CN109188468A - A kind of ground monitoring system monitoring satellite health - Google Patents
A kind of ground monitoring system monitoring satellite health Download PDFInfo
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- CN109188468A CN109188468A CN201811066279.8A CN201811066279A CN109188468A CN 109188468 A CN109188468 A CN 109188468A CN 201811066279 A CN201811066279 A CN 201811066279A CN 109188468 A CN109188468 A CN 109188468A
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/01—Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/13—Receivers
- G01S19/20—Integrity monitoring, fault detection or fault isolation of space segment
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- Testing And Monitoring For Control Systems (AREA)
Abstract
The application provides a kind of ground monitoring system for monitoring satellite health, it includes emulation part, correction portion and monitor portion, wherein satellite orbit, illumination condition, energy scenario, pose adjustment situation, TTC channel and/or thermal control state of the simulation part point for satellite in simulation calculation future time；Wherein the correction portion is used to be modified the emulation data and simulation model that emulate in part based on true satellite data；And the satellite time of day data that wherein monitor portion is used to receive the incoming satellite simulation status data in the emulation part and the correction portion is passed to, and judge whether the satellite simulation status data or the satellite time of day data are in the normal range (NR) of setting.The ground monitoring system of the application carries out estimation calculating to satellitosis when that can not receive satellite time of day information, through emulation mode, promotes the Real-time Monitor Management ability to the satellite whole service period.
Description
Technical field
This application involves satellite simulation technical field more particularly to a kind of ground monitoring systems for monitoring satellite health
System.
Background technique
Since satellite cost is high, need to pay close attention to satellite health constantly, with guarantee satellite normal operation and into
The quick troubleshooting of row.Satellite and ground, which are passed satellite telemetry state come under by ground control station and uploads satellite control, to be referred to
It enables.When grounded receiving station cannot receive signal or earth station does not have sufficient resources and satellite to carry out telemetry communication, satellite
State is in unknown state, so that satellite transit faces more risk, it, cannot be timely especially when satellite is in malfunction
It was found that.
When ground is unsatisfactory for condition of acceptance, the general method using satellitosis storage, when meeting with ground communication,
The satellite telemetry state currently stored and the satellite telemetry state stored before are issued into ground, ground passes through data readback
Mode inquires satellitosis to confirm whether satellite is in normal condition.This method can monitor satellite whole service to a certain degree
The operating status in period, but also face following problems: 1, satellite established with earth station communicate before break down (such as the energy
Shortage, track deviation etc.) when, it cannot find in time, just find that failure, failure fail to handle in time when communicating with earth station, it is special
It is not period longer satellite, fault discovery real-time is poor；2, storage resource is limited on star, if long-term do not establish with ground is led to
Believe failure, satellite state information before may be capped, so that ground lack part data, may lose important information.
In short, current ground monitoring system only monitors satellitosis when satellite is communicated with earth station, low orbit satellite
Face telemetry communication duration is usually a few minutes to more than ten minutes, so that only a small part time satellite period is in prison
Control state.It, can only be right although can be played back using the method for satellite telemetry status information storage to satellite turntable data
Past information is monitored.
For this purpose, there is an urgent need in the art to develop a kind of ground that can monitor satellite whole service periodic duty state in real time
Monitoring system.
Summary of the invention
The application's is designed to provide a kind of ground prison that can monitor satellite whole service periodic duty state in real time
Control system, thus solve it is above-mentioned in the prior art the technical issues of.The present invention establishes a kind of satellite ground monitoring system, in satellite
When cannot be communicated with earth station, expected calculating is carried out to satellitosis by emulation technology, provides the state of satellite transit process
Predictive information；When satellite immigration is communicated with tracking telemetry and command station, simulation model is automatically corrected using the information received
And calculating parameter amendment, to promote ground system simulation capacity.System is all monitored the state and time of day of emulation,
Warning message is provided in time, so that ground staff makes fault countermeasure response as early as possible.
In order to solve the above-mentioned technical problem, the application provides following technical proposals.
In the first aspect, the application provides a kind of ground monitoring system for monitoring satellite health, the ground prison
Control system includes emulation part, correction portion and monitor portion, wherein the simulation part point is in simulation calculation future time
Satellite orbit, illumination condition, energy scenario, pose adjustment situation, TTC channel and/or the thermal control state of satellite；
Wherein the correction portion is used for based on true satellite data to the emulation data and emulation mould in emulation part
Type is modified；
And wherein the monitor portion is used to receive the incoming satellite simulation status data in the emulation part and the school
The incoming satellite time of day data of positive part, and judge the satellite simulation status data or the satellite time of day data are
The no normal range (NR) in setting.
In a kind of embodiment of first aspect, the simulation part point is emulated including satellite trajectory simulation module, the energy
Module, observing and controlling emulation module, Attitude Simulation module, thermal control emulation module and load emulation module, and each emulation module passes through number
Data interaction is carried out according to library.
In a kind of embodiment of first aspect, the monitoring system only emulates satellite health, single to load etc.
Machine performance only emulates single machine switch motion and energy consumption without emulation.
In a kind of embodiment of first aspect, emulate the load of satellite using load emulation module
When, need tracking telemetry and command station that load schedule work is transmitted to the load emulation module.
In a kind of embodiment of first aspect, track emulation module carries out orbit computation and illumination using HPOP model
It calculates, the input as other emulation modules.
In a kind of embodiment of first aspect, the track emulation module needs external input track six roots of sensation number to believe
Breath, the information is by tracking telemetry and command station to providing after satellite orbit determination.
In a kind of embodiment of first aspect, the information in emulation cycle is output to number by the track emulation module
It is called according to library for other emulation modules, wherein emulation cycle is the interval time that satellite and ground control station establish communication twice,
The information includes at least co-ordinates of satellite, satellite light application time and the satellite load working condition under body-fixed coordinate system.
In a kind of embodiment of first aspect, satellite orbit that Attitude Simulation module exports track emulation module and
The working condition of illumination condition and load carries out corresponding posture movement.
In a kind of embodiment of first aspect, thermal control emulation module is according to the illumination condition and appearance of track emulation module
The posture information of state emulation module, in conjunction with the heat power consumption state of single machine on star, each Thermal control units of simulation calculation need to take
Movement.
In a kind of embodiment of first aspect, observing and controlling emulation module is according to satellite orbit, the attitude of satellite and observing and controlling day
Linear state calculates satellite immigration time and Satellite TT antenna and earth station's angle and satellite TT&C surplus.
In a kind of embodiment of first aspect, load emulation module does not examine load operation performance, according to input
Load schedule work generates relevant action sequence, the input emulated as pose adjustment and energy computation.
In a kind of embodiment of first aspect, the illumination condition of energy emulation module combination track emulation module, appearance
The pose adjustment information and thermal control emulation module of state emulation module, load emulation module, observing and controlling emulation module single machine switch
Machine situation calculates the energy consumption situation in entire emulation cycle.
In a kind of embodiment of first aspect, when the energy is unsatisfactory for condition, energy emulation module provides alarm signal
Breath.
In a kind of embodiment of first aspect, mould is emulated in satellite trajectory simulation module, energy emulation module, observing and controlling
After block, Attitude Simulation module, thermal control emulation module and load emulation module complete emulation, satellite simulation status data is generated.
In a kind of embodiment of first aspect, to the emulation data of emulation part and imitated based on true satellite data
True mode is modified the difference including comparing emulation telemetering output data and the practical telemetry of satellite, seeks the difference of the two
Feed back input as dummy satellite makes the two difference minimum.
In a kind of embodiment of first aspect, the correction portion is also used to make using the real-time telemetry information of satellite
For emulate part current input, into the emulation of next round；And/or the satellite telemetry information that tracking telemetry and command station forwards is transmitted to
Monitor portion, to be monitored to truthful data.
In a kind of embodiment of first aspect, when satellite simulation status data or the satellite time of day data not
When in normal range (NR), the monitor portion exports warning message.
Compared with prior art, the beneficial effects of the present application are as follows ground monitoring system as described herein can obtain satellite
Condition monitoring is carried out to real satellite data when telemetering state, when satellite time of day information can not be received, by emulation side
Formula carries out estimation calculating to satellitosis, promotes the Real-time Monitor Management ability to the satellite whole service period.
Figure of description
Fig. 1 schematically shows the schematic diagram of the ground monitoring system according to the application.
Specific embodiment
To keep the purposes, technical schemes and advantages of the application clearer, below in conjunction with the application specific embodiment and
Technical scheme is clearly and completely described in corresponding attached drawing.Obviously, described embodiment is only the application one
Section Example, instead of all the embodiments.Based on the embodiment in the application, those of ordinary skill in the art are not doing
Every other embodiment obtained under the premise of creative work out, shall fall in the protection scope of this application.
In a specific embodiment, the present invention establishes a kind of monitoring system on ground, which has satellite transit
Simulation capacity can be to satellite orbit, illumination condition, energy scenario, the pose adjustment in future time after giving primary condition
Situation, TTC channel, thermal control state carry out simulation calculation.Meanwhile the system is connected with ground control station, in satellite and tracking telemetry and command station
When communication, the satellite telemetry status information that satellite passes down is transmitted to monitoring system, the monitoring system information by ground control station
Modifying model and data correction are carried out to itself；For the satellite for needing to infuse planning tasks arrangement of time on ground, tracking telemetry and command station is also needed
Planning tasks information is transmitted to monitoring system, so that monitoring system carries out Attitude Simulation and energy consumption calculating.
In a specific embodiment, monitoring system includes satellite simulation part, correction portion and monitor portion.Emulation
Part has general satellite transit simulation capacity, includes satellite trajectory simulation, energy emulation, observing and controlling emulation, Attitude Simulation, heat
Control emulation, load emulation, each emulation module carry out data interaction by database.The monitoring system only emulates satellite transit shape
State to the single machines such as load performance without emulation, therefore only emulates single machine switch motion and energy consumption.Due to load task one
As by after floor planning pass through tracking telemetry and command station on note arrive satellite, therefore tracking telemetry and command station need for planning tasks timetable to be transmitted to monitoring be
System is so as to monitoring system simulation load relevant action.
Even if satellite simulation part is emulated using accurate model, after long-time simulation calculation, accumulative mistake can be generated
Difference, if may cause the warning message of mistake to error without correction to reduce the confidence level of monitoring system.For this purpose, mould
The true telemetering state information that type introduces satellite is modified simulation model and emulation data, the accuracy of lift scheme.School
Positive part includes two aspects: first is that the satellite state information stored before issued by satellite, just repairs simulation model
Just；Second is that using the real-time telemetry information of satellite as the current input of emulation part, into the emulation of next round.
The simulation status information and the true telemetering state information of the received satellite of correction portion for emulating part are all exported and are given
Monitor portion, monitor portion are configured by ground staff, set the normal range (NR) of each telemetering amount, monitor portion after going beyond the scope
Provide warning message.If the warning message that simulation part is given out, ground staff takes corresponding prediction scheme for warning message,
Confirm whether fault message is accurate and carries out by true telemetering state when satellite immigration next time is communicated with ground control station machine
Corresponding prediction scheme processing promotes the failure response speed to satellite to achieve the purpose that monitoring and carry out prediction scheme preparation in advance.
Fig. 1 schematically shows the schematic diagram of the ground monitoring system according to the application.This is described in detail below in conjunction with Fig. 1
The ground monitoring system of application.
Emulate part
Track emulation part carries out orbit computation and illumination calculation using HPOP model, as the defeated of other emulation modules
Enter.Track emulation part needs external input track six roots of sensation number information, and the information is by tracking telemetry and command station to providing after satellite orbit determination.
Orbit information includes the co-ordinates of satellite under body-fixed coordinate system, satellite light application time, and emulation part is defeated by the information in emulation cycle
Database is arrived out to call for other emulation modules.When emulation cycle is that satellite establishes the interval of communication with ground control station twice
Between.
Track is emulated the satellite orbit of part output and the working condition of illumination condition and load by Attitude Simulation part
Carry out corresponding posture movement.For example, generating Direct to the sun adjustment in area of illumination, when shadow region and load operation, takes absolute orientation
Or other specific directions, the strategy are set by ground staff.Attitude Simulation also needs to calculate satellite sun windsurfing and the sun
Angle, the input calculated as output as energy charging.
Thermal control emulation part emulates the illumination condition of part and the posture information of Attitude Simulation according to track, in conjunction with single on star
The heat power consumption state of machine, the movement that each Thermal control units of simulation calculation need to take, simulation result, which is exported, emulates part to the energy
It is referred to as calculating.
Observing and controlling emulation according to satellite orbit, the attitude of satellite and itself TT&C antenna state, calculate the satellite immigration time and
Satellite TT antenna and earth station's angle calculate satellite TT&C surplus.
Load emulation part does not examine load operation performance, generates relevant movement sequence according to the load schedule work of input
Column, the input emulated as pose adjustment and energy computation.
Energy emulation part combine the track emulation illumination condition of part, Attitude Simulation part pose adjustment information and
The switching on and shutting down situation of the single machines such as thermal control, load, observing and controlling calculates energy consumption situation in entire emulation cycle, the energy not
When meeting condition, warning message is provided.
For convenience of being managed to the data in each emulation module, modules carry out data interaction by database.
After each emulation module completes emulation, satellite simulation status data is generated, and export to monitor portion.
Correction portion
Since there are phantom errors for emulation part, true satellite data is needed to repair emulation data and simulation model
Just.Satellite can issue the satellite state data of satellite current time and time storage before when being communicated with earth station,
Simulation model can be modified using these data.Makeover process are as follows: compare emulation telemetering output data and satellite is practical
The difference of telemetry, the difference for seeking the two make the two difference minimum as the feed back input of dummy satellite.Ground simulation
Model enters the emulation of next round using the current data of satellite as original state after the completion of correction.Correction portion also needs
The satellite telemetry confidence that tracking telemetry and command station forwards is transmitted to monitor portion, to be monitored to truthful data.
Monitor portion
Monitor portion receives the incoming true shape of satellite of emulation part incoming satellite simulation status data and correction portion
State data.Wherein, the satellite simulation status data for emulating part obtains for simulation calculation, the satellite time of day number of correction portion
According to the satellite time of day telemetry intelligence (TELINT) obtained for ground control station.Whether the more each telemetry intelligence (TELINT) of monitor portion is in normal
Range, when the telemetry of satellite simulation state or the telemetry of satellite time of day are in abnormal range, output
Warning message.
It should also be noted that, the terms "include", "comprise" or its any other variant are intended to nonexcludability
It include so that the process, method, commodity or the equipment that include a series of elements not only include those elements, but also to wrap
Include other elements that are not explicitly listed, or further include for this process, method, commodity or equipment intrinsic want
Element.In the absence of more restrictions, the element limited by sentence "including a ...", it is not excluded that including described want
There is also other identical elements in the process, method of element, commodity or equipment.
The above-mentioned description to embodiment is that this Shen can be understood and applied for the ease of those skilled in the art
Please.Person skilled in the art obviously easily can make various modifications to these embodiments, and described herein
General Principle is applied in other embodiments without paying creative labor.Therefore, the application is not limited to implementation here
Example, those skilled in the art make according to herein disclosed content in the case where not departing from the application scope and spirit
It improves and modifies within all scope of the present application.
Claims (17)
1. a kind of ground monitoring system for monitoring satellite health, the ground monitoring system includes emulation part, correction unit
Point and monitor portion, wherein satellite orbit, illumination condition, the energy of the simulation part point for satellite in simulation calculation future time
Source situation, pose adjustment situation, TTC channel and/or thermal control state；
Wherein the correction portion be used for based on true satellite data to emulation part in emulation data and simulation model into
Row amendment；
And wherein the monitor portion is used to receive the incoming satellite simulation status data in the emulation part and the correction unit
Divide incoming satellite time of day data, and judges whether the satellite simulation status data or the satellite time of day data are located
In the normal range (NR) of setting.
2. satellite health ground monitoring system as described in claim 1, which is characterized in that the simulation part point includes defending
Star orbital road emulation module, energy emulation module, observing and controlling emulation module, Attitude Simulation module, thermal control emulation module and load emulation
Module, and each emulation module carries out data interaction by database.
3. satellite health ground monitoring system as claimed in claim 2, which is characterized in that the monitoring system only emulates
Satellite health to the single machines such as load performance without emulation, therefore only emulates single machine switch motion and energy consumption.
4. satellite health ground monitoring system as claimed in claim 2, which is characterized in that utilizing load emulation module
When emulate to the load of satellite, need tracking telemetry and command station that load schedule work is transmitted to the load emulation module.
5. satellite health ground monitoring system as claimed in claim 2, which is characterized in that track emulation module uses
HPOP model carries out orbit computation and illumination calculation, the input as other emulation modules.
6. satellite health ground monitoring system as claimed in claim 5, which is characterized in that the track emulation module needs
Want external input track six roots of sensation number information, the information is by tracking telemetry and command station to providing after satellite orbit determination.
7. satellite health ground monitoring system as claimed in claim 5, which is characterized in that the track emulation module will
Information in emulation cycle is output to database and calls for other emulation modules, and wherein emulation cycle is satellite and ground control station
Establish twice the interval time of communication, the information include at least body-fixed coordinate system under co-ordinates of satellite, satellite light application time and
Satellite load working condition.
8. satellite health ground monitoring system as claimed in claim 2, which is characterized in that Attitude Simulation module is by track
The satellite orbit and illumination condition of emulation module output and the working condition of load carry out corresponding posture movement.
9. satellite health ground monitoring system as claimed in claim 2, which is characterized in that thermal control emulation module is according to rail
The illumination condition of road emulation module and the posture information of Attitude Simulation module, in conjunction with the heat power consumption state of single machine on star, emulation meter
Calculate the movement that each Thermal control units need to take.
10. satellite health ground monitoring system as claimed in claim 2, which is characterized in that observing and controlling emulation module according to
Satellite orbit, the attitude of satellite and TT&C antenna state calculate satellite immigration time and Satellite TT antenna and earth station's angle
And satellite TT&C surplus.
11. satellite health ground monitoring system as claimed in claim 2, which is characterized in that load emulation module is not examined
Core load operation performance generates relevant action sequence according to the load schedule work of input, as pose adjustment and energy computation
The input of emulation.
12. satellite health ground monitoring system as claimed in claim 2, which is characterized in that energy emulation module combines
The illumination condition of track emulation module, the pose adjustment information of Attitude Simulation module and thermal control emulation module, load emulate mould
The switching on and shutting down situation of block, observing and controlling emulation module single machine calculates the energy consumption situation in entire emulation cycle.
13. satellite health ground monitoring system as claimed in claim 12, which is characterized in that be unsatisfactory for condition in the energy
When, energy emulation module provides warning message.
14. satellite health ground monitoring system as claimed in claim 2, which is characterized in that in satellite trajectory simulation mould
Block, energy emulation module, observing and controlling emulation module, Attitude Simulation module, thermal control emulation module and load emulation module complete emulation
Afterwards, satellite simulation status data is generated.
15. satellite health ground monitoring system as described in claim 1, which is characterized in that be based on true satellite number
It is actually distant including comparing emulation telemetering output data and satellite according to being modified to the emulation data and simulation model that emulate part
The difference of measured data, the difference for seeking the two make the two difference minimum as the feed back input of dummy satellite.
16. satellite health ground monitoring system as described in claim 1, which is characterized in that the correction portion is also used
In using the real-time telemetry information of satellite as emulation part current input, into the emulation of next round；
And/or the satellite telemetry information that tracking telemetry and command station forwards is transmitted to monitor portion, to be monitored to truthful data.
17. satellite health ground monitoring system as described in claim 1, which is characterized in that when satellite simulation status number
According to or the satellite time of day data be not at normal range (NR) when, the monitor portion exports warning message.
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110471311A (en) * | 2019-08-15 | 2019-11-19 | 南京理工大学 | A kind of micro-nano satellite rail control semi-physical simulation synthesis experiment platform |
| CN110689505A (en) * | 2019-12-11 | 2020-01-14 | 长沙天仪空间科技研究院有限公司 | Scene-based satellite-borne remote sensing instrument self-adaptive correction method and system |
| CN111258305A (en) * | 2020-03-06 | 2020-06-09 | 哈工大机器人（岳阳）军民融合研究院 | Satellite operation control center system, equipment management method, equipment and storage medium |
| CN111483615A (en) * | 2020-04-17 | 2020-08-04 | 中国科学院微小卫星创新研究院 | Method for realizing pointing posture of quantum satellite to ground optical station |
| CN113867176A (en) * | 2021-10-12 | 2021-12-31 | 中国科学院空天信息创新研究院 | Satellite receiving station monitoring simulation system |
| CN114285455A (en) * | 2021-12-16 | 2022-04-05 | 广州爱浦路网络技术有限公司 | Satellite energy-saving control method, system, device and storage medium based on core network |
Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1876502A (en) * | 2006-07-07 | 2006-12-13 | 中国科学院力学研究所 | On-line correction method of satellite flight parameter |
| CN1923622A (en) * | 2006-07-07 | 2007-03-07 | 中国科学院力学研究所 | Real-time prediction method for satellite flight parameter |
| US20070129922A1 (en) * | 2005-12-01 | 2007-06-07 | Electronics And Telecommunications Research Institute | Satellite simulation system using component-based satellite modeling |
| CN102521953A (en) * | 2011-11-15 | 2012-06-27 | 北京空间飞行器总体设计部 | Method for recording and downloading satellite measured and controlled telemetry parameters of invisible arc section |
| CN103646127A (en) * | 2013-11-20 | 2014-03-19 | 中国空间技术研究院 | Satellite orbit gesture visual three-dimensional displaying method |
| CN103970034A (en) * | 2014-05-21 | 2014-08-06 | 航天东方红卫星有限公司 | Moonlet control subsystem work state automatic interpretation system |
| CN105205288A (en) * | 2015-10-28 | 2015-12-30 | 中国人民解放军国防科学技术大学 | Mode evolution-based forecasting method for satellite long-term on-orbit running state |
| US20160131737A1 (en) * | 2013-06-24 | 2016-05-12 | Airbus Defense And Space Sas | Method and system for monitoring a phase for transferring a satellite from an intial orbit to a mission orbit |
| CN106374993A (en) * | 2016-08-31 | 2017-02-01 | 长光卫星技术有限公司 | Full-automatic unattended satellite telemetering monitoring platform and data processing method |
| EP3189436A2 (en) * | 2014-09-05 | 2017-07-12 | FTS Computertechnik GmbH | Computer system and method for safety-critical applications |
| EP3373042A1 (en) * | 2015-11-06 | 2018-09-12 | Korea Aerospace Research Institute | Simulation device of satellite, and method therefor |
-
2018
- 2018-09-13 CN CN201811066279.8A patent/CN109188468B/en active Active
Patent Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20070129922A1 (en) * | 2005-12-01 | 2007-06-07 | Electronics And Telecommunications Research Institute | Satellite simulation system using component-based satellite modeling |
| CN1876502A (en) * | 2006-07-07 | 2006-12-13 | 中国科学院力学研究所 | On-line correction method of satellite flight parameter |
| CN1923622A (en) * | 2006-07-07 | 2007-03-07 | 中国科学院力学研究所 | Real-time prediction method for satellite flight parameter |
| CN102521953A (en) * | 2011-11-15 | 2012-06-27 | 北京空间飞行器总体设计部 | Method for recording and downloading satellite measured and controlled telemetry parameters of invisible arc section |
| US20160131737A1 (en) * | 2013-06-24 | 2016-05-12 | Airbus Defense And Space Sas | Method and system for monitoring a phase for transferring a satellite from an intial orbit to a mission orbit |
| CN103646127A (en) * | 2013-11-20 | 2014-03-19 | 中国空间技术研究院 | Satellite orbit gesture visual three-dimensional displaying method |
| CN103970034A (en) * | 2014-05-21 | 2014-08-06 | 航天东方红卫星有限公司 | Moonlet control subsystem work state automatic interpretation system |
| EP3189436A2 (en) * | 2014-09-05 | 2017-07-12 | FTS Computertechnik GmbH | Computer system and method for safety-critical applications |
| CN105205288A (en) * | 2015-10-28 | 2015-12-30 | 中国人民解放军国防科学技术大学 | Mode evolution-based forecasting method for satellite long-term on-orbit running state |
| EP3373042A1 (en) * | 2015-11-06 | 2018-09-12 | Korea Aerospace Research Institute | Simulation device of satellite, and method therefor |
| CN106374993A (en) * | 2016-08-31 | 2017-02-01 | 长光卫星技术有限公司 | Full-automatic unattended satellite telemetering monitoring platform and data processing method |
Non-Patent Citations (2)
| Title |
|---|
| PEIJUN YU: ""A satellite monitor system based on behavior-prediction"", 《2010 3RD INTERNATIONAL SYMPOSIUM ON SYSTEMS AND CONTROL IN AERONAUTICS AND ASTRONAUTICS》 * |
| 杨淑珍 等: ""基于Labview的卫星电源地面监控***研究"", 《计算机测量与控制》 * |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110471311A (en) * | 2019-08-15 | 2019-11-19 | 南京理工大学 | A kind of micro-nano satellite rail control semi-physical simulation synthesis experiment platform |
| CN110689505A (en) * | 2019-12-11 | 2020-01-14 | 长沙天仪空间科技研究院有限公司 | Scene-based satellite-borne remote sensing instrument self-adaptive correction method and system |
| CN111258305A (en) * | 2020-03-06 | 2020-06-09 | 哈工大机器人（岳阳）军民融合研究院 | Satellite operation control center system, equipment management method, equipment and storage medium |
| CN111258305B (en) * | 2020-03-06 | 2023-06-16 | 哈工大机器人（岳阳）军民融合研究院 | Wei Xingyun control center system, equipment management method, equipment and storage medium |
| CN111483615A (en) * | 2020-04-17 | 2020-08-04 | 中国科学院微小卫星创新研究院 | Method for realizing pointing posture of quantum satellite to ground optical station |
| CN111483615B (en) * | 2020-04-17 | 2021-06-29 | 中国科学院微小卫星创新研究院 | Method for realizing pointing posture of quantum satellite to ground optical station |
| CN113867176A (en) * | 2021-10-12 | 2021-12-31 | 中国科学院空天信息创新研究院 | Satellite receiving station monitoring simulation system |
| CN114285455A (en) * | 2021-12-16 | 2022-04-05 | 广州爱浦路网络技术有限公司 | Satellite energy-saving control method, system, device and storage medium based on core network |
| CN114285455B (en) * | 2021-12-16 | 2022-10-21 | 广州爱浦路网络技术有限公司 | Satellite energy-saving control method, system, device and storage medium based on core network |
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