CN106516175A - Autonomous operation and control system of agile imaging satellite, and operation process of system - Google Patents
Autonomous operation and control system of agile imaging satellite, and operation process of system Download PDFInfo
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- CN106516175A CN106516175A CN201611059696.0A CN201611059696A CN106516175A CN 106516175 A CN106516175 A CN 106516175A CN 201611059696 A CN201611059696 A CN 201611059696A CN 106516175 A CN106516175 A CN 106516175A
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G3/00—Observing or tracking cosmonautic vehicles
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
- B64G1/1021—Earth observation satellites
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/244—Spacecraft control systems
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- G—PHYSICS
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Abstract
The invention discloses an autonomous operation and control system of an agile imaging satellite. The autonomous operation and control system comprises a ground support system and an imaging satellite. The imaging satellite is equipped with a satellite housekeeping subsystem, an antenna subsystem, rest on-satellite subsystems, a satellite-borne replanning subsystem and a real-time task receiver. After the antenna subsystem receives a multi-source task message, the task requirement message is transmitted to the replanning subsystem, and the replanning subsystem generates a new task planning scheme, on the one hand, the new task planning scheme is transmitted to the antenna subsystem and sent back to a ground operation and control center, on the other hand, an instruction is generated and transmitted to the satellite housekeeping subsystem, and after the operation and control center receives the planning program from the satellite, the control instruction and the digital transmission scheme same with the satellite are synchronously generated, and sent to a measurement and control center and a ground station. The autonomous operation and control system can enhance the ability of the satellite to perform complex tasks; the actual observation efficiency of the tasks on the satellite can be effectively improved; the pressure of a measurement and control channel can be relieved, and the complexity of ground control is decreased; and a response can be effectively quickly made to emergencies.
Description
Technical field
The present invention relates to a kind of quick imaging satellite independently transports control system and its operational process.
Background technology
If an imaging satellite is wanted efficiently to realize earth observation task, Yun Kong centers, measurement and control center, earth station is needed
With completing jointly for satellite in orbit.Ordinary practice in Yun Kong centers, measurement and control center and earth station are referred to as ground support system,
One imaging satellite itself constitutes an On-Star system, generally comprise Star Service subsystem, antenna subsystem, rail control subsystem,
Imaging load subsystem, data storage subsystem, power subsystem and temperature control subsystem etc..
Current observation mission planning is generally carried out on ground, and one day to a couple of days planning horizon, programme has been formulated
Cheng Hou, generates corresponding control instruction, in the star ground time window on note satellite, satellite is implemented to see over the ground in strict accordance with scheme
Survey.
User sends satellite imagery request to satellite Yun Kong centers, generally comprises imaging region according to job demand
The specific demand such as boundary coordinate, the time period for expecting imaging, the degree of priority of task, the selection of imaging pattern.Yun Kong centers
Be responsible for arranging the demand from different user, different satellites, the then pretreatment in task grouping is given by demand assignment
Module will be decomposed into some Meta tasks with reference to satellite orbit and attitude of satellite corner ability etc. complicated user's request, and produce
The plans are finally generated the executable instruction of satellite, after confirmation is errorless, instruction are passed in observing and controlling by mission planning scheme
The heart, notifies that measurement and control center will be noted in instruction to satellite in certain specific time, by the reception plan of receiving station（That is satellite backhaul
The moment and attitude of mission bit stream and satellite state information）Earth station is sent to, notifies earth station before data back in advance
Adjustment aerial angle prepares to receive.
Within a mission planning cycle, the ground support system of satellite disposably above notes all fingers in this cycle
Order.Antenna subsystem sends it to Star Service subsystem at once after being connected to instruction and preserves, and Star Service subsystem is then combined and defended
The information such as star time service and state, controls the action of other subsystems in the moment call instruction block that calls of instruction, including control appearance
Rail control subsystem performs attitude maneuver, imaging load subsystem and performs imaging and its relevant action, data storage subsystem record
Imaging data, power supply and temperature control subsystem corresponding auxiliary movement of execution etc..Respective action is performed after terminating, each subsystem feedback
Implementing result is preserved to Star Service subsystem, is formed assistance data, and is stored in the unification arrangement passback of data storage subsystem.Star Service
Subsystem checks continually on the time of instruction calls and performs corresponding operation, ties until the mission planning cycle corresponding to the instruction
Beam.
Traditional imaging satellite disclosure satisfy that people with the demand of the visual angle acquisition useful information of space, but run management and control efficiency
Still it is relatively low.With the raising of imaging satellite level of hardware, the attainable function of satellite is also increasing.Such as satellite wide-angle
Attitude maneuver ability, the perception to own resource, the continuous enhancing to the perception of real-time task demand, allow satellite to have
Chance from simple instruction executer be changed into can complete independently complex task intelligent body.The enhancing of these abilities, to satellite
Application target have higher requirement, it is clear that only by traditional satellite ground pipe diameter design cannot almost meet it is ageing and
The high satellite observation task of reliability requirement.
The content of the invention
It is an object of the invention to provide a kind of quick imaging satellite independently transports control system and its operational process, being capable of basis
The satellite task programme worked out and the mission requirements for receiving in real time, carry out autonomous local directed complete set to mission planning scheme,
To reduce the non-productive work of satellite, realization is timely responded to real-time task, improves actual observation efficiency.
The quick imaging satellite of the present invention independently transports control system, and including ground support system and imaging satellite, ground is supported
System includes Yun Kong centers, measurement and control center, earth station, and imaging satellite is equipped with Star Service subsystem, antenna subsystem and star other
Subsystem, imaging satellite are further equipped with the receptor of spaceborne weight-normality dividing system and real-time task, the receptor category of real-time task
In antenna subsystem, real-time short message information exchange is carried out for imaging satellite and user, imaging satellite and ground support system,
Spaceborne weight-normality dividing system, mainly realizes the online mission planning function of all observation missions in system, pre- including at least task
Processing module, task weight planning module and directive generation module, task pretreatment module is for being several yuan by goal decomposition
Task, then according to satellitosis and orbit information by the Target indication information of each Meta task（The geographical position of task object
Information）It is converted into goal directed information（The information such as the SEE time window of target）；Task weight planning module receives pre-processed results,
Cost is calculated with reference to assigned tasks information analysiss, is independently selected suitable method for solving to be solved, and is generated mission planning side
Case；The mission planning scheme for generating is combined satellite command template generation satellite command by directive generation module, is passed to Star Service point and is
System is performed.
The quick imaging satellite of the present invention independently transports the operational process of control system, including：When antenna subsystem receive it is many
After originating task information, weight-normality dividing system is given by mission requirements information transmission, weight-normality dividing system then calls other points to be immediately
The status information of system, is adjusted to original mission planning scheme with reference to all information, generates a new mission planning scheme,
On the one hand new mission planning scheme is passed to into antenna subsystem, and is returned to ground Yun Kong centers, on the one hand generated instruction, pass
Star Service subsystem is passed, it is while instruction is generated, after Yun Kong centers are connected to the programme of satellite, identical on synchronous generation star
Control instruction sum pass plan, be sent respectively to measurement and control center and earth station, earth station and measurement and control center coordinate satellite to complete
A series of imaging task, eventually receives image information, and is distributed to user after being processed into the intelligible product of user.
Further, the multi-source mission bit stream, can derive from ground support system, can be from terrestrial user
Vital task or the contingency tasks generated according to its information for getting that handheld terminal, or other satellites are not completed.
The quick imaging satellite of the present invention independently transports control system, and the real time information obtained on star can be made full use of to carry out soon
Fast task is processed and planning, and satellite is performed according to set mission planning scheme, and can obtain unknown mission bit stream in real time, when
Satellite reception can be carried out to programme from main modulation to after real-time task information, ensureing that mission planning scheme is relatively steady
Total benefit as high as possible is obtained on the premise of fixed.Compared to tradition fortune control system, autonomous fortune control system can lift satellite execution
The ability of complex task；Star can effectively be lifted to take up an official post pragmatic border observed efficiency；The pressure of observing and controlling passage can be alleviated, ground line is reduced
The complexity of control；Can effectively, the emergent accident of quick response.
Description of the drawings
Fig. 1 is the autonomous fortune control cooperative system figure of the present invention.
Specific embodiment
The autonomous fortune control system of the present invention is equipped with the reception of spaceborne weight-normality dividing system and real-time task on imaging satellite
Device.Weight-normality dividing system mainly realizes the online mission planning function of all observation missions in system, and current task can be advised
Draw the cycle in task disposably planned according to constraints and resource situation, also can be with reference to original mission planning scheme
The weight-normality that newly arrived contingency tasks are carried out with task is drawn, and meets the requirement of real-time of emergency scheduling；The receptor of real-time task
Belong to antenna subsystem, real-time short message information exchange, i.e. user is carried out for satellite and user, satellite and ground support system
Mission requirements information can be sent to satellite using Big Dipper short message by different terminals, satellite can be by the reception of real-time task
Qi Xiangyunkong centers send task weight programme.
Weight-normality dividing system is including at least three big modules：Task pretreatment module, task weight planning module and instruction life
Into module.
The function of task pretreatment module be by goal decomposition be several Meta tasks, then according to satellitosis and track
The Target indication information of each Meta task is converted into goal directed information by information.So-called Target indication information just refers to task mesh
Target geographical location information, represents generally with the longitude and latitude of target and altitude information；Goal directed information is exactly feeling the pulse with the finger-tip target
The information such as SEE time window, the satellite fixed with a certain are relevant, represent that the satellite can be to the target imaging when.For
General user, they simultaneously do not know about the information such as the orbit parameter of being yet indifferent to satellite, propose to provide Target indication during demand
Information, it is necessary to which it is goal directed information to be arranged by the task pretreatment module in satellite weight-normality dividing system, directly could be weighed
Planning algorithm is directly used, the typically Target indication information such as mission requirements that general business user and other satellites are transmitted.It is right
In a part of special user, which submits to the terminal of demand possess the function of task pretreatment, such as the office worker at Yun Kong centers,
User of special movement terminal etc. directly can send goal directed information to satellite, make full use of ground based terminal computing capability
The characteristics of strong, computing pressure on star is greatly decreased, also shorten from user propose demand to the whole closed loop for receiving data when
Between.
After task pretreatment module terminates, pre-processed results（That is goal directed information）Task weight planning module is delivered to,
Task weight planning module then carrys out analytical calculation cost with reference to assigned tasks information, independently selects suitable method for solving to be asked
Solution, and generate mission planning scheme.On the one hand weight-normality dividing system passes weight programme back ground by antenna subsystem, separately
On the one hand scheme is passed to into directive generation module, scheme is combined satellite command template generation satellite command by directive generation module,
Pass to the execution of Star Service subsystem.
On star, the source of the task requests that autonomous weight-normality is drawn is various, can both derive from ground support system, can be with
From the handheld terminal of terrestrial user, if there is the vital task not completed or the information life got according to which in other satellites
Into contingency tasks can also be used as the input information of weight-normality dividing system.
It is as follows that quick imaging satellite independently transports control system operation flow process：When antenna subsystem receives multi-source mission bit stream
Afterwards, then the state of other subsystems is called to believe immediately to weight-normality dividing system, weight-normality dividing system mission requirements information transmission
Breath, is adjusted to original mission planning scheme with reference to all information, generates a new mission planning scheme, on the one hand will be new
Mission planning scheme pass to antenna subsystem, and be returned to ground Yun Kong centers, on the one hand generate instruction, pass to Star Service point
System, it is while instruction is generated, after Yun Kong centers are connected to the programme of satellite, synchronous to generate identical control instruction on star
Sum passes plan, is sent respectively to measurement and control center and earth station, earth station and measurement and control center coordinate satellite complete it is a series of into
As task, image information is eventually received, and user is distributed to after being processed into the intelligible product of user.
Above-mentioned specific embodiment is the invention is not limited in, some details of the embodiment of the present invention should not be constituted to this
The restriction of invention, those skilled in the art are without departing from design concept of the present invention and scope of the claimed protection
In the case of, the various modifications made to technical scheme and improvement all should drop into protection scope of the present invention.
Claims (3)
1. quick imaging satellite independently transports control system, including ground support system and imaging satellite, the ground support system bag
Kuo Yunkong centers, measurement and control center, earth station, imaging satellite are equipped with other subsystems on Star Service subsystem, antenna subsystem and star,
It is characterized in that：Imaging satellite is further equipped with the receptor of spaceborne weight-normality dividing system and real-time task, the reception of real-time task
Device belongs to antenna subsystem, carries out real-time short message information for imaging satellite and user, imaging satellite and ground support system
Interaction, spaceborne weight-normality dividing system mainly realizes the online mission planning function of all observation missions in system, including at least appointing
Business pretreatment module, task weight planning module and directive generation module, task pretreatment module is for being some by goal decomposition
Individual Meta task, then according to satellitosis and orbit information by the Target indication information of each Meta task（The geography of task object
Positional information）It is converted into goal directed information（The information such as the SEE time window of target）；Task weight planning module receives pretreatment
As a result, cost is calculated with reference to assigned tasks information analysiss, independently select suitable method for solving to be solved, and generate task rule
The scheme of drawing；The mission planning scheme for generating is combined satellite command template generation satellite command by directive generation module, passes to Star Service
Subsystem is performed.
2. agility imaging satellite as claimed in claim 1 independently transports the operational process of control system, it is characterised in that include：When
After antenna subsystem receives multi-source mission bit stream, weight-normality dividing system, weight-normality dividing system is given by mission requirements information transmission
The status information of other subsystems is then called immediately, original mission planning scheme is adjusted with reference to all information, generate one
On the one hand new mission planning scheme is passed to antenna subsystem, and is returned in the fortune control of ground by individual new mission planning scheme
The heart, on the one hand generates instruction, passes to Star Service subsystem, and while instruction is generated, Yun Kong centers are connected to the planning side of satellite
It is after case, synchronous to generate identical control instruction sum on star and pass plan, be sent respectively to measurement and control center and earth station, earth station and
Measurement and control center coordinates satellite to complete a series of imaging task, eventually receives image information, and is processed into user Ke Li
User is distributed to after the product of solution.
3. agility imaging satellite as claimed in claim 2 independently transports the operational process of control system, it is characterised in that：The multi-source
Mission bit stream, can derive from ground support system, can be from the handheld terminal of terrestrial user, or other satellites
Unfinished vital task or the contingency tasks generated according to its information for getting.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
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| CN201611059696.0A CN106516175B (en) | 2016-11-28 | 2016-11-28 | Quick imaging satellite independently transports control system and its operational process |
| GB1719540.5A GB2559024B (en) | 2016-11-28 | 2017-11-24 | Autonomous operation and control system of agile imaging satellite |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
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| CN201611059696.0A CN106516175B (en) | 2016-11-28 | 2016-11-28 | Quick imaging satellite independently transports control system and its operational process |
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| CN106516175A true CN106516175A (en) | 2017-03-22 |
| CN106516175B CN106516175B (en) | 2018-11-27 |
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| CN106742086A (en) * | 2016-11-28 | 2017-05-31 | 中国人民解放军国防科学技术大学 | Quick imaging satellite independently transports control system |
| CN107590046A (en) * | 2017-09-05 | 2018-01-16 | 北京空间飞行器总体设计部 | A kind of remote sensing satellite load task command verification method and system |
| CN108021433A (en) * | 2017-12-01 | 2018-05-11 | 中国人民解放军国防科技大学 | Target observation method for multi-satellite cluster |
| CN109102195A (en) * | 2018-08-21 | 2018-12-28 | 深圳市天智运控科技有限公司 | A kind of satellite Autonomous rolls task configuration method and system online |
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Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1997026187A1 (en) * | 1996-01-19 | 1997-07-24 | Itt Manufacturing Enterprises, Inc. | Satellite exclusion zone viewing and control system |
| JP2009179141A (en) * | 2008-01-30 | 2009-08-13 | Mitsubishi Electric Corp | Satellite observation system |
| CN102305630A (en) * | 2011-05-17 | 2012-01-04 | 哈尔滨工业大学 | Autonomous synthetic aperture radar (SAR) satellite orbit determination method based on extended kalman filter |
| CN102479085A (en) * | 2010-11-30 | 2012-05-30 | 中国人民解放军国防科学技术大学 | Agile satellite task planning method |
| CN102866709A (en) * | 2012-07-20 | 2013-01-09 | 航天东方红卫星有限公司 | Method for implementing in-orbit maneuvering imaging task of agile earth observing satellite |
| JP2014172553A (en) * | 2013-03-12 | 2014-09-22 | Mitsubishi Electric Corp | Satellite control system |
| CN105511482A (en) * | 2015-11-30 | 2016-04-20 | 上海卫星工程研究所 | Mode regulation and control method for autonomous imaging task planning |
| CN106742086A (en) * | 2016-11-28 | 2017-05-31 | 中国人民解放军国防科学技术大学 | Quick imaging satellite independently transports control system |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109076192B (en) * | 2016-02-29 | 2022-04-05 | 优鲁格斯股份有限公司 | Planet scale analysis system |
-
2016
- 2016-11-28 CN CN201611059696.0A patent/CN106516175B/en not_active Expired - Fee Related
-
2017
- 2017-11-24 GB GB1719540.5A patent/GB2559024B/en active Active
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1997026187A1 (en) * | 1996-01-19 | 1997-07-24 | Itt Manufacturing Enterprises, Inc. | Satellite exclusion zone viewing and control system |
| JP2009179141A (en) * | 2008-01-30 | 2009-08-13 | Mitsubishi Electric Corp | Satellite observation system |
| CN102479085A (en) * | 2010-11-30 | 2012-05-30 | 中国人民解放军国防科学技术大学 | Agile satellite task planning method |
| CN102305630A (en) * | 2011-05-17 | 2012-01-04 | 哈尔滨工业大学 | Autonomous synthetic aperture radar (SAR) satellite orbit determination method based on extended kalman filter |
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Also Published As
| Publication number | Publication date |
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| CN106516175B (en) | 2018-11-27 |
| GB201719540D0 (en) | 2018-01-10 |
| GB2559024B (en) | 2020-09-23 |
| GB2559024A (en) | 2018-07-25 |
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