CN107544332A - Data processing method and related product - Google Patents
Data processing method and related product Download PDFInfo
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- CN107544332A CN107544332A CN201710826950.3A CN201710826950A CN107544332A CN 107544332 A CN107544332 A CN 107544332A CN 201710826950 A CN201710826950 A CN 201710826950A CN 107544332 A CN107544332 A CN 107544332A
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Abstract
The embodiments of the invention provide a kind of data processing method and Related product, methods described comprises the following steps：Determine the relative motion parameter between target object and space equipment；It is determined that safe class corresponding with the relative motion parameter；When the safe class is less than predetermined level, prevention policies are determined according to the relative motion parameter, and strengthen the defensive ability/resistance ability of the space equipment according to the prevention policies.The relative motion parameter between target object and space equipment can be determined by the embodiment of the present invention, and further determine that safe class corresponding to the relative motion parameter, when safe class is less than predetermined level, corresponding prevention policies are then determined according to relative motion parameter, and then, strengthen the defensive ability/resistance ability of space equipment according to the prevention policies, to ensure the security of space equipment.
Description
Technical field
The present invention relates to Internet technical field, and in particular to a kind of control method and device applied to space equipment.
Background technology
With the fast development of information technology, huge change also is brought to life, for example, the appearance of Internet of Things.Thing
Networking can be regarded as：Communication between thing and thing, it is unlike interpersonal communication taking human as leading, normal conditions
Under, if being that the wrong hair of information or leakage are sent out taking human as leading communication characteristicses, being as leading people can be by various mode
Correct what is come.But the communication in Internet of Things, communication two party is all object in most cases, and itself can not carry out manual intervention,
Thus, in Internet of Things communication process, higher requirement is proposed to the reliability of wireless telecommunication system.
Certainly, as the fast development of technology of Internet of things, its application have been not limited to earth environment, Internet of Things is distinctive
Advantage, the preview of its function, in the case where I takes charge of the cooperation with relevant departments, is also being contemplated into structure space in space environment
Internet of Things.Therefore, how to solve the problems, such as that the function of resisting space trash of space equipment is urgently to be resolved hurrily.
The content of the invention
The embodiments of the invention provide a kind of control method and Related product applied to space equipment, can run into too
During empty rubbish, effectively resisted, enhance the defence capability of space equipment.
First aspect of the embodiment of the present invention provides a kind of control method applied to space equipment, including：
Determine the relative motion parameter between target object and space equipment；
It is determined that safe class corresponding with the relative motion parameter；
When the safe class is less than predetermined level, prevention policies are determined according to the relative motion parameter, and according to
The prevention policies strengthen the defensive ability/resistance ability of the space equipment.
Second aspect of the embodiment of the present invention provides a kind of control device applied to space equipment, including：
First determining unit, for determining the relative motion parameter between target object and space equipment；
Second determining unit, for determining safe class corresponding with the relative motion parameter；
Processing unit, for when the safe class is less than predetermined level, being determined according to the relative motion parameter anti-
Shield strategy, and according to the defensive ability/resistance ability of the prevention policies enhancing space equipment.
The third aspect of the embodiment of the present invention provides a kind of controller, including：
Processor and memory；Wherein, the processor is by calling the code in the memory or instructing to perform
Such as the instruction of the part or all of step described in first aspect of the embodiment of the present invention.
Fourth aspect, the embodiments of the invention provide a kind of computer-readable recording medium, wherein, it is described computer-readable
Storage medium is used to store computer program, wherein, the computer program causes computer to perform such as the embodiment of the present invention the
The instruction of part or all of step described in one side.
5th aspect, the embodiments of the invention provide a kind of computer program product, wherein, the computer program product
Non-transient computer-readable recording medium including storing computer program, the computer program are operable to make calculating
Machine is performed such as the part or all of step described in first aspect of the embodiment of the present invention.The computer program product can be one
Individual software installation bag.
Implement the embodiment of the present invention, have the advantages that：
As can be seen that by the embodiment of the present invention, the relative motion parameter between target object and space equipment is determined, really
Fixed safe class corresponding with relative motion parameter, when safe class is less than predetermined level, determined according to relative motion parameter
Prevention policies, and according to the defensive ability/resistance ability of the prevention policies enhancing space equipment, it is seen that, it may be determined that target object and space
Relative motion parameter between equipment, and safe class corresponding to the relative motion parameter is further determined that, it is low in safe class
When predetermined level, then corresponding prevention policies are determined according to relative motion parameter, and then, strengthen space according to the prevention policies and set
Standby defensive ability/resistance ability, to ensure the security of space equipment.
Brief description of the drawings
Technical scheme in order to illustrate the embodiments of the present invention more clearly, make required in being described below to embodiment
Accompanying drawing is briefly described, it should be apparent that, drawings in the following description are some embodiments of the present invention, for ability
For the those of ordinary skill of domain, on the premise of not paying creative work, it can also be obtained according to these accompanying drawings other attached
Figure.
A kind of embodiment schematic flow sheet of Fig. 1 control methods applied to space equipment provided in an embodiment of the present invention；
The embodiment flow signal of Fig. 2 another control methods for being applied to space equipment provided in an embodiment of the present invention
Figure；
Fig. 3 a are a kind of example structure signals of control device applied to space equipment provided in an embodiment of the present invention
Figure；
Fig. 3 b are first of the detection means applied to space equipment described in Fig. 3 a provided in an embodiment of the present invention
The structural representation of determining unit；
Fig. 3 c are second of the control device applied to space equipment described in Fig. 3 a provided in an embodiment of the present invention
The structural representation of determining unit；
Fig. 3 d are the another of the control device applied to space equipment described in Fig. 3 a provided in an embodiment of the present invention
Structural representation；
Fig. 4 is a kind of example structure schematic diagram of controller provided in an embodiment of the present invention.
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 carried out clear, complete
Site preparation describes, it is clear that described embodiment is part of the embodiment of the present invention, rather than whole embodiments.Based on this hair
Embodiment in bright, the every other implementation that those of ordinary skill in the art are obtained under the premise of creative work is not made
Example, belongs to the scope of protection of the invention.
Term " first ", " second ", " the 3rd " in description and claims of this specification and the accompanying drawing and "
Four " etc. be to be used to distinguish different objects, rather than for describing particular order.In addition, term " comprising " and " having " and it
Any deformation, it is intended that cover non-exclusive include.Such as contain the process of series of steps or unit, method, be
The step of system, product or equipment are not limited to list or unit, but alternatively also including the step of not listing or list
Member, or alternatively also include for the intrinsic other steps of these processes, method, product or equipment or unit.
Referenced herein " embodiment " is it is meant that the special characteristic, structure or the characteristic that describe can wrap in conjunction with the embodiments
In at least one embodiment of the present invention.It is identical that each position in the description shows that the phrase might not be each meant
Embodiment, nor the independent or alternative embodiment with other embodiments mutual exclusion.Those skilled in the art explicitly and
Implicitly understand, embodiment described herein can be combined with other embodiments.
It should be noted that the space equipment in the embodiment of the present invention can be following at least one：Space station, space
Cabin, spaceship, cosmograd, aircraft, flying saucer, fire balloon, rocket, satellite etc..Space equipment due to away from the earth, because
This, in its running, once breaking down, then consequence is quite serious.Space equipment in the embodiment of the present invention, inside it
And outside distributed substantial amounts of sensor, the sensor can be with following at least one：Temperature sensor, ambient light sensing
Device, gravity sensor, acceleration transducer, Smoke Sensor, emission detecting sensor, humidity sensor, baroceptor, pressure
Force snesor etc..Sensor can be used for the various data for detecting space equipment, and then, the running status of space equipment is added
With monitoring.Space equipment can include at least one controller, and controller can be following at least one：Control platform or clothes
Business device.Controller can obtain the data that sensor detects, and then, these data are analyzed, to obtain user's needs
Result.Certainly, the controller in the embodiment of the present invention can integrate CPU, or, artificial intelligence chip, or, quantum core
Piece.
Further, the keeper in the embodiment of the present invention can be configured with mobile terminal, and the mobile terminal can include
Smart mobile phone (such as Android phone, iOS mobile phones, Windows Phone mobile phones), tablet personal computer, palm PC, notebook
Computer, satellite phone, mobile internet device (MID, Mobile Internet Devices) or Wearable etc., certainly
It can also include the other equipment with network savvy, such as intelligent television, intelligent air condition, intelligent kettle, intelligent lamp, intelligence
The smart machine of switch or some Internet of Things.For space equipment under operation, it is possible that space trash, therefore,
The embodiment of the present invention, it is proposed that a kind of control method applied to space equipment, including：
Determine the relative motion parameter between target object and space equipment；
It is determined that safe class corresponding with the relative motion parameter；
When the safe class is less than predetermined level, prevention policies are determined according to the relative motion parameter, and according to
The prevention policies strengthen the defensive ability/resistance ability of the space equipment.
As can be seen that by the embodiment of the present invention, the service data of space equipment is obtained, service data is screened,
Misoperation data are obtained, determine the target location of misoperation data, the predeterminable area centered on target location is carried out
Monitoring, obtains monitoring data, monitoring data is analyzed, obtain analysis result, maintenance processing is carried out according to analysis result, from
And the service data of space equipment can be monitored, to obtain misoperation data, and these misoperation data are chased after
The individual position found and occurred extremely of tracing to the source, and make further monitoring to the position, analysis result is obtained, is carried out according to analysis result
Maintenance is handled, and improves the ability of maintenance of space equipment.
Referring to Fig. 1, the embodiment stream for a kind of control method applied to space equipment provided in an embodiment of the present invention
Journey schematic diagram.The control method applied to space equipment described in the present embodiment, comprises the following steps：
101st, the relative motion parameter between target object and space equipment is determined.
Wherein, above-mentioned target object can be space trash, and space trash can be following at least one：Meteor, discard
Flight equipment, solar windstorm etc..Certainly, in the process of running, if running into target object, target object is then for space equipment
Can possess certain flying speed, certain threat so can be just caused to space equipment.Wherein, for taking speed, target
Object has a speed, and space equipment also has a speed, is a vector if speed, therefore, can pass through momentum theorem
And law of conservation of energy determines the last final speed of space equipment and the speed of target object.
Alternatively, in above-mentioned steps 101, the relative motion parameter between target object and space equipment is determined, it may include
Following steps：
11st, the first operational factor and attribute information of the target object are determined, first operational factor includes：Speed
Degree, acceleration, angular speed, running temperature and gravitation size, the attribute information include following at least one：Quality, density, body
Product, material type；
12nd, first operational factor is converted into by the 3rd operational factor according to the attribute information；
13rd, the second operational factor of the space equipment is obtained；
14th, the relative motion parameter is determined according to the 3rd operational factor and second operational factor.
Wherein, above-mentioned first operational factor may include following at least one：Speed, acceleration, angular speed, running temperature and
Gravitation size, wherein, speed is the flying speed of target object, and acceleration can be the acceleration of target object, and angular speed can
Think angular speed when target object flight, running temperature refers to the surface temperature of target object, and gravitation size is then target
The gravitation size that object is subject to.Above-mentioned attribute information can be following at least one：Quality, density, volume, material type, shape
Shape.Quality is the quality of target object, and density can be the density of target object, and volume is then the volume size of target object,
Material type is then the main component that what or target object target object be, for example, material property can be：Diamond, iron, titanium
Alloy etc., shape refers to the concrete shape of target object performance, for example, centrum, column, spheroid etc..Can on space equipment
To be provided with various sensors, the first operational factor and attribute information of target object can be obtained by these sensors, is entered
One step, the first operational factor can be converted, for example, because target object has the shape of its own, therefore, it is necessary to root
Turning the first operational factor according to its attribute information to be converted, the purpose of conversion is target object carrying out equivalent process, for example,
If target object is a spheroid, a point can be equivalent to, in another example, target object is an irregular thing
Body, then can be by its equivalent regular shape, for example, the first operational factor can be converted into one according to attribute information
The operational factor of point, obtains the 3rd operational factor, it is possible to further obtain the operational factor of space equipment itself, i.e., second
Operational factor, further, relative motion parameter is determined according to the second operational factor and the 3rd operational factor, by taking speed as an example,
If both, it may be determined that sum velocity (one in relative motion parameter), different conjunctions between space equipment and target object
Speed is also different to the extent of injury of space equipment, in this way, can obtain relative motion parameter through the above way.
Certainly, above-mentioned second operational factor may include following at least one：Speed, acceleration, angular speed, running temperature and
Gravitation size, wherein, speed is the flying speed of space equipment, and acceleration can be the acceleration of space equipment, and angular speed can
Think angular speed when space equipment flight, running temperature refers to the surface temperature of space equipment, and gravitation size is then space
The gravitation size that equipment is subject to.Above-mentioned attribute information can be following at least one：Quality, density, volume, material type, shape
Shape.Quality is the quality of space equipment, and density can be the density of space equipment, and volume is then the volume size of space equipment,
Material type is then the main component that what or target object space equipment be, for example, material property can be：Diamond, iron, titanium
Alloy etc., shape refers to the concrete shape of space equipment performance, for example, centrum, column, spheroid etc..
Alternatively, before above-mentioned steps 101, can also comprise the following steps：
The distance between target object and space equipment are detected, when distance therebetween is less than pre-determined distance threshold value,
Step 101 is performed, when distance therebetween is more than or equal to pre-determined distance threshold value, does not perform step 101.
Wherein, above-mentioned pre-determined distance threshold value can voluntarily be set or system default by user.
102nd, safe class corresponding with the relative motion parameter is determined.
Wherein, different relative motion parameters corresponds to different safe classes, therefore, it is possible to be determined in relative motion parameter
Afterwards, safe class corresponding to the relative motion parameter is determined.
Wherein, the relative motion parameter is a multi-Dimensional parameters；In above-mentioned steps 102, it is determined that joining with the relative motion
Safe class corresponding to number, including：
21st, weighted value corresponding to each dimensional parameter in the multi-Dimensional parameters is determined；
22nd, the weighted value according to corresponding to the multi-Dimensional parameters and its each dimension determines target alarms parameter；
23rd, determine that the target alarms parameter is corresponding according to the mapping relations between default alarm parameter and safe class
Safe class, as safe class corresponding to the relative motion parameter.
Wherein, relative motion parameter can include multiple dimensions, for example, speed is a dimension, acceleration is a dimension
Degree, direction is a dimension, and distance is dimension, etc..Therefore, a weighted value, the power can be corresponded to per dimension
Weight values can be empirical value, for example, default setting weighted value corresponding to per dimension, or, certain mode meter can be passed through
Calculate, for example, determining the irrelevance between each dimensional parameter and default normal parameter, determined according to these irrelevances each
Weighted value corresponding to dimensional parameter.For example, 3 dimensions, the irrelevance of 3 dimensions is divided into a1, a2, a3, then, weighted value can
To be respectively：A1/ (a1+a2+a3), a2/ (a1+a2+a3) and a3/ (a1+a2+a3).According to the multi-Dimensional parameters and per one-dimensional
Weighted value is weighted corresponding to degree, obtains target alarms parameter, and then, according to default alarm parameter and safe class
Between mapping relations determine safe class corresponding to target alarms parameter, as corresponding to relative motion parameter safety etc.
Level, wherein, the mapping relations between above-mentioned default alarm parameter and safe class can protect before the embodiment of the present invention is performed
In the memory that controller be present.
103rd, when the safe class is less than predetermined level, prevention policies are determined according to the relative motion parameter, and
Strengthen the defensive ability/resistance ability of the space equipment according to the prevention policies.
Wherein, above-mentioned predetermined level can voluntarily be set or system default by user.Above-mentioned prevention policies can include
Following at least one：Lift the speed of space equipment, the thickness of enhancing space equipment, the flight track of change space equipment, control
Space equipment processed is opened fire etc. to target object.When safe class is less than predetermined level, explain the situation more serious, object
Body is possible to hit space equipment at any time, and then, prevention policies can be determined according to relative motion parameter, for example, default set
Mapping relations between operational factor and prevention policies, the protection according to corresponding to the mapping relations can determine relative motion parameter
Strategy, and then, according to the defensive ability/resistance ability of prevention policies enhancing space equipment.
Alternatively, in above-mentioned steps 103, prevention policies are determined according to the relative motion parameter, it may include following steps：
31st, the impulsive force corresponding to target object according to the relative motion parameter prediction, and the target object
Contact the contact area of the space equipment；
32nd, prevention policies are determined according to the impulsive force and the contact area,
Wherein it is possible to according to relative motion parameter prediction target object can caused by impulsive force, and be likely to be exposed
The contact area of space equipment, on the one hand in order to reduce this impulsive force, on the other hand, also for supporting for enhancing contact area
Imperial ability, for example, thickness corresponding to enhancing contact area, in this way, can be according to corresponding to determining the impulsive force and contact area
Prevention policies, effectively to resist target object.
As can be seen that by the embodiment of the present invention, the service data of space equipment is obtained, service data is screened,
Misoperation data are obtained, determine the target location of misoperation data, the predeterminable area centered on target location is carried out
Monitoring, obtains monitoring data, monitoring data is analyzed, obtain analysis result, maintenance processing is carried out according to analysis result, from
And the service data of space equipment can be monitored, to obtain misoperation data, and these misoperation data are chased after
The individual position found and occurred extremely of tracing to the source, and make further monitoring to the position, analysis result is obtained, is carried out according to analysis result
Maintenance is handled, and improves the ability of maintenance of space equipment.
Referring to Fig. 2, the embodiment stream for a kind of control method applied to space equipment provided in an embodiment of the present invention
Journey schematic diagram.The control method applied to space equipment described in the present embodiment, comprises the following steps：
201st, monitor in preset range the first object whether occur.
Wherein, above-mentioned preset range is the monitor area of the related sensor on space equipment, and certainly, preset range also may be used
Voluntarily to be set by user.So, it is possible to achieve preset range is monitored, above-mentioned first object can be space trash,
Space trash can be following at least one：Meteor, discarded flight equipment, solar windstorm etc..
Whether the volume for the 202nd, detecting first object is more than preset vol.
Wherein, above-mentioned preset vol can voluntarily be set by user, or, system default.Can by camera, or
Telescope detects the volume of the first object, it is of course also possible to the attraction between space equipment and target object be determined, according to this
The anti-volume for pushing away the first object of attraction.
203rd, when the volume of first object is more than the preset vol, using first object as the target
Object, determine the relative motion parameter between the target object and space equipment.
Wherein, when the volume of the first object is more than preset vol, using the first object as target object, if the first object
Volume be less than preset vol, then can be not considered as target object.And then it may further determine that target object is set with space
Relative motion parameter between standby.
204th, safe class corresponding with the relative motion parameter is determined.
205th, when the safe class is less than predetermined level, prevention policies are determined according to the relative motion parameter, and
Strengthen the defensive ability/resistance ability of the space equipment according to the prevention policies.
Wherein, the specific descriptions of above-mentioned steps 203- steps 205 can refer to the control applied to space equipment described by Fig. 1
The corresponding steps of method processed, will not be repeated here.
As can be seen that by the embodiment of the present invention, monitor and whether occur the first object in preset range, detect the first object
Volume whether be more than preset vol, when the volume of the first object is more than preset vol, using the first object as target object,
The service data of space equipment is obtained, service data is screened, obtains misoperation data, determines misoperation data
Target location, the predeterminable area centered on target location is monitored, obtains monitoring data, monitoring data is divided
Analysis, obtains analysis result, maintenance processing is carried out according to analysis result, it is thus possible to be supervised to the service data of space equipment
Survey, to obtain misoperation data, and these misoperation data are chased after with individual trace to the source and finds the position occurred extremely, and to the position
Work further monitoring is put, analysis result is obtained, maintenance processing is carried out according to analysis result, improve the maintenance energy of space equipment
Power.
Consistent with the abovely, the control method applied to space equipment provided below for the implementation embodiments of the present invention
Device, it is specific as follows：
Fig. 3 a are referred to, are a kind of embodiment knot of control device applied to space equipment provided in an embodiment of the present invention
Structure schematic diagram.The control device applied to space equipment described in the present embodiment, including：First determining unit 301, second
Determining unit 302 and processing unit 303, it is specific as follows：
First determining unit 301, for determining the relative motion parameter between target object and space equipment；
Second determining unit 302, for determining safe class corresponding with the relative motion parameter；
Processing unit 303, for when the safe class is less than predetermined level, being determined according to the relative motion parameter
Prevention policies, and according to the defensive ability/resistance ability of the prevention policies enhancing space equipment.
Alternatively, if Fig. 3 b, Fig. 3 b are the first determination of the control device applied to space equipment described in Fig. 3 a
The specific refinement structure of unit 301, first determining unit 301 may include：First determining module 3011, conversion module
3012nd, the determining module 3014 of acquisition module 3013 and second, it is specific as follows；
First determining module 3011, for determining the first operational factor and attribute information of the target object, described
One operational factor includes：Speed, acceleration, angular speed, running temperature and gravitation size, the attribute information include it is following at least
It is a kind of：Quality, density, volume, material type；
Conversion module 3012, join for first operational factor to be converted into the 3rd operation according to the attribute information
Number；
Acquisition module 3013, for obtaining the second operational factor of the space equipment；
Second determining module 3014, for determining the phase according to the 3rd operational factor and second operational factor
To operational factor.
Alternatively, the relative motion parameter is a multi-Dimensional parameters；Such as Fig. 3 c, Fig. 3 c are to be applied to described in Fig. 3 a
The specific refinement structure of second determining unit 302 of the control device of space equipment, second determining unit 302 may include：
3rd determining module 3021 and the 4th determining module 3022, it is specific as follows:
3rd determining module 3021, for determining weighted value corresponding to each dimensional parameter in the multi-Dimensional parameters；And
Target alarms parameter is determined according to weighted value corresponding to the multi-Dimensional parameters and its each dimension；
4th determining module 3022, for determining institute according to the mapping relations between default alarm parameter and safe class
Safe class corresponding to target alarms parameter is stated, as safe class corresponding to the relative motion parameter.
Alternatively, the processing unit 303 determines the specific implementation of prevention policies according to the relative motion parameter
For：
The impulsive force corresponding to target object according to the relative motion parameter prediction, and target object contact
The contact area of the space equipment；And prevention policies are determined according to the impulsive force and the contact area,
Alternatively, if Fig. 3 d, Fig. 3 d are a kind of modification of the control device applied to space equipment described in Fig. 3 a
Structure, it can also include monitoring unit 304 and detection unit 305 compared with Fig. 3 a, specific as follows：
Monitoring unit 304, whether occurs the first object in preset range for monitoring；
Whether detection unit 305, the volume for detecting first object are more than preset vol, and in first thing
When the volume of body is more than the preset vol, using first object as the target object.
As can be seen that by the control device applied to space equipment described by the embodiment of the present invention, object is determined
Relative motion parameter between body and space equipment, it is determined that safe class corresponding with relative motion parameter, low in safe class
When predetermined level, prevention policies are determined according to relative motion parameter, and strengthen supporting for the space equipment according to prevention policies
Imperial ability, it is seen that, it may be determined that the relative motion parameter between target object and space equipment, and further determine that the relative fortune
Safe class corresponding to row parameter, when safe class is less than predetermined level, then corresponding protection is determined according to relative motion parameter
Strategy, and then, according to the defensive ability/resistance ability of prevention policies enhancing space equipment, to ensure the security of space equipment.
It should be noted that the detection means applied to space equipment described by apparatus of the present invention embodiment is with function
The form of unit is presented.Term " unit " used herein above should be understood to implication as most wide as possible, each for realizing
The object of function described by " unit " for example can be integrated circuit ASIC, single circuit, for performing one or more softwares
Or the processor (shared, special or chipset) and memory of firmware program, combinational logic circuit, and/or realization is provided
Other suitable components of above-mentioned function.
For example, the first determining unit 301, for determining the relative motion parameter between target object and space equipment
Function can be as shown in Figure 4 controller realize, specifically can be by processor 3000 by calling in memory 4000
Executable program code, determine the relative motion parameter between target object and space equipment.
Consistent with the abovely, referring to Fig. 4, being filled for a kind of control applied to space equipment provided in an embodiment of the present invention
The example structure schematic diagram put.The control device applied to space equipment described in the present embodiment, including：It is at least one
Input equipment 1000；At least one output equipment 2000；At least one processor 3000, such as CPU；With memory 4000, on
Input equipment 1000, output equipment 2000, processor 3000 and memory 4000 is stated to connect by bus 5000.
It should be noted that processor 3000 here can be a treatment element or multiple treatment elements
General designation.For example, the treatment element can be central processing unit (Central Processing Unit, CPU) or
Specific integrated circuit (Application Specific Integrated Circuit, ASIC), or be arranged to implement
One or more integrated circuits of the embodiment of the present application, such as：One or more microprocessors (digital singnal
Processor, DSP), or, one or more field programmable gate array (Field Programmable Gate Array,
FPGA)。
Memory 4000 can be the general designation of a storage device or multiple memory elements, and can for storage
Parameter, data etc. required for configuration processor code or the operation of application program running gear.And memory 4000 can be included at random
Memory (RAM), nonvolatile memory (non-volatile memory), such as magnetic disk storage, flash memory can also be included
(Flash) etc..
Bus 5000 can be that industry standard architecture (Industry Standard Architecture, ISA) is total
Line, external equipment interconnection (Peripheral Component, PCI) bus or extended industry-standard architecture (Extended
Industry Standard Architecture, EISA) bus etc..The bus can be divided into address bus, data/address bus, control
Bus processed etc..For ease of representing, only represented in Fig. 4 with a thick line, it is not intended that an only bus or a type of
Bus.
Above-mentioned processor 3000, is used for：
Determine the relative motion parameter between target object and space equipment；
It is determined that safe class corresponding with the relative motion parameter；
When the safe class is less than predetermined level, prevention policies are determined according to the relative motion parameter, and according to
The prevention policies strengthen the defensive ability/resistance ability of the space equipment.
Alternatively, above-mentioned processor 3000 determines the relative motion parameter between target object and space equipment, including：
The first operational factor and attribute information of the target object are determined, first operational factor includes：Speed, add
Speed, angular speed, running temperature and gravitation size, the attribute information include following at least one：Quality, density, volume, thing
Matter type；
First operational factor is converted into by the 3rd operational factor according to the attribute information；
Obtain the second operational factor of the space equipment；
The relative motion parameter is determined according to the 3rd operational factor and second operational factor.
Alternatively, above-mentioned processor 3000, the relative motion parameter are a multi-Dimensional parameters；
It is described to determine corresponding with relative motion parameter safe class, including：
Determine weighted value corresponding to each dimensional parameter in the multi-Dimensional parameters；
Target alarms parameter is determined according to weighted value corresponding to the multi-Dimensional parameters and its each dimension；
Determine that the target alarms parameter is corresponding according to the mapping relations between default alarm parameter and safe class
Safe class, as safe class corresponding to the relative motion parameter.
Alternatively, above-mentioned processor 3000 determines prevention policies according to the relative motion parameter, including：
The impulsive force corresponding to target object according to the relative motion parameter prediction, and target object contact
The contact area of the space equipment；
Prevention policies are determined according to the impulsive force and the contact area,
Alternatively, above-mentioned processor 3000 also particularly useful for：
Whether there is the first object in monitoring preset range；
Whether the volume for detecting first object is more than preset vol；
When the volume of first object is more than the preset vol, using first object as the object
Body.
The embodiment of the present invention also provides a kind of computer-readable storage medium, wherein, the computer-readable storage medium can be stored with journey
Sequence, it is applied to the portion of the control method of space equipment when the program performs including any one described in above method embodiment
Point or Overall Steps.
The embodiment of the present invention also provides a kind of computer program product, and the computer program product includes storing calculating
The non-transient computer-readable recording medium of machine program, the computer program are operable to make computer perform side as described above
Any one described in method embodiment is applied to the part or all of step of the control method of space equipment.
Although combining each embodiment herein, invention has been described, however, implementing the present invention for required protection
During, those skilled in the art are by checking the accompanying drawing, disclosure and appended claims, it will be appreciated that and it is real
Other changes of the existing open embodiment.In the claims, the word of " comprising " (comprising) one is not excluded for other compositions
Part or step, "a" or "an" are not excluded for multiple situations.Single processor or other units can realize claim
In some functions enumerating.Mutually different has been recited in mutually different dependent some measures, it is not intended that these are arranged
Apply to combine and produce good effect.
It will be understood by those skilled in the art that embodiments of the invention can be provided as method, apparatus (equipment) or computer journey
Sequence product.Therefore, in terms of the present invention can use complete hardware embodiment, complete software embodiment or combine software and hardware
The form of embodiment.Moreover, the present invention can use the calculating for wherein including computer usable program code in one or more
The computer program that machine usable storage medium is implemented on (including but is not limited to magnetic disk storage, CD-ROM, optical memory etc.)
The form of product.Computer program is stored/distributed in suitable medium, is provided together with other hardware or one as hardware
Part, other distribution forms can also be used, such as pass through the wired or wireless telecommunication systems of Internet or other.
The present invention be with reference to the embodiment of the present invention method, apparatus (equipment) and computer program product flow chart with/
Or block diagram describes.It should be understood that can by each flow in computer program instructions implementation process figure and/or block diagram and/
Or square frame and the flow in flow chart and/or block diagram and/or the combination of square frame.These computer program instructions can be provided
To the processor of all-purpose computer, special-purpose computer, Embedded Processor or other programmable data processing devices to produce one
Individual machine so that produced by the instruction of computer or the computing device of other programmable data processing devices for realizing
The device for the function of being specified in one flow of flow chart or multiple flows and/or one square frame of block diagram or multiple square frames.
These computer program instructions, which may be alternatively stored in, can guide computer or other programmable data processing devices with spy
Determine in the computer-readable memory that mode works so that the instruction being stored in the computer-readable memory, which produces, to be included referring to
Make the manufacture of device, the command device realize in one flow of flow chart or multiple flows and/or one square frame of block diagram or
The function of being specified in multiple square frames.
These computer program instructions can be also loaded into computer or other programmable data processing devices so that counted
Series of operation steps is performed on calculation machine or other programmable devices to produce computer implemented processing, so as in computer or
The instruction performed on other programmable devices is provided for realizing in one flow of flow chart or multiple flows and/or block diagram one
The step of function of being specified in individual square frame or multiple square frames.
Although with reference to specific features and embodiment, invention has been described, it is clear that, do not departing from this hair
In the case of bright spirit and scope, various modifications and combinations can be carried out to it.Correspondingly, the specification and drawings are only institute
The exemplary illustration of the invention that attached claim is defined, and be considered as covered in the scope of the invention any and all and repair
Change, change, combining or equivalent.Obviously, those skilled in the art can to the present invention carry out it is various change and modification without
Depart from the spirit and scope of the present invention.So, if the present invention these modifications and variations belong to the claims in the present invention and its
Within the scope of equivalent technologies, then the present invention is also intended to comprising including these changes and modification.
Claims (10)
- A kind of 1. control method applied to space equipment, it is characterised in that including：Determine the relative motion parameter between target object and space equipment；It is determined that safe class corresponding with the relative motion parameter；When the safe class is less than predetermined level, prevention policies are determined according to the relative motion parameter, and according to described Prevention policies strengthen the defensive ability/resistance ability of the space equipment.
- 2. according to the method for claim 1, it is characterised in that relative between the determination target object and space equipment Operational factor, including：The first operational factor and attribute information of the target object are determined, first operational factor includes：Speed, acceleration Degree, angular speed, running temperature and gravitation size, the attribute information include following at least one：Quality, density, volume, material Type；First operational factor is converted into by the 3rd operational factor according to the attribute information；Obtain the second operational factor of the space equipment；The relative motion parameter is determined according to the 3rd operational factor and second operational factor.
- 3. method according to claim 1 or 2, it is characterised in that the relative motion parameter is a multi-Dimensional parameters；It is described to determine corresponding with relative motion parameter safe class, including：Determine weighted value corresponding to each dimensional parameter in the multi-Dimensional parameters；Target alarms parameter is determined according to weighted value corresponding to the multi-Dimensional parameters and its each dimension；Determine that the target alarms parameter is corresponding safe according to the mapping relations between default alarm parameter and safe class Grade, as safe class corresponding to the relative motion parameter.
- 4. according to the method described in any one of claims 1 to 3, it is characterised in that described true according to the relative motion parameter Determine prevention policies, including：The impulsive force corresponding to target object according to the relative motion parameter prediction, and described in target object contact The contact area of space equipment；Prevention policies are determined according to the impulsive force and the contact area.
- 5. according to the method described in any one of Claims 1-4, it is characterised in that methods described also includes：Whether there is the first object in monitoring preset range；Whether the volume for detecting first object is more than preset vol；When the volume of first object is more than the preset vol, using first object as the target object.
- A kind of 6. control device applied to space equipment, it is characterised in that including：First determining unit, for determining the relative motion parameter between target object and space equipment；Second determining unit, for determining safe class corresponding with the relative motion parameter；Processing unit, for when the safe class is less than predetermined level, protection plan to be determined according to the relative motion parameter Slightly, and according to the prevention policies defensive ability/resistance ability of the space equipment is strengthened.
- 7. device according to claim 6, it is characterised in that first determining unit includes：First determining module, for determining the first operational factor and attribute information of the target object, the first operation ginseng Number includes：Speed, acceleration, angular speed, running temperature and gravitation size, the attribute information include following at least one：Matter Amount, density, volume, material type；Conversion module, for first operational factor to be converted into the 3rd operational factor according to the attribute information；Acquisition module, for obtaining the second operational factor of the space equipment；Second determining module, for determining that the relative motion is joined according to the 3rd operational factor and second operational factor Number.
- 8. the device according to claim 6 or 7, it is characterised in that the relative motion parameter is a multi-Dimensional parameters；Second determining unit includes：3rd determining module, for determining weighted value corresponding to each dimensional parameter in the multi-Dimensional parameters；And according to described Weighted value corresponding to multi-Dimensional parameters and its each dimension determines target alarms parameter；4th determining module, for determining that the target is accused according to the mapping relations between default alarm parameter and safe class Safe class corresponding to alert parameter, as safe class corresponding to the relative motion parameter.
- 9. according to the device described in any one of claim 6 to 8, it is characterised in that the processing unit is according to the relative fortune Row parameter determines that the specific implementation of prevention policies is：The impulsive force corresponding to target object according to the relative motion parameter prediction, and described in target object contact The contact area of space equipment；And prevention policies are determined according to the impulsive force and the contact area.
- 10. according to the device described in any one of claim 6 to 9, it is characterised in that described device also includes：Monitoring unit, whether occurs the first object in preset range for monitoring；Whether detection unit, the volume for detecting first object are more than preset vol, and in the body of first object When product is more than the preset vol, using first object as the target object.
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Application publication date: 20180105 |