CN106850051A - A kind of space junk cleaning system and method based on microsatellite - Google Patents
A kind of space junk cleaning system and method based on microsatellite Download PDFInfo
- Publication number
- CN106850051A CN106850051A CN201710236792.6A CN201710236792A CN106850051A CN 106850051 A CN106850051 A CN 106850051A CN 201710236792 A CN201710236792 A CN 201710236792A CN 106850051 A CN106850051 A CN 106850051A
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- space junk
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- space
- microsatellite
- moonlet
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04B—TRANSMISSION
- H04B7/00—Radio transmission systems, i.e. using radiation field
- H04B7/14—Relay systems
- H04B7/15—Active relay systems
- H04B7/185—Space-based or airborne stations; Stations for satellite systems
- H04B7/1851—Systems using a satellite or space-based relay
- H04B7/18519—Operations control, administration or maintenance
Abstract
System is cleared up the invention discloses a kind of space junk based on microsatellite, it is included：Ground observation and analysis module, orbital position and space junk process task purpose for determining space junk；Carrier module, is communicated to connect with ground observation and analysis module, and trapping module feeding in space is subscribed track by it according to the instruction of ground observation and analysis module；Space trapping module, communicates to connect with ground observation and analysis module, and it includes the fragment adapter moonlet being mounted in carrier module and multiple observations for being attached on the fragment adapter moonlet and manipulates microsatellite；Observation is used to be observed space junk to obtain observation data with manipulation microsatellite, and fragment adapter moonlet is used to process space junk with manipulation microsatellite according to observation data control observation.Its advantage is：Can realize that the failure spacecraft being currently running to space carries out Measuring error；Space junk can be carried out the treatment that leaves the right or normal track.
Description
Technical field
The present invention relates to outer space Space environment detection and space junk Removal Technology field, and in particular to one kind is based on micro-
The space junk cleaning system and method for moonlet.
Background technology
With the development of space technology, increasing spacecraft is launched on Earth's orbit.According to statistics, mankind's activity
Each type objects close to 6000 tons are left in space, wherein 40% is located on LEO.The research of NASA and ESA shows
Show, current all of space junk（Including failure spacecraft, scrap spacecraft, spacecraft clash into the fragment to be formed, around the earth
The aerolite of operation）Although Mitigation methods can reduce the generation of space junk, all it is not enough to keep space debris environment
Stabilization.These space junks are uncontrolled, it is impossible to determine its movement locus, and the operation to spacecraft causes very big harm, must
Periodically removing must be taken measures to give.
The content of the invention
System and method is cleared up it is an object of the invention to provide a kind of space junk based on microsatellite, it includes ground
Face is observed and analysis system, delivery system and the part of space capture systems three, it is possible to achieve space junk is obtained, voluntary recall,
And reusable failure spacecraft maintenance treatment etc..
In order to achieve the above object, the present invention is achieved through the following technical solutions：
A kind of space junk cleaning system based on microsatellite, it is characterized in that, comprising：
Ground observation and analysis module, for determining the orbital position of space junk and the purpose of space junk process task；
Carrier module, communicates to connect with ground observation and analysis module, and it is according to the instruction of ground observation and analysis module by sky
Between trapping module feeding subscribe track；
Space trapping module, communicates to connect with ground observation and analysis module, and it includes the fragment being mounted in carrier module and connects
Pipe moonlet and the multiple observations being attached on the fragment adapter moonlet and manipulation microsatellite；Observation is used with manipulation microsatellite
In being observed to space junk to obtain observation data, fragment adapter moonlet is used for according to observation data control observation and behaviour
Control microsatellite is processed space junk.
The above-mentioned cleaning system of the space junk based on microsatellite, wherein：
Space junk is entered after the connection that the observation completes to space junk with manipulation microsatellite from the mode actively adhered to
Row treatment.
The above-mentioned cleaning system of the space junk based on microsatellite, wherein：
Described fragment adapter moonlet obtains the movement position and attitude information of space junk according to observation data.
The above-mentioned cleaning system of the space junk based on microsatellite, wherein：Described ground observation and analysis module bag
Contain：
Large-scale photon telescope, ground radar system, orbit information storehouse, task analysis platform；Large-scale photon telescope and ground
Radar system obtains orbital position of the space junk within the Observable time period, and the track provided by orbit information storehouse is believed
Breath obtains the complete track information of space junk, and task analysis platform is empty according to the complete orbit information analytical calculation of space junk
Between trapping module launch time, transmitting position, enter the orbit time and injection position.
The above-mentioned cleaning system of the space junk based on microsatellite, wherein：
In the space trapping module, 4 fragment adapter moonlets are attached with observation and manipulation microsatellite.
A kind of space junk method for cleaning, it is characterized in that, system is cleared up using the above-mentioned space junk based on microsatellite
Unite to complete, the method includes the steps of：
S1, ground observation and analysis module determine the orbital position of space junk and the purpose of space junk process task；
S2, carrier module mounting space trapping module, track is subscribed by space trapping module feeding；
Close to after space junk, multiple observation is with manipulation microsatellite from different perspectives to space junk for S3, fragment adapter moonlet
It is observed acquisition observation data；
S4, fragment adapter moonlet analysis observation data, according to analysis result control observation with manipulation microsatellite to space junk
Processed.
A kind of space junk method for cleaning based on microsatellite, it is characterized in that, described step S4 is specifically included：
S41, fragment adapter moonlet analysis observation data obtain the movement position and attitude information of space junk；
S42, fragment adapter moonlet are according to analysis result to the nearest observation of metric space fragment attachment point and manipulation microsatellite
Send instruction；
S43, chosen observation and manipulation microsatellite are adhered to space junk, and racemization is carried out to space junk after attachment, remaining
Observation returns fragment adapter moonlet original position again with manipulation microsatellite.
Above-mentioned space junk method for cleaning, wherein, in the step S43：
The chosen observation completes the connection to space junk with manipulation microsatellite from the mode of actively attachment.
The present invention has advantages below compared with prior art：Can realize that the fault satellites being currently running to space are carried out
Measuring error；Passive space vehicle can be carried out the treatment that leaves the right or normal track.
Brief description of the drawings
Fig. 1 is system block diagram of the invention；
Fig. 2 is the internal structure relation block diagram of ground observation of the invention and analysis module；
Fig. 3 is the internal structure relation block diagram of space trapping module of the invention.
Specific embodiment
Below in conjunction with accompanying drawing, by describing a preferably specific embodiment in detail, the present invention is further elaborated.
As shown in Figure 1, 2, system is cleared up the invention discloses a kind of space junk based on microsatellite, it is included：Ground
Face is observed and analysis module, carrier module and space trapping module.Ground observation is used to determine space junk with analysis module
The treatment of orbital position and space junk task objective（Task objective include space junk is carried out breakdown maintenance, become rail or
Person leaves the right or normal track treatment）, ground observation is generally observed by optics and radar with analysis module to space junk, and according to task
Sponsor unit's requirement determines the purpose of space junk process task, and determines carrier module（Mounting space trapping module）
Launch time, launch site, time of entering the orbit, injection position；Carrier module is communicated to connect with ground observation with analysis module, is used
Trapping module feeding in space is subscribed into track in the instruction according to ground observation and analysis module, carrier module there can be fortune
Carry the equipment such as carrier rocket 5 of function；Space trapping module is communicated to connect with ground observation with analysis module, and it includes carrying
Fragment adapter moonlet in the carrier module and multiple observations being attached on the fragment adapter moonlet 7 are micro- with manipulation defends
Star 6；Observation is used to be observed space junk to obtain observation data with manipulation microsatellite 6, and fragment adapter moonlet 7 is used for
Space junk is processed with manipulation microsatellite 6 according to observation data control observation, specifically, fragment adapter moonlet 7 can
Sight is manipulated with attitude information and according to the information with the movement position of acquisition space junk after being analyzed according to observation data
Survey carries out different operating, kinetic characteristic of the observation packet containing space junk with manipulation microsatellite 6（Including track and attitude motion
Information）, mass property（Quality, inertia and centroid position including space junk）, architectural characteristic（Including flexible vibration situation,
Attachment point situation）Observation information.
It is broken to space after the connection that the observation completes to space junk with manipulation microsatellite 6 from the mode actively adhered to
Piece is processed, and attachment herein can be realized by the attachment device based on Van der Waals force so that observation and manipulation microsatellite 6
Formed with space junk and be stably connected with.
Described ground observation is included with analysis module：Large-scale photon telescope 1, ground radar system 2, orbit information storehouse
3rd, task analysis platform 4.Large-scale photon telescope 1 and the observation of ground radar system 2 obtain space junk in the Observable time period
Interior orbital position, the orbit information provided by orbit information storehouse 3 obtains the complete track information of space junk, task analysis
Platform 4 according to launch time of the complete orbit information analytical calculation space trapping module of space junk, transmitting position, enter the orbit when
Between and injection position.
4 fragments are attached with the present embodiment, in the space trapping module, in observation and manipulation microsatellite 6 take over small
Satellite 7.
The invention also discloses a kind of space junk method for cleaning, its above-mentioned cleaning of the space junk based on microsatellite
System is completed, and the method includes the steps of：
S1, ground observation and analysis module determine the orbital position and space junk process task purpose of space junk；Specifically,
Integral utilization space target track, RCS characteristics, photometric property, adaptive optical imaging and radar imagery means are to task object
Comprehensive analysis is carried out, the orbital position and task objective of space junk are determined by ground observation and analysis system；
S2, carrier module mounting space trapping module, track is subscribed by space trapping module feeding；
S3, fragment adapter moonlet 7 are close to after space junk, and multiple observation is broken to space from different perspectives with manipulation microsatellite 6
Piece is observed acquisition observation data；
S4, the analysis observation data of fragment adapter moonlet 7, obtain space junk kinetic characteristic（Believe including track and attitude motion
Breath）, mass property（Quality, inertia and centroid position including space junk）, architectural characteristic（Including flexible vibration situation, attached
Point situation etc.）, according to space junk Characteristics Control metric space fragment attachment point recently, athletic posture and space junk it is close
Observation with manipulation microsatellite 6 space junk is processed.
Described step S4 is specifically included：
S41, the analysis observation data of fragment adapter moonlet 7 obtain the movement position and attitude information of space junk；
S42, fragment adapter moonlet 7 send instruction to a certain observation according to analysis result with manipulation microsatellite 6；
S43, chosen observation and manipulation microsatellite 6 are adhered to space junk, and observation has observation monument with manipulation microsatellite 6
Point and the spacecrafts rendezvous interface of cooperation, by observing the attachment with manipulation microsatellite 6 to space junk, make noncooperative space broken
Piece is changed into cooperative target, the spacecrafts rendezvous of the target that can be cooperated to target by fragment adapter moonlet 7, be target maintenance with
Left the right or normal track offer condition, and racemization is carried out to space junk after attachment, and it is small that remaining observation returns fragment adapter again with manipulation microsatellite 6
The original position of satellite 7.
In the step S43：Mode of the chosen observation with manipulation microsatellite 6 from actively attachment is completed to sky
Between fragment connection.
Adhere to 4 observations and manipulation microsatellite 6 in a specific embodiment, on a fragment adapter moonlet 7, when
After fragment adapter moonlet 7 is close with target debris, 6,4 observations of 4 observations and manipulation microsatellite are discharged micro- with manipulation
Observation system above satellite 6 is observed to space junk from different angles respectively, and observation information is passed into fragment connects
Pipe moonlet 7, fragment adapter moonlet 7 analyzes the movement position and attitude information for obtaining space junk.Afterwards, fragment adapter is small
Satellite 7 sends instruction to some observation with manipulation microsatellite 6, and the observation afterwards is adhered to manipulation microsatellite 6 to space junk,
Racemization is carried out to target after attachment, it is in situ that other three observations revert to fragment adapter moonlet 7 again with manipulation microsatellite 6
Put.The observation adhered to space junk is examined by connecting interface between the two with manipulation microsatellite 6 to failure spacecraft
Survey, and pass information to fragment adapter moonlet 7, fragment adapter moonlet 7 is analyzed to information, implement and cooperative target
Docking, after docking using carry mechanical arm system target is repaired, maintenance finished after, space capture mould
Block departs from target, and target continues to complete the task of oneself.
Although present disclosure is discussed in detail by above preferred embodiment, but it should be appreciated that above-mentioned
Description is not considered as limitation of the present invention.After those skilled in the art have read the above, for of the invention
Various modifications and substitutions all will be apparent.Therefore, protection scope of the present invention should be limited to the appended claims.
Claims (8)
1. a kind of space junk based on microsatellite clears up system, it is characterised in that include：
Ground observation and analysis module, for determining the orbital position of space junk and the purpose of space junk process task；
Carrier module, communicates to connect with ground observation and analysis module, and it is according to the instruction of ground observation and analysis module by sky
Between trapping module feeding subscribe track；
Space trapping module, communicates to connect with ground observation and analysis module, and it includes the fragment being mounted in carrier module and connects
Pipe moonlet（7）And it is attached to the fragment adapter moonlet（7）On multiple observations and manipulation microsatellite（6）；Observation and behaviour
Control microsatellite（6）For being observed to obtain observation data, fragment adapter moonlet to space junk（7）For according to observation
Data control observation and manipulation microsatellite（6）Space junk is processed.
2. the space junk based on microsatellite as claimed in claim 1 clears up system, it is characterised in that：
The observation and manipulation microsatellite（6）To space junk after the connection for completing to space junk from the mode of active attachment
Processed.
3. the space junk based on microsatellite as claimed in claim 1 clears up system, it is characterised in that：
Described fragment adapter moonlet（7）The movement position and attitude information of space junk are obtained according to observation data.
4. the space junk based on microsatellite as claimed in claim 1 clears up system, it is characterised in that see on described ground
Survey is included with analysis module：
Large-scale photon telescope（1）, ground radar system（2）, orbit information storehouse（3）, task analysis platform（4）；Large-scale photon
Telescope（1）With ground radar system（2）Observation obtains orbital position of the space junk within the Observable time period, by track
Information bank（3）The orbit information of offer obtains the complete track information of space junk, task analysis platform（4）According to space junk
The launch time of complete orbit information analytical calculation space trapping module, transmitting position, enter the orbit time and injection position.
5. the space junk based on microsatellite as claimed in claim 1 clears up system, it is characterised in that：
In the space trapping module, observe and manipulation microsatellite（6）On be attached with 4 fragment adapter moonlets（7）.
6. a kind of space junk method for cleaning, it is characterised in that using as described in any one in claim 1 ~ 5 based on micro-
The space junk of moonlet clears up system to complete, and the method includes the steps of：
S1, ground observation and analysis module determine the orbital position of space junk and the purpose of space junk process task；
S2, carrier module mounting space trapping module, track is subscribed by space trapping module feeding；
S3, fragment adapter moonlet（7）Close to after space junk, multiple is observed and manipulation microsatellite（6）From different perspectives to sky
Between fragment be observed acquisition observation data；
S4, fragment adapter moonlet（7）Analysis observation data, according to analysis result control observation and manipulation microsatellite（6）To sky
Between fragment processed.
7. space junk method for cleaning as claimed in claim 6, it is characterised in that described step S4 is specifically included：
S41, fragment adapter moonlet（7）Analysis observation data obtain the movement position and attitude information of space junk；
S42, fragment adapter moonlet（7）Defended to the nearest observation of metric space fragment attachment point is micro- with manipulation according to analysis result
Star（6）Send instruction；
S43, chosen observation and manipulation microsatellite（6）Adhere to space junk, racemization is carried out to space junk after attachment, its
Remaining observation and manipulation microsatellite（6）Again fragment adapter moonlet original position is returned.
8. space junk method for cleaning as claimed in claim 7, it is characterised in that in the step S43：
The chosen observation and manipulation microsatellite（6）The mode adhered to from active completes the connection to space junk.
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| CN201710236792.6A CN106850051B (en) | 2017-04-12 | 2017-04-12 | Space debris cleaning system and method based on microsatellite |
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| CN201710236792.6A CN106850051B (en) | 2017-04-12 | 2017-04-12 | Space debris cleaning system and method based on microsatellite |
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| CN106850051B CN106850051B (en) | 2020-04-03 |
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Cited By (10)
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| CN108216686A (en) * | 2017-12-07 | 2018-06-29 | 兰州交通大学 | Space trash method for cleaning based on satellite equipments |
| CN108259077A (en) * | 2017-12-11 | 2018-07-06 | 西北工业大学 | The method and system carried out data transmission using inert satellite antenna |
| CN109421942A (en) * | 2017-08-27 | 2019-03-05 | 南京乐朋电子科技有限公司 | Rotary and telescopic space trash recycles airship |
| CN109444917A (en) * | 2018-10-09 | 2019-03-08 | 中国人民解放军国防科技大学 | Space station external structure detection and maintenance system and method based on micro-nano satellite cluster |
| CN109969433A (en) * | 2019-04-01 | 2019-07-05 | 中国人民解放军国防科技大学 | Space debris batch removing system based on low-earth orbit satellite |
| CN109991680A (en) * | 2019-04-16 | 2019-07-09 | 上海微小卫星工程中心 | A kind of space junk that passively combines led is from perceiving system and method, satellite system |
| CN110002014A (en) * | 2019-03-21 | 2019-07-12 | 武汉大学 | A kind of space junk correlating method and medium |
| CN110254755A (en) * | 2019-07-05 | 2019-09-20 | 中国人民解放军国防科技大学 | Space debris removing device and method and space debris maintenance method |
| CN110341990A (en) * | 2019-07-05 | 2019-10-18 | 中国人民解放军国防科技大学 | Space debris racemization capturing device |
| CN110395412A (en) * | 2019-07-05 | 2019-11-01 | 中国人民解放军国防科技大学 | Space debris clearing system and method and task planning method thereof |
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| CN110341990A (en) * | 2019-07-05 | 2019-10-18 | 中国人民解放军国防科技大学 | Space debris racemization capturing device |
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