CN109740942A - Method and management system are managed independently in spacecraft energy resource system safety - Google Patents
Method and management system are managed independently in spacecraft energy resource system safety Download PDFInfo
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- CN109740942A CN109740942A CN201910007120.7A CN201910007120A CN109740942A CN 109740942 A CN109740942 A CN 109740942A CN 201910007120 A CN201910007120 A CN 201910007120A CN 109740942 A CN109740942 A CN 109740942A
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Abstract
The present invention relates to a kind of spacecraft energy resource system safeties to manage independently method, comprising steps of the state value of a. timing acquiring spacecraft energy resource system；B. with the presence or absence of the factor for influencing spacecraft state in timing detection spacecraft energy resource system；C. the data generated in a step and in the b step are handled；D. the processing result in the step c is analyzed, processing method is provided, abnormal problem is disposed.Management method and management system according to the present invention, are greatly reduced the time of energy resource system anomaly, improve the speed disposed extremely.The link manually participated in is greatly reduced in this method, has saved human cost.
Description
Technical field
The present invention relates to the invention belongs to space flight electric field more particularly to a kind of spacecraft energy resource system safety are autonomous
Management method and management system.
Background technique
With the continuous growth of spacecraft time in orbit, the time in observing and controlling area is not lengthened gradually yet, this is to space flight
More stringent requirements are proposed for the autonomous management ability of device.The energy resource system system one of the most key as spacecraft, it is autonomous
Managerial ability decides the task execution success or failure of entire spacecraft.The most basic requirement of autonomous management is ensuring that the peace of spacecraft
Entirely, the present invention is based on this purpose to propose a kind of energy resource system safety autonomous management method.
The autonomous management of spacecraft energy resource system is the expansion based on autonomous monitor in real time to spacecraft current state, and
There are many factors for influencing spacecraft state.In order to efficiently and accurately judge whether spacecraft energy resource system is in abnormal shape
State is quickly effectively disposed, and needs to carry out influence factor combing classification comprehensively, and reasonable autonomous investigation and processing is arranged
Process guarantees that spacecraft can be restored to normal condition in the shortest time.
In order to realize the recovery of spacecraft energy resource system abnormality, traditional way is joined by artificial interpretation correlation
Number determines the position that occurs extremely, analyzes abnormal Producing reason, then further according to analysis as a result, formulate corresponding scheme into
Row restores.The shortcomings that this way, mainly includes two aspects that the real-time of 1. artificial interpretation cannot ensure, due to long-term in-orbit fortune
Capable spacecraft have for a long time operates in outside observing and controlling area, data can not timely downlink, enter observing and controlling area after, in magnanimity
Abnormal data is found in information to be also required to take a long time.After this will lead to the abnormal generation some time, it can not also position and ask
Topic is disposed.2. comprehensive cannot ensure, artificial interpretation, when note abnormalities parameter after, it will usually stop continue interpretation, hurry
It is abnormal in positioning, it is disposed.If many places anomaly parameter occurs in the same time, exception later can be ignored, and may lead
It causes more serious exception not find in first time, delays abnormal disposition.
Summary of the invention
The purpose of the present invention is to solve the above problem, provides a kind of spacecraft energy resource system safety autonomous management method
And management system, it realizes to the promptly and accurately positioning of failure and from main process task.
For achieving the above object, the present invention provides a kind of spacecraft energy resource system safety autonomous management method, packet
Include following steps:
A. the state value of timing acquiring spacecraft energy resource system；
B. with the presence or absence of the factor for influencing spacecraft state in timing detection spacecraft energy resource system；
C. the data generated in a step and in the b step are handled；
D. the processing result in the step c is analyzed, processing method is provided, abnormal problem is disposed.
According to an aspect of the present invention, in a step, state parameter list L, the parameter energy in the list are established
Enough reflect that the institute of spacecraft energy resource system is stateful.
According to an aspect of the present invention, in the b step, influence factor list S is established, is covered in the list all
The influence factor of the state parameter of spacecraft energy resource system can be changed.
According to an aspect of the present invention, in the step c, pair of the state parameter Yu the influence factor is established
It should be related to, when the change of all state parameters can find corresponding influence factor, enable f (V, Ω)=0；
When the change for having at least one state parameter, when can not find corresponding influence factor, it is considered as energy resource system
At least one exception is produced, this season f (V, Ω)=exception number, whereinHad an impact by what is generated in this period
The set of factor, V are the collection value of all state parameters in list L in this period.
According to an aspect of the present invention, in the Step d, problem disposition library H is established, all exceptions is saved in library and asks
The solution of topic.
According to an aspect of the present invention, the period of setting influence factor detection and the period of state parameter acquisition, each
Period sends one group of V and Ω value into the step c, then filters out all status parameter values X that can not find corresponding relationship,
WhereinAnd the value n for representing abnormal problem quantity is generated, then X and n are sent in the Step d
It sets.
According to an aspect of the present invention, according to X and n, at least one solution is found in described problem disposition library H and is arranged
It applies, and driven computer is handled.
For achieving the above object, the present invention also provides a kind of realization spacecraft energy resource system safety autonomous management sides
The management system of method, comprising:
Clock module is used for setting time；
State acquisition module, according to the time that the clock module is set, the state of timing acquiring spacecraft energy resource system
Value；
Influence factor module, according to the clock module set time, timing detect spacecraft energy resource system in whether
In the presence of the factor for influencing spacecraft state；
State and influence factor comprehensive analysis module are received and are sent out by the state acquisition module and the influence factor module
The real time data sent, and the data received are handled；
Problem disposes module, receives the data processed result sent by the state and influence factor comprehensive analysis module,
And result is analyzed, processing method is provided, abnormal problem is disposed.
According to an aspect of the present invention, state parameter list L is established, the parameter in the list L is able to reflect space flight
The institute of device energy resource system is stateful, and the list L is stored in the state acquisition module.
According to an aspect of the present invention, influence factor list S is established, covering in the list S all can change space flight
The influence factor of the state parameter of device energy resource system, the list S are stored in the influence factor module.
According to an aspect of the present invention, the corresponding relationship f for establishing the state parameter Yu the influence factor, when all
When the change of state parameter can find corresponding influence factor, f (V, Ω)=0 is enabled；
When the change for having at least one state parameter, when can not find corresponding influence factor, it is considered as energy resource system
At least one exception is produced, this season f (V, Ω)=exception number, whereinHad an impact by what is generated in this period
The set of factor, V are the collection value of all state parameters in list L in this period；
The corresponding relationship f is stored in the state and influence factor comprehensive analysis module.
According to an aspect of the present invention, problem disposition library H is established, the solution of all abnormal problems is saved in library,
Described problem disposition library H is stored in described problem disposition module.
According to an aspect of the present invention, the clock module gives period and the state parameter acquisition of influence factor detection
Period, in each period, the influence factor module and the state acquisition module can be comprehensive to the state and influence factor
Analysis module sends one group of V and Ω value, and the state and influence factor comprehensive analysis module can filter out nothing according to the value received
Method finds all status parameter values X of corresponding relationship, whereinAnd the value n for representing abnormal problem quantity is generated, so
X, n are sent to described problem disposition module afterwards.
According to an aspect of the present invention, described problem disposition module is disposed in the H of library according to the value of X and n in described problem
At least one solution is found, and driven computer is handled.
The time of energy resource system anomaly is greatly reduced in management method and management system according to the present invention, improves
The speed of abnormal disposition.The link manually participated in is greatly reduced in this method, has saved human cost.
Detailed description of the invention
It in order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, below will be to institute in embodiment
Attached drawing to be used is needed to be briefly described, it should be apparent that, the accompanying drawings in the following description is only some implementations of the invention
Example, for those of ordinary skill in the art, without creative efforts, can also obtain according to these attached drawings
Obtain other attached drawings.
Fig. 1 schematically shows a kind of spacecraft energy resource system safety autonomous management side of embodiment according to the present invention
The flow chart of method.
Specific embodiment
It, below will be to embodiment in order to illustrate more clearly of embodiment of the present invention or technical solution in the prior art
Needed in attached drawing be briefly described.It should be evident that the accompanying drawings in the following description is only of the invention some
Embodiment for those of ordinary skills without creative efforts, can also be according to these
Attached drawing obtains other attached drawings.
When being described for embodiments of the present invention, term " longitudinal direction ", " transverse direction ", "upper", "lower", " preceding ",
" rear ", "left", "right", "vertical", "horizontal", "top", "bottom" "inner", orientation or positional relationship expressed by "outside" are based on phase
Orientation or positional relationship shown in the drawings is closed, is merely for convenience of description of the present invention and simplification of the description, rather than instruction or dark
Show that signified device or element must have a particular orientation, be constructed and operated in a specific orientation, therefore above-mentioned term cannot
It is interpreted as limitation of the present invention.
The present invention is described in detail with reference to the accompanying drawings and detailed description, embodiment cannot go to live in the household of one's in-laws on getting married one by one herein
It states, but therefore embodiments of the present invention are not defined in following implementation.
Fig. 1 schematically shows a kind of spacecraft energy resource system safety autonomous management side of embodiment according to the present invention
The flow chart of method.As shown in Figure 1, spacecraft energy resource system safety autonomous management method according to the present invention includes following step
It is rapid:
A. the state value of timing acquiring spacecraft energy resource system；
B. with the presence or absence of the factor for influencing spacecraft state in timing detection spacecraft energy resource system；
C. the data generated in a step and in the b step are handled；
D. the processing result in the step c is analyzed, processing method is provided, abnormal problem is disposed.
A kind of embodiment according to the present invention establishes state parameter list L, the ginseng in the list in above-mentioned a step
The institute that number is able to reflect spacecraft energy resource system is stateful.
In above-mentioned b step, influence factor list S is established, covering in the list all can change spacecraft energy resource system
State parameter influence factor.Influence factor herein refers exclusively to positive influences factor, the program control command that had both correctly issued, remote control
Instruction etc.；Negative effect factor, single-particle inversion as caused by space environment etc. is not in the list.
In above-mentioned step c, establish the corresponding relationship of state parameter and influence factor, when all state parameters change all
When can find corresponding influence factor, f (V, Ω)=0 is enabled；
When the change for having at least one state parameter, when can not find corresponding influence factor, it is considered as energy resource system
At least one exception is produced, this season f (V, Ω)=exception number, whereinHad an impact by what is generated in this period
The set of factor, V are the collection value of all state parameters in list L in this period.
In above-mentioned Step d, problem disposition library H is established, the solution of all abnormal problems is saved in library, is usually referred to
Order or command chain.
In the present embodiment, setting influence factor detection period and state parameter acquisition period, each period to
One group of V and Ω value is sent in the step c, then filters out all status parameter values X that can not find corresponding relationship, whereinAnd the value n for representing abnormal problem quantity is generated, then X and n are sent in above-mentioned Step d and are disposed.Root
According to X and n, at least one solution is found in problem disposition library H, and driven computer is handled.
Goal of the invention to realize the present invention realizes above-mentioned spacecraft energy resource system safety certainly the present invention also provides a kind of
The management system of main management method, the management system include:
Clock module is used for setting time；
State acquisition module, according to the time that the clock module is set, the state of timing acquiring spacecraft energy resource system
Value；
Influence factor module, according to the clock module set time, timing detect spacecraft energy resource system in whether
In the presence of the factor for influencing spacecraft state；
State and influence factor comprehensive analysis module are received and are sent out by the state acquisition module and the influence factor module
The real time data sent, and the data received are handled；
Problem disposes module, receives the data processed result sent by the state and influence factor comprehensive analysis module,
And result is analyzed, processing method is provided, abnormal problem is disposed.
A kind of embodiment according to the present invention, above-mentioned list L are stored in the state acquisition module, above-mentioned list S
It being stored in the influence factor module, above-mentioned corresponding relationship f is stored in the state and influence factor comprehensive analysis module,
Above problem disposition library H is stored in described problem disposition module.
In one embodiment of the invention, clock module gives period and the state parameter acquisition of influence factor detection
Period, in each period, influence factor module and state acquisition module can be sent to state and influence factor comprehensive analysis module
One group of V and Ω value, state and influence factor comprehensive analysis module can be according to the values received, and corresponding relationship can not be found by filtering out
All status parameter values X, whereinAnd the value n for representing abnormal problem quantity is generated, X, n are then sent to problem
Dispose module.Problem disposes module and finds at least one solution in problem disposition library H according to the value of X and n, and drives
Computer is handled.
According to the above method of the present invention and system, problems of the prior art are solved, the energy is greatly reduced
The time of system exception discovery, improve the speed disposed extremely.The link manually participated in is greatly reduced in this method, saves
Human cost.
The foregoing is merely an embodiment of the invention, are not intended to restrict the invention, for this field
For technical staff, the invention may be variously modified and varied.All within the spirits and principles of the present invention, made any
Modification, equivalent replacement, improvement etc., should all be included in the protection scope of the present invention.
Claims (14)
1. method is managed independently in a kind of spacecraft energy resource system safety, comprising the following steps:
A. the state value of timing acquiring spacecraft energy resource system；
B. with the presence or absence of the factor for influencing spacecraft state in timing detection spacecraft energy resource system；
C. the data generated in a step and in the b step are handled；
D. the processing result in the step c is analyzed, processing method is provided, abnormal problem is disposed.
2. method is managed independently in spacecraft energy resource system safety according to claim 1, which is characterized in that in a
In step, state parameter list L is established, the institute that the parameter in the list is able to reflect spacecraft energy resource system is stateful.
3. method is managed independently in spacecraft energy resource system safety according to claim 2, which is characterized in that in the b
In step, influence factor list S is established, the influence of all state parameters that can change spacecraft energy resource system is covered in the list
Factor.
4. method is managed independently in spacecraft energy resource system safety according to claim 3, which is characterized in that in the c
In step, the corresponding relationship of the state parameter Yu the influence factor is established, when the change of all state parameters can be found
When corresponding influence factor, f (V, Ω)=0 is enabled；
When the change for having at least one state parameter, when can not find corresponding influence factor, it is considered as energy resource system generation
At least one exception, this season f (V, Ω)=exception number, whereinFor all influence factors generated in this period
Set, V is the collection value of all state parameters in list L in this period.
5. method is managed independently in spacecraft energy resource system safety according to claim 4, which is characterized in that in the d
In step, problem disposition library H is established, the solution of all abnormal problems is saved in library.
6. method is managed independently in spacecraft energy resource system safety according to claim 5, which is characterized in that setting influences
The period of factor detection and the period of state parameter acquisition, each period send one group of V and Ω value into the step c, then
All status parameter values X that can not find corresponding relationship are filtered out, whereinAnd it generates one and represents abnormal problem quantity
Value n, then X and n are sent in the Step d and are disposed.
7. method is managed independently in spacecraft energy resource system safety according to claim 6, which is characterized in that according to X and
N finds at least one solution in described problem disposition library H, and driven computer is handled.
8. a kind of management for the spacecraft energy resource system safety autonomous management method realized as described in one of claim 1 to 7
System characterized by comprising
Clock module is used for setting time；
State acquisition module, according to the time that the clock module is set, the state value of timing acquiring spacecraft energy resource system；
Influence factor module, according to the time that the clock module is set, timing detects whether there is in spacecraft energy resource system
Influence the factor of spacecraft state；
State and influence factor comprehensive analysis module, reception are sent by the state acquisition module and the influence factor module
Real time data, and the data received are handled；
Problem disposes module, receives the data processed result sent by the state and influence factor comprehensive analysis module, and right
As a result it is analyzed, provides processing method, abnormal problem is disposed.
9. management system according to claim 8, which is characterized in that state parameter list L is established, in the list L
The institute that parameter is able to reflect spacecraft energy resource system is stateful, and the list L is stored in the state acquisition module.
10. management system according to claim 8, which is characterized in that establish influence factor list S, contain in the list S
The influence factor of all state parameters that can change spacecraft energy resource system is covered, the list S is stored in the influence factor mould
In block.
11. management system according to claim 8, which is characterized in that establish the state parameter and the influence factor
Corresponding relationship f enable f (V, Ω)=0 when the change of all state parameters can find corresponding influence factor；
When the change for having at least one state parameter, when can not find corresponding influence factor, it is considered as energy resource system generation
At least one exception, this season f (V, Ω)=exception number, whereinFor all influence factors generated in this period
Set, V is the collection value of all state parameters in list L in this period；
The corresponding relationship f is stored in the state and influence factor comprehensive analysis module.
12. management system according to claim 8, which is characterized in that establish problem disposition library H, saved in library all different
The solution of Chang Wenti, described problem disposition library H are stored in described problem disposition module.
13. management system according to claim 8, which is characterized in that the clock module gives influence factor detection
Period and the period of state parameter acquisition, in each period, the influence factor module and the state acquisition module can Xiang Suoshu
State and influence factor comprehensive analysis module send one group of V and Ω value, and the state and influence factor comprehensive analysis module can roots
According to the value received, all status parameter values X that can not find corresponding relationship are filtered out, whereinAnd generate one represent it is different
Then X, n are sent to described problem disposition module by the value n of normal problematic amount.
14. the management system according to one of claim 8 to 13, which is characterized in that described problem dispose module according to X and
The value of n finds at least one solution in described problem disposition library H, and driven computer is handled.
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114285455A (en) * | 2021-12-16 | 2022-04-05 | 广州爱浦路网络技术有限公司 | Satellite energy-saving control method, system, device and storage medium based on core network |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104297699A (en) * | 2014-09-26 | 2015-01-21 | 航天东方红卫星有限公司 | Satellite power supply health condition tracking and detecting method based on intelligent interpretation |
| CN104299659A (en) * | 2013-07-16 | 2015-01-21 | 中广核工程有限公司 | Method, device and system for monitoring running state of nuclear power plant |
| CN105929337A (en) * | 2016-05-10 | 2016-09-07 | 中国人民解放军国防科学技术大学 | Data processing unit of spacecraft functional structure lithium battery system |
| CN106023345A (en) * | 2016-06-29 | 2016-10-12 | 北京奇虎科技有限公司 | Car repair prompting method and system |
-
2019
- 2019-01-04 CN CN201910007120.7A patent/CN109740942B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104299659A (en) * | 2013-07-16 | 2015-01-21 | 中广核工程有限公司 | Method, device and system for monitoring running state of nuclear power plant |
| CN104297699A (en) * | 2014-09-26 | 2015-01-21 | 航天东方红卫星有限公司 | Satellite power supply health condition tracking and detecting method based on intelligent interpretation |
| CN105929337A (en) * | 2016-05-10 | 2016-09-07 | 中国人民解放军国防科学技术大学 | Data processing unit of spacecraft functional structure lithium battery system |
| CN106023345A (en) * | 2016-06-29 | 2016-10-12 | 北京奇虎科技有限公司 | Car repair prompting method and system |
Non-Patent Citations (1)
| Title |
|---|
| 王环 等: "专家知识在在轨管理中应用的设想", 《航天器工程》 * |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114285455A (en) * | 2021-12-16 | 2022-04-05 | 广州爱浦路网络技术有限公司 | Satellite energy-saving control method, system, device and storage medium based on core network |
| CN114285455B (en) * | 2021-12-16 | 2022-10-21 | 广州爱浦路网络技术有限公司 | Satellite energy-saving control method, system, device and storage medium based on core network |
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