CN112583470B - Optimal matching-based satellite measurement and control planning and scheduling method - Google Patents

Optimal matching-based satellite measurement and control planning and scheduling method Download PDF

Info

Publication number
CN112583470B
CN112583470B CN202011478196.7A CN202011478196A CN112583470B CN 112583470 B CN112583470 B CN 112583470B CN 202011478196 A CN202011478196 A CN 202011478196A CN 112583470 B CN112583470 B CN 112583470B
Authority
CN
China
Prior art keywords
genes
operator
gene
fitness
scheduling method
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN202011478196.7A
Other languages
Chinese (zh)
Other versions
CN112583470A (en
Inventor
吕泽石
秦亮
张延平
党彰
王书宇
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Xi'an Huanyu Satellite Tt & C And Data Application Co ltd
Original Assignee
Xi'an Huanyu Satellite Tt & C And Data Application Co ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Xi'an Huanyu Satellite Tt & C And Data Application Co ltd filed Critical Xi'an Huanyu Satellite Tt & C And Data Application Co ltd
Priority to CN202011478196.7A priority Critical patent/CN112583470B/en
Publication of CN112583470A publication Critical patent/CN112583470A/en
Application granted granted Critical
Publication of CN112583470B publication Critical patent/CN112583470B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • 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
    • H04B7/18502Airborne stations
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02DCLIMATE CHANGE MITIGATION TECHNOLOGIES IN INFORMATION AND COMMUNICATION TECHNOLOGIES [ICT], I.E. INFORMATION AND COMMUNICATION TECHNOLOGIES AIMING AT THE REDUCTION OF THEIR OWN ENERGY USE
    • Y02D30/00Reducing energy consumption in communication networks
    • Y02D30/70Reducing energy consumption in communication networks in wireless communication networks

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Physics & Mathematics (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Signal Processing (AREA)
  • General Factory Administration (AREA)
  • Management, Administration, Business Operations System, And Electronic Commerce (AREA)

Abstract

The invention provides a satellite measurement and control planning and scheduling method based on optimal matching, which is characterized in that applied limiting conditions are firstly divided into strong limiting items and weak limiting items before a genetic algorithm is executed, available arc segments are screened out according to the strong limiting items, a large number of diversity genes are generated through a shuffling algorithm and a diversity generation algorithm, initial genes and the diversity genes are combined into an initialized genome, the original genome meets the applied strong limiting items, the genes are subjected to fitness grading according to the applied weak limiting items, the genetic algorithm operations of selection, crossing and variation are carried out, and finally the result with the highest grading is output. Therefore, the method can more conveniently and quickly deal with various complex constraint conditions in the engineering.

Description

Optimal matching-based satellite measurement and control planning and scheduling method
Technical Field
The invention relates to the field of satellite measurement and control, in particular to a satellite measurement and control planning and scheduling method based on optimal matching.
Background
With the development of science and technology, people continuously explore and develop the aerospace field, various aircrafts and satellites are manufactured and widely applied to various fields, the problem of satellite measurement and control scheduling is an NP-hard problem, an optimal solution cannot be generated, a currently adopted solution usually mainly adopts a Genetic Algorithm (GA), but the algorithm can only simply score according to time and equipment service duration in the execution process, an output result is only the maximum score, the judgment of certain necessary limits cannot be realized, and the requirements of complex conditions such as lifting circle requirements, equipment limits, manual assigned plans, application priorities, satellite priorities and the like in engineering cannot be met.
Disclosure of Invention
In order to solve the technical problems, the invention provides a satellite measurement and control planning and scheduling method based on optimal matching, which comprises the steps of firstly, dividing applied limiting conditions into strong limiting items and weak limiting items according to experience, screening available arc segments according to the strong limiting items before executing a genetic algorithm, generating a small amount of initial genes from the screened available arc segments through a shuffling algorithm, generating a large amount of diversity genes through a diversity generation algorithm, and combining the initial genes and the diversity genes into an initialized genome; and then, fitness scoring is carried out on the genes according to the weak restriction items, and the genetic algorithm operation of selection, intersection and variation is carried out, and finally the result with the highest score is output.
The invention provides a satellite measurement and control planning and scheduling method based on optimal matching, which comprises the following steps:
s1, determining the applied limiting conditions, and dividing the limiting conditions into strong limiting items and weak limiting items;
s2, screening available arc segments according to the applied strong limitation items, and coding each available arc segment;
s3, generating initial genes by using the screened available radians through a shuffling algorithm, generating diversity genes by using a diversity generation algorithm, and combining the initial genes and the diversity genes into an initialized genome;
s4, scoring fitness according to the applied weak restriction terms, judging whether convergence conditions are met or not, outputting a gene generation result and decoding if the convergence conditions are met, and ending the program; if the convergence condition is not satisfied, performing step S5;
s5, carrying out genetic operations of selection, crossover and mutation:
s5.1, selecting a gene with high fitness to enter the next round;
s5.2, crossing the father genes selected in the selection stage to generate new genes, and combining the new genes with the father genes to form a new gene pool;
s5.3, performing mutation operation on the basis of the new gene pool to obtain a new generation of population;
and S6, repeating the steps S4 and S5 on the new generation of population until a convergence condition is met, outputting a gene generation result, decoding, and ending the program.
Further, the strong limitation items comprise time limitation, equipment limitation, lifting ring limitation and unavailable resource limitation.
Further, the weak restriction items include lifting rail requirements, service duration and elevation coefficients.
Further, in step S4, the fitness score rule is: and the gene fitness is sigma (lifting orbit demand coefficient + service duration coefficient + elevation coefficient) (10 + application priority + satellite priority), corresponding coefficients are distributed to each weak restriction item, the sum is 1, weighting operation is carried out on the weak restriction items and the application priority and the satellite priority, and the priority degree of the application priority is higher than the satellite priority.
Further, in step S2, the encoding is performed by real number encoding, and each available arc segment of each application corresponds to one encoding.
Further, in step S5.1, the selection operator selects by combining the sorting selection operator with the elite retention operator, the sorting selection operator assigns different selection probabilities to different genes according to the fitness, and the elite retention operator directly selects a gene with the highest fitness for the next round.
Further, in step S5.2, the crossover operator employs an order crossover operator and a sysread sequence crossover operator.
Further, in step S5.3, the mutation operator employs a multi-segment inversion mutation operator and a multi-point crossover mutation operator, the multi-segment inversion mutation operator is employed in the former stage to perform mutation with a large change, and the multi-point crossover mutation operator is employed in the latter stage.
Further, the decoding mode is used for inquiring genes from beginning to end in a FIFO (first in first out) mode, and each gene is decoded respectively.
Further, the convergence condition is whether the score meets the requirement or whether the scheduling times reach an upper limit.
The invention has the following beneficial effects:
according to the method, the applied limiting conditions are divided into the strong limiting items and the weak limiting items before the genetic algorithm is executed, the strong limiting items are screened firstly to generate the initialized genome, and then the fitness scoring is carried out on the gene only according to the applied weak limiting items.
Additional aspects and advantages of the invention will be set forth in part in the description which follows and, in part, will be obvious from the description, or may be learned by practice of the invention.
Drawings
The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this application, illustrate embodiment(s) of the invention and together with the description serve to explain the principles of the invention:
FIG. 1 is a schematic flow chart of a satellite measurement and control planning and scheduling method based on optimal matching;
FIG. 2 is a schematic diagram of a Syswerda sequence crossover operator;
FIG. 3 is a diagram illustrating a multi-segment inversion mutation operator;
FIG. 4 is a diagram illustrating a multi-point crossover mutation operator.
Detailed Description
The invention will be described in further detail below with reference to the figures and specific embodiments.
As shown in fig. 1: a satellite measurement and control planning and scheduling method based on optimal matching comprises the following steps:
s1, firstly, determining applied limiting conditions, and dividing the limiting conditions into strong limiting items and weak limiting items according to actual engineering requirements;
s2, screening available arc segments according to the applied strong limitation items, coding each available arc segment, and enabling the screened available arc segments to meet the applied strong limitation items;
s3, generating a small amount of initial genes through a shuffling algorithm according to the screened available radians, generating a large amount of diversity genes through a diversity generation algorithm, and combining the initial genes and the diversity genes into an initialized genome; wherein, the shuffling algorithm flow is as follows:
step 1: taking the available arc segment as PJ to obtain the size of the PJ;
step 2: randomly selecting 1 number i from 1-size, and exchanging size positions and i positions in PJ;
Step3:size=size-1;
step 4: if size >1, go back to Step2, otherwise end.
The diversity generation algorithm flow is as follows:
step 1: setting i to be 1, and setting the initial number of individuals to be generated to be PJ;
step 2: obtaining seed solution SD ═ SD1, SD2, …, sdn,
step 3: let QY be n/RN, RN be a random number between the intervals [5, n/5], and let j be 1;
step 4: given the array F (1, 2, …, n), a subsequence of F is defined as F (h: s) ═ s, s + h, s +2h, …, s + λ h, where h is a positive integer, s is a positive integer between 1 and h, and λ is a largest non-negative integer satisfying s + λ h < n; defining the permutation F (h) ═ (F (h: h), F (h: h-1), …, F (h:1)) for h < n, yielding sequence F (j);
step 5: sequentially placing the elements in the seed solution SD in the knife sequence NS according to the positions established by the elements in the sequence F (j), and generating NS (NS1, NS2, … and nsn), wherein NS is a diversity solution;
step 6: if j < ═ QY and i < ═ PJ, return to Step 4;
step 7: if i < ═ PJ, returning to Step2, otherwise, ending the process.
S4, scoring fitness according to the applied weak restriction terms, judging whether convergence conditions are met or not, outputting a gene generation result and decoding if the convergence conditions are met, and ending the program; if the convergence condition is not satisfied, the process proceeds to step S5. The screened genes meet the strong restriction terms of the application, and fitness scoring is carried out according to the weak restriction terms of the application, so that the genes with high fitness scoring meet both the strong restriction terms and the weak restriction terms; through the fitness scoring only according to the applied weak restriction items, the fitness scoring judgment of the strong restriction items is not needed, the time of system operation is greatly shortened, more restriction conditions can be judged and scored, and the judgment of complex restriction conditions is realized, so that various complex restriction conditions in engineering can be more conveniently and quickly responded.
S5, carrying out genetic operations of selection, crossover and mutation:
s5.1, selecting a gene with high fitness to enter the next round;
s5.2, crossing the father genes selected in the selection stage to generate new genes, and combining the new genes with the father genes to form a new gene pool;
s5.3, performing mutation operation with lower probability on the basis of the new gene pool to obtain a new generation of population;
and S6, repeating the steps S4 and S5 on the new generation of population until a convergence condition is met, outputting a gene generation result, decoding, and ending the program.
Specifically, the strong restriction items include time restriction, equipment restriction, lifting ring restriction, and unavailable resource restriction.
Specifically, the weak restriction items include a lifting rail requirement, a service duration, an elevation coefficient and the like.
Specifically, in step S4, the fitness score rule is: and (3) gene fitness sigma (ascending and descending orbit demand coefficient + service duration coefficient + elevation coefficient) (10 application priority + satellite priority), namely distributing corresponding coefficients for each weak restriction item, wherein the sum is 1, weighting calculation is carried out on the application priority and the satellite priority, the priority of the application priority is higher than the satellite priority, the sum of the fitness of each gene is obtained according to the formula, and sequencing calculation is carried out.
Specifically, in step S2, the codes are encoded by real numbers, each available arc segment of each application corresponds to one code, and the total length of the genes is the sum of the total number of available arc segments of all applications.
Specifically, in step S5.1, the selection operator is selected by combining the sorting selection operator with the elite retention operator, the sorting selection operator assigns different selection probabilities to different genes according to the fitness, and the elite retention operator directly selects a gene with the highest fitness for the next round; wherein the sorting selection operator comprises the following steps:
step 1: sorting according to the gene fitness;
step 2: assigning the probability of selection to each gene by ranking, the first being (2n)/n (n +1), the second being (2n-2)/n (n +1), and so on, the last being 2/n (n + 1);
step 3: generating a random number in the range of 1 to n (n + 1);
step 4: determining a corresponding gene according to the random number, and selecting the gene in the next round;
step 5: if the total number of choices meets the requirement, the method is ended, otherwise, the method returns to Step 3.
Specifically, in step S5.2, the crossover operator uses an order crossover operator and a sysread sequence crossover operator, and a specific operator is selected according to a fixed probability when a specific crossover operation is performed. The order crossover operator operates as follows: the method comprises the steps of firstly randomly determining two crossing positions, exchanging fragments between the crossing points, deleting genes to be exchanged from another parent individual from an original parent individual from a second crossing position, then filling in the rest genes from the second crossing position, and sequentially crossing to generate a child individual by directly exchanging the fragments between certain two gene positions of the two parent individuals, wherein the child individual inherits the absolute position relationship between certain fragments of genes of the parent individuals.
As shown in fig. 2, the sysread sequence crossover operator operates as follows: selecting a certain father of the two father individuals as a reference object (setting the father as 2), randomly selecting K positions in the father, finding K elements selected by the father 2 in the father 1, rearranging the K elements in the father 1 according to the sequence of the individuals 2, and finally directly and sequentially filling other elements in the individuals 1 into vacant positions of the individuals 1 according to the original sequence to generate a new individual, wherein the son individual generated by the operator mainly inherits the relative sequence relationship among the genes of the father.
Specifically, in step S5.3, the mutation operation is performed with a lower probability based on the new gene pool, in this embodiment, a mode of combining multiple segments of inversion mutation operators and multipoint exchange mutation operators is adopted, the multiple segments of inversion mutation operators are adopted at the early stage to perform mutation with a larger change, and the multipoint exchange mutation operators are adopted at the later stage.
As shown in fig. 3, the multi-segment inversion mutation operator randomly selects K positions (K > ═ 2) as the mutation points in the parent, and inverts the elements between every two mutation points (including the elements corresponding to the two mutation points) in sequence from front to back.
As shown in FIG. 4, the multiple point crossover mutation operator randomly selects a mutation gene site i in the parent, the corresponding gene is g i Determining the allele, randomly selecting an element g in the allele i Replacing the original gene g at position i of the parent chromosome i Ensure g i ≠g j
Specifically, the decoding method comprises the steps of inquiring genes from beginning to end according to FIFO (first-in first-out), decoding each gene respectively, selecting the gene if the application corresponding to the gene is not completely met, removing conflict items in the subsequent genes, and executing in a circulating mode until the gene is empty.
Specifically, the convergence condition is whether the score meets the requirement or whether the scheduling frequency reaches an upper limit.
In other embodiments, the strong restriction term and the weak restriction term may be determined and divided differently according to actual engineering requirements.
The technical solutions provided by the embodiments of the present invention are described in detail above, and the principles and embodiments of the present invention are explained herein by using specific examples, and the descriptions of the embodiments are only used to help understanding the principles of the embodiments of the present invention; meanwhile, for a person skilled in the art, according to the embodiments of the present invention, there may be variations in the specific implementation manners and application ranges, and in summary, the present disclosure should not be construed as limiting the invention.

Claims (7)

1. A satellite measurement and control planning and scheduling method based on optimal matching is characterized in that: the method comprises the following steps:
s1, determining the applied limiting conditions, and dividing the limiting conditions into strong limiting items and weak limiting items; the strong limitation items comprise time limitation, equipment limitation, lifting ring limitation and unavailable resource limitation; the weak limitation items comprise lifting rail requirements, service duration and elevation coefficients;
s2, screening available arc segments according to the applied strong limitation items, and coding each available arc segment;
s3, generating initial genes by using the screened available arc segments through a shuffling algorithm, generating diversity genes by using a diversity generation algorithm, and combining the initial genes and the diversity genes into an initialized genome;
s4, scoring fitness according to the applied weak restriction terms, judging whether convergence conditions are met or not, outputting a gene generation result and decoding if the convergence conditions are met, and ending the program; if the convergence condition is not satisfied, performing step S5;
s5, carrying out genetic operations of selection, crossover and mutation:
s5.1, selecting a gene with high fitness to enter the next round;
s5.2, crossing the father genes selected in the selection stage to generate new genes, and combining the new genes with the father genes to form a new gene pool;
s5.3, performing mutation operation on the basis of the new gene pool to obtain a new generation of population;
s6, repeating the steps S4 and S5 on the new generation of population until a convergence condition is met, outputting a gene generation result, decoding, and ending the program;
in step S4, the fitness score rule is: and the gene fitness is sigma (lifting orbit demand coefficient + service duration coefficient + elevation coefficient) (10 + application priority + satellite priority), namely corresponding coefficients are distributed to each weak restriction item, the sum is 1, weighting operation is carried out on the application priority and the satellite priority, and the priority degree of the application priority is higher than that of the satellite.
2. The optimal matching based satellite measurement and control planning and scheduling method according to claim 1, wherein: in step S2, the encoding is performed by real number encoding, and each available arc segment of each application corresponds to one encoding.
3. The optimal matching based satellite measurement and control planning and scheduling method according to claim 1, wherein: in step S5.1, the selection operator is selected by combining the sorting selection operator with the elite reservation operator, the sorting selection operator assigns different selection probabilities to different genes according to the fitness, and the elite reservation operator directly selects a gene with the highest fitness to enter the next round.
4. The optimal matching based satellite measurement and control planning and scheduling method according to claim 1, wherein: in step S5.2, the crossover operator employs an order crossover operator and a sysread sequence crossover operator.
5. The optimal matching based satellite measurement and control planning and scheduling method according to claim 1, wherein: in step S5.3, the mutation operator is a combination of a multi-segment inversion mutation operator and a multi-point crossover mutation operator, the multi-segment inversion mutation operator is used in the early stage to perform a mutation with a large change, and the multi-point crossover mutation operator is used in the later stage.
6. The optimal matching based satellite measurement and control planning and scheduling method according to claim 1, wherein: the decoding mode is used for inquiring genes from beginning to end according to an FIFO mode, and each gene is decoded respectively.
7. The optimal matching based satellite measurement and control planning and scheduling method according to claim 1, wherein: the convergence condition is whether the score meets the requirement or whether the scheduling times reach the upper limit.
CN202011478196.7A 2020-12-15 2020-12-15 Optimal matching-based satellite measurement and control planning and scheduling method Active CN112583470B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202011478196.7A CN112583470B (en) 2020-12-15 2020-12-15 Optimal matching-based satellite measurement and control planning and scheduling method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202011478196.7A CN112583470B (en) 2020-12-15 2020-12-15 Optimal matching-based satellite measurement and control planning and scheduling method

Publications (2)

Publication Number Publication Date
CN112583470A CN112583470A (en) 2021-03-30
CN112583470B true CN112583470B (en) 2022-08-12

Family

ID=75135139

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202011478196.7A Active CN112583470B (en) 2020-12-15 2020-12-15 Optimal matching-based satellite measurement and control planning and scheduling method

Country Status (1)

Country Link
CN (1) CN112583470B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113778646B (en) * 2021-08-22 2024-04-05 物产中大公用环境投资有限公司 Task level scheduling method and device based on execution time prediction

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IT201700056428A1 (en) * 2017-05-24 2018-11-24 Telespazio Spa INNOVATIVE SATELLITE SCHEDULING METHOD BASED ON GENETIC ALGORITHMS AND SIMULATED ANNEALING AND RELATIVE MISSION PLANNER
CN107733515B (en) * 2017-08-31 2019-12-31 北京空间飞行器总体设计部 Satellite communication link analysis method under in-orbit complex environment
CN108880663B (en) * 2018-07-20 2020-09-22 大连大学 Space-ground integrated network resource allocation method based on improved genetic algorithm
CN109933842B (en) * 2019-01-23 2021-08-06 北京航空航天大学 Moving target single-star task planning method based on constraint satisfaction genetic algorithm
CN111913787B (en) * 2020-06-19 2022-10-18 合肥工业大学 Imaging satellite scheduling method and system based on genetic algorithm

Also Published As

Publication number Publication date
CN112583470A (en) 2021-03-30

Similar Documents

Publication Publication Date Title
CN108880663B (en) Space-ground integrated network resource allocation method based on improved genetic algorithm
Magalhaes-Mendes A comparative study of crossover operators for genetic algorithms to solve the job shop scheduling problem
CN109299142B (en) Convolutional neural network structure searching method and system based on evolutionary algorithm
Li et al. Search algorithms for regression test case prioritization
CN102122251B (en) A kind of many spacecraft parallel tests method for scheduling task based on genetic algorithm
CN109271320B (en) Higher-level multi-target test case priority ordering method
US8924341B2 (en) Method and system for optimizing mixed integer programming solutions
CN112583470B (en) Optimal matching-based satellite measurement and control planning and scheduling method
CN108460463A (en) High-end equipment flow line production dispatching method based on improved adaptive GA-IAGA
US20080154808A1 (en) Use and construction of time series interactions in a predictive model
CN111913785B (en) Multi-satellite task scheduling method and system
CN108776461A (en) A kind of flexible job shop scheduling method and system
Poladian et al. Multi-objective evolutionary algorithms and phylogenetic inference with multiple data sets
JP4335010B2 (en) Fuzzy preferences in multi-objective optimization
Entezari-Maleki et al. A genetic algorithm to increase the throughput of the computational grids
CN116450366B (en) Multi-objective optimal scheduling method, equipment and medium for satellite measurement, operation and control resources
CN106548301B (en) Power consumer clustering method and device
CN110209487B (en) ISAR resource scheduling method based on genetic algorithm
JPH05319707A (en) Control method for group management elevator
Hussein et al. Dynamic process scheduling using genetic algorithm
Laili et al. Rotated neighbor learning-based auto-configured evolutionary algorithm
CN114707808A (en) Reverse-order equipment network comprehensive scheduling method based on dynamic root node process set
Oda et al. Performance evaluation of WMN using WMN-GA system for different mutation operators
CN111858003A (en) Hadoop optimal parameter evaluation method and device
CN116401037B (en) Genetic algorithm-based multi-task scheduling method and system

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant