CN108650012A - It a kind of satellite antenna shake monitoring and influences to eliminate analysis method and system - Google Patents

It a kind of satellite antenna shake monitoring and influences to eliminate analysis method and system Download PDF

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CN108650012A
CN108650012A CN201810310758.3A CN201810310758A CN108650012A CN 108650012 A CN108650012 A CN 108650012A CN 201810310758 A CN201810310758 A CN 201810310758A CN 108650012 A CN108650012 A CN 108650012A
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satellite antenna
reaction time
satellite
model
shake
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CN108650012B (en
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钱晋希
马骏骁
魏振超
张阁
张雯
吴志强
张博
杜妍
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China Academy of Space Technology CAST
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    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04BTRANSMISSION
    • H04B17/00Monitoring; Testing
    • H04B17/10Monitoring; Testing of transmitters
    • H04B17/101Monitoring; Testing of transmitters for measurement of specific parameters of the transmitter or components thereof
    • H04B17/102Power radiated at antenna
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04BTRANSMISSION
    • H04B17/00Monitoring; Testing
    • H04B17/30Monitoring; Testing of propagation channels
    • H04B17/309Measuring or estimating channel quality parameters
    • H04B17/318Received signal strength
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04BTRANSMISSION
    • H04B17/00Monitoring; Testing
    • H04B17/30Monitoring; Testing of propagation channels
    • H04B17/391Modelling the propagation channel
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04BTRANSMISSION
    • H04B7/00Radio transmission systems, i.e. using radiation field
    • H04B7/14Relay systems
    • H04B7/15Active relay systems
    • H04B7/185Space-based or airborne stations; Stations for satellite systems
    • H04B7/1851Systems using a satellite or space-based relay

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Signal Processing (AREA)
  • Electromagnetism (AREA)
  • Quality & Reliability (AREA)
  • Astronomy & Astrophysics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Physics & Mathematics (AREA)
  • Radio Relay Systems (AREA)

Abstract

The invention discloses a kind of satellite antenna shake monitoring and influence to eliminate analysis method and system, wherein the method includes:The equivalent isotropically radiated power of satellite antenna is monitored, its variation tendency is obtained;Strength model is generated according to variation tendency, and causes to make judgement to whether Strength Changes state is shaken by satellite antenna;According to court verdict and reaction time model, the theoretical reaction time is calculated;According to the comparison result in theoretical reaction time and real reaction time, the dispelling tactics to match is selected to complete to eliminate the influence that satellite antenna is shaken.The present invention is by monitoring satellite antenna radiation intensity threshold situation of change; calculating reacting time limiting value; with the reaction time of earth station or user the most key technical indicator; in the case where ensureing satellite-signal and user or earth station's parameter is working properly or satellite-signal is with user or earth station's not chain rupture, provides and eliminate antenna and shake the handover scheme affected to signal strength and flow.

Description

It a kind of satellite antenna shake monitoring and influences to eliminate analysis method and system
Technical field
The invention belongs to technical field of satellite communication more particularly to a kind of satellite antenna shake monitoring and influence to eliminate analysis Method and system.
Background technology
In satellite communication, antenna is its important component, carries sending and receiving for signal, directly affects terminal Between signal transmit.Satellite communication is even more so, if carrying out the transformation and transmission of electromagnetic wave without antenna, satellite movement Communication can not be achieved.But in actual application, on the one hand, the netted large aperture antenna entrained by satellite is by more waves Shu Zucheng, in order to complete the tasks such as certain tracking or signal relaying, satellite antenna, which has, more and more large-scale to become Gesture.But due to the limitation of launching condition, antenna generally all shows expansion so that antenna is relatively light and with centainly soft Property, it can cause certain shake when emitting signal beam or work.On the other hand, satellite in orbit during, it is larger Flexible antennas can undergo the influence of space environment noise, and the large aperture antenna wave beam of satellite can be made to be likely to the finger for moment occur To jitter problem.In message transmitting procedure, satellite needs to control spaceborne when establishing communication link with user or earth station Antenna is accurately directed to receiver, and the shake of satellite antenna can lead to the generation of error, influences the pointing accuracy of satellite antenna, Small variation can all produce bigger effect user or ground station reception signal strength.When satellite is in work service state When, it is each that whether the stability of antenna can correctly transmit the link budget, network communication quality, signaling of satellite communication network etc. Aspect impacts, and antenna is even up to thousands of kilometers since its bore is larger, to the coverage area on ground, once it shakes Phenomenon may make the earth large area coverage area inaccurately even network interruption of the area of coverage, seriously reduce communication quality.
Invention content
The technology of the present invention solves the problems, such as:Overcome the deficiencies of the prior art and provide a kind of satellite antenna shake monitoring and shadow It rings and eliminates analysis method and system, by monitoring satellite antenna radiation intensity threshold situation of change, and calculate user or ground The reaction time limiting value stood is ensureing satellite-signal with the reaction time of earth station or user the most key technical indicator In the case that user or earth station's parameter be working properly or satellite-signal and user or earth station's not chain rupture, elimination day is provided Line shakes the handover scheme affected to signal strength and flow.
In order to solve the above-mentioned technical problem, the invention discloses a kind of satellite antenna shake monitorings and influence to eliminate analysis side Method, including:
The equivalent isotropically radiated power of satellite antenna is monitored, the variation tendency of equivalent isotropically radiated power is obtained;
Strength model is generated according to the variation tendency of equivalent isotropically radiated power, according to strength model to Strength Changes state Whether cause to make judgement by satellite antenna shake;
According to court verdict and reaction time model, the theoretical reaction time is calculated;
According to the comparison result in theoretical reaction time and real reaction time, the dispelling tactics to match is selected to complete to defending The influence of star antenna shake is eliminated.
In above-mentioned satellite antenna shakes monitoring and influences to eliminate analysis method, equivalent omnidirectional's spoke to satellite antenna It penetrates power to be monitored, obtains the variation tendency of equivalent isotropically radiated power, including:
By satellite signal receiver, the signal that satellite antenna is launched is received, and strong to the signal received Angle value is observed, and continues to track signal strength values with the variation tendency of time, obtains the change of equivalent isotropically radiated power Change trend.
It is described according to equivalent isotropically radiated power in above-mentioned satellite antenna shakes monitoring and influences to eliminate analysis method Variation tendency generates strength model, is sentenced to whether Strength Changes state is caused to make by satellite antenna shake according to strength model Certainly, including:
According to the variation tendency of equivalent isotropically radiated power, antenna coverage areas is divided into increasing intensity region and intensity subtracts Zonule;
Region is reduced to increasing intensity region and intensity respectively and establishes analysis model;
Cause to make judgement according to whether the analysis model Strength Changes state of foundation is shaken by satellite antenna.
It is described respectively to increasing intensity region and strong in above-mentioned satellite antenna shakes monitoring and influences to eliminate analysis method Degree reduces region and establishes analysis model, including:
Analysis model is established to increasing intensity region, obtains increasing intensity region shake monitoring model;Wherein, intensity increases The signal strength in region increases, and signal, which has, to be continued and not disconnected state;
Region is reduced to intensity and establishes analysis model, intensity is obtained and reduces region shake monitoring model;Wherein, intensity reduces The signal strength in region reduces, and chain rupture may occur for signal.
In above-mentioned satellite antenna shakes monitoring and influences to eliminate analysis method, monitoring model is shaken in increasing intensity region, For:
If signal strength is less than setting saltus step thresholding in setting transformation period, alternatively, being jumped when signal strength reaches setting The time for becoming thresholding is unsatisfactory for setting time threshold value, then adjudicates this change in signal strength and caused by satellite antenna shake;
If signal strength meets or exceeds setting saltus step thresholding in setting transformation period, and when duration satisfaction setting Between threshold value, then adjudicate this change in signal strength not by satellite antenna shake cause.
In above-mentioned satellite antenna shakes monitoring and influences to eliminate analysis method, intensity reduces region and shakes monitoring model, For:
If later strength variation tendency shows ascendant trend within certain time, the change of this signal strength is adjudicated Change and is caused by satellite antenna shake;
If signal strength continues to decline in setting transformation period, this change in signal strength is adjudicated not by satellite antenna Shake causes.
It is described according to court verdict and reaction time in above-mentioned satellite antenna shakes monitoring and influences to eliminate analysis method The theoretical reaction time is calculated in model, including:
When court verdict indication signal Strength Changes are caused by satellite antenna shake, according to reaction time model, calculate Obtain the theoretical reaction time.
It is described according to theoretical reaction time and reality in above-mentioned satellite antenna shakes monitoring and influences to eliminate analysis method The comparison result in reaction time selects the dispelling tactics to match to complete to eliminate the influence that satellite antenna is shaken, including:
When the real reaction time being less than the theoretical reaction time,
For increasing intensity region, power control method is selected to reduce the intensity for the antenna shaken, each parameter is made to work Normally, realize that effect of jitter is eliminated;
Region is reduced for intensity, nearby covering satellite or same satellite remaining element antenna is searched, enhances this antenna Gain makes beam coverage and main lobe width increase, and realizes that the antenna effect of jitter of not chain rupture is eliminated.
Correspondingly, the invention also discloses a kind of satellite antenna shake monitoring and influence to eliminate analysis system, including:
Monitoring modular is monitored for the equivalent isotropically radiated power to satellite antenna, obtains equivalent omnidirectional radiation work( The variation tendency of rate;
Judging module, for generating strength model according to the variation tendency of equivalent isotropically radiated power, according to strength model Cause to make judgement to whether Strength Changes state is shaken by satellite antenna;
Computing module, for according to court verdict and reaction time model, the theoretical reaction time to be calculated;
Execution module, for the comparison result according to theoretical reaction time and real reaction time, select to match disappears Except strategy is completed to eliminate the influence that satellite antenna is shaken.
The present invention has the following advantages:
(1) when the signal strength of ground satellite station or user terminal changes its main cause can be adjudicated in time whether It is shaken for satellite antenna;
(2) the reaction time threshold value of earth station or user terminal can be provided when satellite antenna is shaken;
(3) it can ensure user or earth station with larger probability and while satellite parametric reduction is working properly or not chain rupture The influence for completing antenna shake is eliminated.
Description of the drawings
Fig. 1 is a kind of satellite antenna shake monitoring and to influence to eliminate the step flow of analysis method in the embodiment of the present invention Figure;
Fig. 2 is a kind of increasing intensity region shake monitoring model schematic diagram in the embodiment of the present invention;
Fig. 3 is a kind of intensity reduction region shake monitoring model schematic diagram in the embodiment of the present invention;
Fig. 4 is a kind of reaction time model schematic in the embodiment of the present invention;
Fig. 5 is a kind of radiation patterns schematic diagram in the embodiment of the present invention.
Specific implementation mode
To make the object, technical solutions and advantages of the present invention clearer, below in conjunction with attached drawing to disclosed by the invention Embodiment is described in further detail.
Referring to Fig.1, it shows a kind of satellite antenna shake monitoring in the embodiment of the present invention and influences to eliminate analysis method Flow chart of steps.In the present embodiment, analysis method is eliminated in the satellite antenna shake monitoring and influence, including:
Step 101, the equivalent isotropically radiated power of satellite antenna is monitored, obtains the change of equivalent isotropically radiated power Change trend.
In the present embodiment, the prison to the equivalent isotropically radiated power of satellite antenna can be realized by earth station or user It surveys.For example, can be carried out to the signal that satellite antenna is launched by (earth station or user side) satellite signal receiver It receives, and the signal strength values received is observed, and continue to track signal strength values with the variation tendency of time, obtain To the variation tendency of equivalent isotropically radiated power.
Step 102, strength model is generated according to the variation tendency of equivalent isotropically radiated power, according to strength model to intensity Whether variable condition is caused to make judgement by satellite antenna shake.
In the present embodiment, antenna coverage areas can be divided by force according to the variation tendency of equivalent isotropically radiated power Degree increases region and intensity reduces region;Region is reduced to increasing intensity region and intensity respectively and establishes analysis model;According to building Whether vertical analysis model Strength Changes state is caused to make judgement by satellite antenna shake.
Preferably, analysis model is established to increasing intensity region, obtains increasing intensity region shake monitoring model.Wherein, The signal strength of increasing intensity region increases, and signal, which has, to be continued and not disconnected state, as shown in Figure 2.
Preferably, region is reduced to intensity and establishes analysis model, obtained intensity and reduce region shake monitoring model.Wherein, The signal strength that intensity reduces region reduces, and chain rupture may occur for signal, as shown in Figure 3.
Preferably, monitoring model is shaken in increasing intensity region, is used for:It is set if signal strength is less than in setting transformation period Determine saltus step thresholding, alternatively, when the time that signal strength reaches setting saltus step thresholding is unsatisfactory for setting time threshold value, then adjudicates this time Change in signal strength is caused by satellite antenna shake;And if signal strength meets or exceeds setting in setting transformation period Saltus step thresholding, and the duration meet setting time threshold value, then adjudicate this change in signal strength not by satellite antenna shake draw It rises.
Preferably, intensity reduces region shake monitoring model, is used for:If later strength variation tendency is in certain time range Ascendant trend is inside showed, then adjudicates this change in signal strength and is caused by satellite antenna shake;And if signal strength is being set Determine to continue to decline in transformation period, then adjudicates this change in signal strength and do not caused by satellite antenna shake.
Step 103, according to court verdict and reaction time model, the theoretical reaction time is calculated.
In the present embodiment, when court verdict indication signal Strength Changes are caused by satellite antenna shake, according to reaction The theoretical reaction time is calculated in time model.
Preferably, with reference to Fig. 4, a kind of reaction time model schematic in the embodiment of the present invention is shown.Reaction time mould The resolving principle of type is as follows:
According to estimation area, estimation antenna shakes angle [alpha], according to the distance R of satellite to the earth, with reference to Fig. 4, estimation variation Region relative path length L is:
L=α × R
Because terrestrial coverage area is farther out from satellite distance, it is assumed that terrestrial coverage area is circle, and actual area area is small In using L/2 as the area of a circle of radius, therefore, overlay area estimated value is bigger than actual value.Area reckoning, which is more than actual value, can allow letter Number of users in number range of receiving increases, can be smaller than actual value when calculating single user's amplitude transformation period.Then change area For:
By the user distribution rate that earth station is prior, the number of users in shake region can be obtained, the angular speed of antenna shake is ω When, then can obtain the Strength Changes time in range is:
To sum up, the reaction time threshold value (that is, theoretical reaction time) of earth station or subscriber terminal equipment is obtained.
Step 104, according to the comparison result in theoretical reaction time and real reaction time, the dispelling tactics to match are selected It completes to eliminate the influence that satellite antenna is shaken.
In the present embodiment, when the real reaction time being less than the theoretical reaction time, for increasing intensity region, work(is selected Rate control methods reduce the intensity for the antenna shaken, and keep each parameter working properly, realize that effect of jitter is eliminated;Intensity is subtracted Zonule searches nearby covering satellite or same satellite remaining element antenna, enhances this antenna gain, make beam coverage Increase with main lobe width, realizes that the antenna effect of jitter of not chain rupture is eliminated.Wherein, the real reaction time refers to:Earth station or use The time that family is adjusted.
Based on above-described embodiment, illustrated with reference to a specific example.
(1) by earth station or the satellite signal receiver of user, the signal that satellite antenna is launched is received, Meanwhile the signal strength values received are observed by satellite signal receiver, and continue to track its intensity with the time Variation tendency.For example, because satellite relative to satellite antenna quality big, volume weight, set satellite body in scheme and do not shake, satellite Antenna does the rotation that angular speed is gradually reduced about tangential, radial direction or normal orientation so that the bowing of antenna, the elevation angle changes. Radiation patterns schematic diagram is as shown in Figure 5.If orbit plane is coordinate plane, Z axis is directed toward the earth's core by centroid of satellite, and X-axis is in track It is vertical with Z axis and be directed toward satellite velocities direction in plane, Y-axis it is orthogonal with X, the Z axis right hand and with orbit plane normal parallel, one Under fixed condition, orbital coordinate system is consistent with satellite body coordinate system, then region B in Fig. 5 can be obtained and belong to increasing intensity region, and Region A belongs to intensity and reduces region.
(2) according to variation tendency, antenna coverage areas is divided into increasing intensity region and intensity reduces region, and is right respectively Increasing intensity region and intensity reduce region and establish analysis model, cause to do to whether Strength Changes state is shaken by satellite antenna Go out judgement.For example, shaking monitoring model according to increasing intensity region, Fig. 2 illustrates the increment as satellite antenna shake time domain B Variation, wherein TupIt measures the intensity learnt in advance for system and increases duration threshold, QupMeasured in advance for system learn it is strong Spend upper limit saltus step thresholding.If intensity value is no more than the saltus step thresholding, or is no more than the time more than the time of the saltus step thresholding Threshold value illustrates to change caused by the Strength Changes are shaken by satellite antenna.Meanwhile shake monitoring mould in region is reduced according to intensity Type, Fig. 3 illustrate the decrement variation as satellite antenna shake time domain A, wherein TdownMeasure the intensity learnt in advance for system Reduce duration threshold, QdownMeasure the low intensity limit saltus step thresholding learnt in advance for system.It should if intensity value is not less than Saltus step thresholding, or it is no more than time threshold less than the time of the saltus step thresholding, illustrate that the Strength Changes are shaken by satellite antenna Caused variation.
(3) when change in signal strength judgement is is caused by antenna shake, then according to reaction time model, earth station is calculated Or the reaction time threshold value of user.For example, according to reaction time model, when the antenna shake angle of geostationary orbit satellite is At 0.6 degree, region of variation relative path length is:
L0.6=α × R=0.6 × 36000000=2.16 × 107
Its variation area, which can be obtained, is:
Finally, when the angular velocity omega of antenna shake is 6 × 10-10When degrees second, the Strength Changes time can be obtained in range For:
To sum up, the reaction time threshold value t for obtaining earth station or subscriber terminal equipment is 2.73 × 10-7
(4) reaction time of actual ground station or user are compared with the threshold value that reaction time model calculates, The real reaction time is earth station or the time that user is adjusted, and is less than threshold value 2.73 × 10 when the real reaction time-7When, it is right In increasing intensity region, the methods of power control may be used, reduce the intensity for the antenna shaken, make satellite, earth station Or the parameters of user are working properly, realize that effect of jitter is eliminated;For intensity reduce region, can take for example search it is attached Nearly covering satellite or same satellite remaining element antenna, enhance its antenna gain, and beam coverage and main lobe width is made to increase The methods of add, realize that the antenna effect of jitter of not chain rupture is eliminated.For example, certain region is increasing intensity region, then it can apply and open Ring power control, earth station's firing order control the transmission power of satellite antenna, make its reduction, then realize that running parameter is normal; When certain region be formidable opponent reduce region when, then can be arranged by the software of earth station or user, adjust satellite antenna gain or Person's beam coverage makes the earth station or user be switching to the state covered by uncovered, then can be achieved satellite with User or earth station's not chain rupture.Later, earth station or user continue to keep the monitoring to signal strength state.
It is as follows that analysis method specific implementation flow totality case is eliminated in classical satellite antenna shake monitoring and influence:
Step 1, certain earth station or certain user are monitored the intensity of certain geostationary orbit satellite antenna, tracker State of strength variation tendency show that the earth station or user's intensity belong to increasing intensity region;
Step 2 shakes monitoring model according to increasing intensity region, is jumped when the increment variation upper limit value in the region is no more than Become thresholding Qup, or more than the saltus step thresholding time be no more than time threshold Tup, illustrate that the Strength Changes are trembled by satellite antenna Variation caused by dynamic can adjudicate the current satellite antenna and be shaken;
Step 3 calculates the reaction time that the region increases region according to reaction time model, and antenna shake angle is 0.6 degree, the angular velocity omega of antenna shake is 6 × 10-10When degrees second, it can be deduced that its Strength Changes time is 2.73 × 10-7
Step 4, earth station reduce the intensity for the antenna shaken by software using the methods of power control, While with satellite chain rupture does not occur for earth station or user, keep various functions parameter normal.Later, earth station or user continue Keep the monitoring to signal strength state.
Conclusion:By step 1, the present invention can monitor the signal strength of satellite antenna in real time, and adjudicate the satellite antenna Signal strength changed, i.e. intensity enhancing, it is critical that, by step 2, the present invention can adjudicate the satellite antenna Antenna dither state has occurred, and according to step 3, earth station when satellite antenna is shaken can be obtained in time or user is anti- Between seasonable, the method that the last present invention can provide power control in time eliminates satellite antenna shake to maximum possible The influence brought.
In embodiments of the present invention, it also discloses a kind of satellite antenna shake monitoring and influences to eliminate analysis system, including: Monitoring modular is monitored for the equivalent isotropically radiated power to satellite antenna, obtains the variation of equivalent isotropically radiated power Trend;Judging module, for generating strength model according to the variation tendency of equivalent isotropically radiated power, according to strength model to strong Whether degree variable condition is caused to make judgement by satellite antenna shake;Computing module, for according to court verdict and reaction time The theoretical reaction time is calculated in model;Execution module, for the comparison knot according to theoretical reaction time and real reaction time Fruit selects the dispelling tactics to match to complete to eliminate the influence that satellite antenna is shaken.
For system embodiments, since it is corresponding with embodiment of the method, so description is fairly simple, correlation Place referring to embodiment of the method part explanation.
Each embodiment in this explanation is described in a progressive manner, the highlights of each of the examples are with its The difference of his embodiment, the same or similar parts between the embodiments can be referred to each other.
The above, best specific implementation mode only of the invention, but scope of protection of the present invention is not limited thereto, Any one skilled in the art in the technical scope disclosed by the present invention, the change or replacement that can be readily occurred in, It should be covered by the protection scope of the present invention.
The content that description in the present invention is not described in detail belongs to the known technology of professional and technical personnel in the field.

Claims (9)

1. analysis method is eliminated in a kind of satellite antenna shake monitoring and influence, which is characterized in that including:
The equivalent isotropically radiated power of satellite antenna is monitored, the variation tendency of equivalent isotropically radiated power is obtained;
According to the variation tendency of equivalent isotropically radiated power generate strength model, according to strength model to Strength Changes state whether Cause to make judgement by satellite antenna shake;
According to court verdict and reaction time model, the theoretical reaction time is calculated;
According to the comparison result in theoretical reaction time and real reaction time, the dispelling tactics to match is selected to complete to satellite day The influence of line shake is eliminated.
2. analysis method is eliminated in satellite antenna shake monitoring according to claim 1 and influence, which is characterized in that described right The equivalent isotropically radiated power of satellite antenna is monitored, and obtains the variation tendency of equivalent isotropically radiated power, including:
By satellite signal receiver, the signal that satellite antenna is launched is received, and the signal strength values to receiving It is observed, and continues the variation tendency for tracking signal strength values with the time, the variation for obtaining equivalent isotropically radiated power becomes Gesture.
3. analysis method is eliminated in satellite antenna shake monitoring according to claim 1 and influence, which is characterized in that described Strength model is generated according to the variation tendency of equivalent isotropically radiated power, according to strength model to Strength Changes state whether by satellite Antenna shake causes to make judgement, including:
According to the variation tendency of equivalent isotropically radiated power, antenna coverage areas is divided into increasing intensity region and intensity reduces area Domain;
Region is reduced to increasing intensity region and intensity respectively and establishes analysis model;
Cause to make judgement according to whether the analysis model Strength Changes state of foundation is shaken by satellite antenna.
4. analysis method is eliminated in satellite antenna shake monitoring according to claim 3 and influence, which is characterized in that described point It is other that analysis model is established to increasing intensity region and intensity reduction region, including:
Analysis model is established to increasing intensity region, obtains increasing intensity region shake monitoring model;Wherein, increasing intensity region Signal strength increase, signal, which has, to be continued and not disconnected state;
Region is reduced to intensity and establishes analysis model, intensity is obtained and reduces region shake monitoring model;Wherein, intensity reduces region Signal strength reduce, chain rupture may occur for signal.
5. analysis method is eliminated in satellite antenna shake monitoring according to claim 4 and influence, which is characterized in that intensity increases Monitoring model is shaken in big region, is used for:
If signal strength is less than setting saltus step thresholding in setting transformation period, alternatively, when signal strength reaches setting saltus step door The time of limit is unsatisfactory for setting time threshold value, then adjudicates this change in signal strength and caused by satellite antenna shake;
If signal strength meets or exceeds setting saltus step thresholding in setting transformation period, and the duration meets setting time threshold Value is then adjudicated this change in signal strength and is not caused by satellite antenna shake.
6. analysis method is eliminated in satellite antenna shake monitoring according to claim 4 and influence, which is characterized in that intensity subtracts Monitoring model is shaken in zonule, is used for:
If later strength variation tendency shows ascendant trend within certain time, adjudicate this change in signal strength by Satellite antenna shake causes;
If signal strength continues to decline in setting transformation period, adjudicates this change in signal strength and do not shaken by satellite antenna Cause.
7. analysis method is eliminated in satellite antenna shake monitoring according to claim 1 and influence, which is characterized in that described According to court verdict and reaction time model, the theoretical reaction time is calculated, including:
When court verdict indication signal Strength Changes are caused by satellite antenna shake, according to reaction time model, it is calculated The theoretical reaction time.
8. analysis method is eliminated in satellite antenna shake monitoring according to claim 1 and influence, which is characterized in that described According to the comparison result in theoretical reaction time and real reaction time, the dispelling tactics to match is selected to complete to shake satellite antenna Influence eliminate, including:
When the real reaction time being less than the theoretical reaction time,
For increasing intensity region, selects power control method to reduce the intensity for the antenna shaken, keeps each parameter working properly, Realize that effect of jitter is eliminated;
Region is reduced for intensity, nearby covering satellite or same satellite remaining element antenna is searched, enhances this antenna gain, So that beam coverage and main lobe width is increased, realizes that the antenna effect of jitter of not chain rupture is eliminated.
9. analysis system is eliminated in a kind of satellite antenna shake monitoring and influence, which is characterized in that including:
Monitoring modular is monitored for the equivalent isotropically radiated power to satellite antenna, obtains equivalent isotropically radiated power Variation tendency;
Judging module, for generating strength model according to the variation tendency of equivalent isotropically radiated power, according to strength model to strong Whether degree variable condition is caused to make judgement by satellite antenna shake;
Computing module, for according to court verdict and reaction time model, the theoretical reaction time to be calculated;
Execution module selects the elimination plan to match for the comparison result according to theoretical reaction time and real reaction time It slightly completes to eliminate the influence that satellite antenna is shaken.
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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112928426A (en) * 2021-02-25 2021-06-08 上海卫星工程研究所 Large-scale deployable satellite antenna profile precision in-orbit active control device and method
CN115882980A (en) * 2023-03-03 2023-03-31 江苏晨创科技有限公司 Prediction system for influence on satellite communication signals based on antenna pointing
CN117074799A (en) * 2023-10-18 2023-11-17 深圳市博格斯通信技术有限公司 Circularly polarized antenna and real-time detection method thereof

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101188456A (en) * 2007-12-19 2008-05-28 哈尔滨工业大学 A performance tracking and testing method for space optical communication system
EP2099141A2 (en) * 2008-03-05 2009-09-09 Raysat, Inc. Reduced cost mobile satellite antenna system using a plurality of satellite transponders
WO2010083453A1 (en) * 2009-01-15 2010-07-22 Walton Enterprises. Inc. Apparatus and method for clearing water from dish antenna covers
CN101943913A (en) * 2010-08-04 2011-01-12 北京爱科迪信息通讯技术有限公司 Intelligent control system for portable satellite antenna and method
US7880685B2 (en) * 2003-10-02 2011-02-01 Toyon Research Corporation Switched-resonance antenna phase shifter and phased array incorporating same
CN105742781A (en) * 2016-01-28 2016-07-06 华为技术有限公司 Antenna adjustment system and base station
CN106950565A (en) * 2017-01-24 2017-07-14 王洋 Space-borne SAR Imaging jitter compensation method, imaging method

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7880685B2 (en) * 2003-10-02 2011-02-01 Toyon Research Corporation Switched-resonance antenna phase shifter and phased array incorporating same
CN101188456A (en) * 2007-12-19 2008-05-28 哈尔滨工业大学 A performance tracking and testing method for space optical communication system
EP2099141A2 (en) * 2008-03-05 2009-09-09 Raysat, Inc. Reduced cost mobile satellite antenna system using a plurality of satellite transponders
WO2010083453A1 (en) * 2009-01-15 2010-07-22 Walton Enterprises. Inc. Apparatus and method for clearing water from dish antenna covers
CN101943913A (en) * 2010-08-04 2011-01-12 北京爱科迪信息通讯技术有限公司 Intelligent control system for portable satellite antenna and method
CN105742781A (en) * 2016-01-28 2016-07-06 华为技术有限公司 Antenna adjustment system and base station
CN106950565A (en) * 2017-01-24 2017-07-14 王洋 Space-borne SAR Imaging jitter compensation method, imaging method

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
CHU-JUNG YEH: "《On the Performance of Receive ZF MIMO Broadcast Systems with Channel Estimation Errors》", 《2011 IEEE INTERNATIONAL CONFERENCE ON COMMUNICATIONS (ICC)》 *
潘时龙: "《微波光子雷达及关键技术》", 《科技导报》 *

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112928426A (en) * 2021-02-25 2021-06-08 上海卫星工程研究所 Large-scale deployable satellite antenna profile precision in-orbit active control device and method
CN112928426B (en) * 2021-02-25 2023-01-24 上海卫星工程研究所 Large-scale deployable satellite antenna profile precision in-orbit active control device and method
CN115882980A (en) * 2023-03-03 2023-03-31 江苏晨创科技有限公司 Prediction system for influence on satellite communication signals based on antenna pointing
CN115882980B (en) * 2023-03-03 2023-07-18 江苏晨创科技有限公司 Prediction system for influence of antenna pointing on satellite communication signals
CN117074799A (en) * 2023-10-18 2023-11-17 深圳市博格斯通信技术有限公司 Circularly polarized antenna and real-time detection method thereof
CN117074799B (en) * 2023-10-18 2024-01-16 深圳市博格斯通信技术有限公司 Circularly polarized antenna and real-time detection method thereof

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