is classified aboard, further make the user with some authority just can carry out operating accordingly with this authority, do not have the user of operating right can not operate some application software on aircraft or other devices, and then improved the security of aircraft.
Refer to Fig. 5, Fig. 5 is that the present invention is for the block scheme of identification authentication system one embodiment of airborne infosystem.The present embodiment comprises for the identification authentication system of airborne infosystem:
Be positioned at ground surface end 10 generation module 101, be positioned at aircraft end 20 importing module 201, be positioned at the first receiver module 202 of aircraft end 20 and the authority opening module 203 that is positioned at aircraft end 20.Wherein:
Described generation module 101, for generating the user configuration information of each user identity and the configuration of corresponding authority; Described identity refers to the unique identification information for identifying user feature, and for example identity can include but not limited to: username and password, user's palmmprint, iris, face, auricle, voice vocal print, fingerprint and/or the fingers/hand palm/hand back vein distribute etc.User can pass through the input username and passwords such as physical button, touch-screen, Speech input with registered user's identity; Can pass through the special-purpose recognition device such as palmmprint, iris, face, auricle, voice vocal print, fingerprint, the distribution of the fingers/hand palm/hand back vein with identity of registered user etc.
Particularly, described generation module 101 comprises:
The second receiver module 1011, for receiving each user's identity registration information;
Described authority can include but not limited to administrator right and domestic consumer's authority, for example can aircraft maintainers be set to administrator right, pilot is set to common authority; Administrator right be superior to common authority, the content that the user that authority is higher can check or operate is more, for example out-of-limit high user, also more to the authority of access, inquiry or the operation of relative application software on aircraft etc.; Out-of-limit low user reduces accordingly in the authority of some access, inquiry or operation.Described application software can be but be not limited to be that data load software (loading aboard the data of other equipment); Archive files produces application software etc.
User configuration information generation module 1013, for generating the user configuration information of user identity and authority configuration according to the authority information of each identity registration information and configuration; Wherein:
Described each identity registration information is associated with the authority information of configuration, and each log-on message closes bind by one and points to authority information, so that when follow-up input identity information, can find fast the authority information being associated with this identity information.
Derive module 1014, for deriving user configuration information.Wherein:
By automatic or manual derivation user configuration information, when derivation configuration information by manual, first receive the derivation command information of user's input, according to deriving command information, send derivation action command, according to deriving action command, user configuration information is derived.This user configuration information can cause to a mobile storage means, then is directed in the corresponding system in aircraft by mobile storage means.
Described the first receiver module 202, for receiving the identity information of user's input; Particularly, the identity information of described reception user input, refers to the identity request information that user inputs; When identity is username and password, identity request information is the login of username and password; When identity is palmmprint, vocal print etc., identity request information is the input log-on message of sound, palm.
Described authority opening module 203, for opening and the corresponding authority of identity information of inputting according to the identity information receiving.Wherein:
Described authority opening module 203 comprises:
Authority is opened submodule 2032, for the identity request information to authentication success, opens and the corresponding authority of this identity request information.Particularly, described authority is opened submodule, for searching according to second the authority configuration information that module 20313 finds, opens corresponding authority.
Embodiment of the present invention, by create or generate the user configuration information that contains user identity and authority configuration in ground surface end, by ground user configuration information import in aircraft, so that can user be carried out the management of authority and authority is classified aboard, further make the user with some authority just can carry out operating accordingly with this authority, do not have the user of operating right can not operate some application software on aircraft or other devices, and then improved the security of aircraft.
These are only embodiments of the present invention; not thereby limit the scope of the claims of the present invention; every equivalent structure or conversion of equivalent flow process that utilizes instructions of the present invention and accompanying drawing content to do; or be directly or indirectly used in other relevant technical fields, be all in like manner included in scope of patent protection of the present invention.
Claims (10)
1. for an identity identifying method for airborne infosystem, comprising:
In ground surface end, generate the user configuration information of each user identity and the configuration of corresponding authority;
In aircraft termination, receive the user configuration information importing;
Receive the identity information of user's input;
According to the identity information receiving, open and the corresponding authority of identity information of inputting.
2. the identity identifying method for airborne infosystem as claimed in claim 1, is characterized in that, the step that generates the user configuration information of each user identity and the configuration of corresponding authority in ground surface end comprises:
Receive each user's identity registration information;
The authority corresponding according to each user's who receives identity registration information configuration;
According to the authority information of each identity registration information and configuration, generate the user configuration information of user identity and authority configuration; And
Derive user configuration information.
3. the identity identifying method for airborne infosystem as claimed in claim 2, is characterized in that,
The identity information of described reception user input refers to the identity request information that receives user's input;
In the step of the corresponding authority information of identity information of opening and inputting according to the identity information receiving, comprising:
The identity request information receiving is authenticated;
The identity request information of authentication success is opened and the corresponding authority of this identity request information.
4. the identity identifying method for airborne infosystem as claimed in claim 3, is characterized in that, in the step that the identity request information receiving is authenticated, comprising:
In user configuration information, search the identity information matching with this identity request information;
Judge whether to find the identity information matching with this identity request information;
If find the identity information matching with this identity request information, search the authority configuration information matching with this identity information.
5. the identity identifying method for airborne infosystem as described in any one claim in claim 1 to 4, is characterized in that:
Described identity is the unique identification information for identifying user feature, and described identity comprises: username and password, user's palmmprint, iris, face, auricle, voice vocal print, fingerprint and/or the fingers/hand palm/hand back vein distribute.
6. for an identification authentication system for airborne infosystem, comprising:
Be positioned at the generation module of ground surface end, for generating the user configuration information of each user identity and the configuration of corresponding authority;
Be positioned at the importing module of aircraft end, for receive the user configuration information importing in aircraft termination;
Be positioned at the first receiver module of aircraft end, for receiving the identity information of user's input;
And the authority opening module that is positioned at aircraft end, for opening and the corresponding authority of identity information of inputting according to the identity information receiving.
7. the identification authentication system for airborne infosystem as claimed in claim 6, is characterized in that:
Described generation module comprises:
The second receiver module, for receiving each user's identity registration information;
Configuration module, each user's who receives for basis authority corresponding to identity registration information configuration; User configuration information generation module, for generating the user configuration information of user identity and authority configuration according to the authority information of each identity registration information and configuration; And
Derive module, for deriving user configuration information.
8. the identification authentication system for airborne infosystem as claimed in claim 7, is characterized in that:
Described the first receiver module, also for receiving the identity request information of user's input;
Described authority opening module comprises:
Authentication module, authenticates for the identity request information to receiving;
Authority is opened submodule, for the identity request information to authentication success, opens and the corresponding authority of this identity request information.
9. the identification authentication system for airborne infosystem as claimed in claim 8, is characterized in that:
Described authentication module comprises:
First searches module, for search the identity information matching with this identity request information at user configuration information;
Judge module, for judging whether to find the identity information matching with identity request information;
Second searches module, for obtaining finding after the identity information matching with this identity request information in judge module judgement, searches the authority configuration information matching with this identity information;
Described authority is opened submodule, also for according to second search module searches to authority configuration information open corresponding authority.
10. the identification authentication system for airborne infosystem as described in any one claim in claim 6 to 9, is characterized in that:
Described identity is the unique identification information for identifying user feature, and described identity comprises: username and password, user's palmmprint, iris, face, auricle, voice vocal print, fingerprint and/or the fingers/hand palm/hand back vein distribute.
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| CN104392723A (en) * | 2014-12-03 | 2015-03-04 | 厦门大学 | Sharing instrument platform management method based on voiceprint recognition technology |
| CN104991563A (en) * | 2015-05-12 | 2015-10-21 | 零度智控（北京）智能科技有限公司 | Graded unmanned plane operating method and system |
| CN105975826A (en) * | 2016-04-20 | 2016-09-28 | 中国石油大学(华东) | Enterprise economic management information security system |
| CN112542156A (en) * | 2020-12-08 | 2021-03-23 | 山东航空股份有限公司 | Civil aviation maintenance worker card system based on voiceprint recognition and voice instruction control |
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