[go: up one dir, main page]

CN111262615B - Multitask-oriented satellite communication network adaptive compensation method and device - Google Patents

Multitask-oriented satellite communication network adaptive compensation method and device Download PDF

Info

Publication number
CN111262615B
CN111262615B CN201911375189.1A CN201911375189A CN111262615B CN 111262615 B CN111262615 B CN 111262615B CN 201911375189 A CN201911375189 A CN 201911375189A CN 111262615 B CN111262615 B CN 111262615B
Authority
CN
China
Prior art keywords
satellite
sub
compensation
compensation scheme
task type
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
CN201911375189.1A
Other languages
Chinese (zh)
Other versions
CN111262615A (en
Inventor
忻向军
刘博�
张琦
李姗姗
高然
陶滢
田清华
田凤
张丽佳
沈宇飞
陈东
曹桂兴
刘乃金
张伟
王拥军
杨雷静
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.)
Beijing Institute of Technology BIT
Beijing University of Posts and Telecommunications
China Academy of Space Technology CAST
Original Assignee
Beijing Institute of Technology BIT
Beijing University of Posts and Telecommunications
China Academy of Space Technology CAST
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 Beijing Institute of Technology BIT, Beijing University of Posts and Telecommunications, China Academy of Space Technology CAST filed Critical Beijing Institute of Technology BIT
Priority to CN201911375189.1A priority Critical patent/CN111262615B/en
Publication of CN111262615A publication Critical patent/CN111262615A/en
Application granted granted Critical
Publication of CN111262615B publication Critical patent/CN111262615B/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
    • H04B7/1851Systems using a satellite or space-based relay
    • 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
    • H04B7/18519Operations control, administration or maintenance
    • 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
    • H04B7/18521Systems of inter linked satellites, i.e. inter satellite service
    • 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
    • H04B7/18528Satellite systems for providing two-way communications service to a network of fixed stations, i.e. fixed satellite service or very small aperture terminal [VSAT] system
    • 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
    • H04B7/1853Satellite systems for providing telephony service to a mobile station, i.e. mobile satellite service
    • 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
    • H04B7/1853Satellite systems for providing telephony service to a mobile station, i.e. mobile satellite service
    • H04B7/18532Arrangements for managing transmission, i.e. for transporting data or a signalling message

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)
  • Radio Relay Systems (AREA)
  • Mobile Radio Communication Systems (AREA)

Abstract

本发明实施例提供了一种面向多任务的卫星通信网络自适应补偿方法和装置,所述方法包括:获取当前通信任务的任务类型;根据所述任务类型,确定总体补偿方案;其中,所述总体补偿方案包括:与所述当前通信任务中涉及的各传输链路分别对应的子补偿方案;所述各传输链路为激光链路或者微波链路;通信过程中,分别在所述各传输链路阶段,采用与所述各传输链路对应的子补偿方案进行通信补偿。本发明实施例中,根据当前通信任务的任务类型,确定出与当前通信任务中涉及的各传输链路分别对应的子补偿方案,并在各传输链路阶段,分别采用对应的子补偿方案进行通信补偿,因此,提高了网络传输的性能。

Figure 201911375189

Embodiments of the present invention provide a multi-task-oriented satellite communication network adaptive compensation method and device, the method includes: acquiring a task type of a current communication task; determining an overall compensation scheme according to the task type; wherein, the The overall compensation scheme includes: sub-compensation schemes corresponding to each transmission link involved in the current communication task; each transmission link is a laser link or a microwave link; In the link stage, the sub-compensation scheme corresponding to each transmission link is used for communication compensation. In the embodiment of the present invention, according to the task type of the current communication task, a sub-compensation scheme corresponding to each transmission link involved in the current communication task is determined, and in each transmission link stage, the corresponding sub-compensation scheme is used to perform Communication compensation, therefore, improves the performance of network transmissions.

Figure 201911375189

Description

面向多任务的卫星通信网络自适应补偿方法和装置Multitask-oriented satellite communication network adaptive compensation method and device

技术领域technical field

本发明涉及卫星通信技术领域,特别是涉及一种面向多任务的卫星通信网络自适应补偿方法和装置。The invention relates to the technical field of satellite communication, in particular to a multi-task-oriented satellite communication network adaptive compensation method and device.

背景技术Background technique

图1为卫星通信网络的体系架构图,卫星通信网络由天基骨干网、天基接入网及地面系统三部分组成,其中,天基骨干网采用激光通信,由GEO(Geosychronons Earth Orbit,地球同步轨道)卫星和MEO(medium earth orbit,中地球轨道)卫星通过ISL(Inter-Satellite Link,星间链路)技术连接构成,负责空间数据的传输与分发,为所连接的LEO(medium earth orbit,低地球轨道)卫星提供信息交换服务;天基接入网采用激光与微波融合接入方案,由LEO卫星移动通信星座构成,通过ISL与天基骨干网相连,并为地面系统的移动用户提供空间信息服务。Figure 1 is the architecture diagram of the satellite communication network. The satellite communication network consists of three parts: the space-based backbone network, the space-based access network and the ground system. Synchronous orbit) satellite and MEO (medium earth orbit, medium earth orbit) satellite are connected through ISL (Inter-Satellite Link, inter-satellite link) technology, responsible for the transmission and distribution of space data, for the connected LEO (medium earth orbit, inter-satellite link) technology , Low Earth Orbit) satellites provide information exchange services; the space-based access network adopts the laser and microwave fusion access scheme, which is composed of the LEO satellite mobile communication constellation, which is connected to the space-based backbone network through ISL, and provides mobile users of the ground system. Spatial Information Service.

上述卫星通信网络中,存在多种传输链路,如:卫星之间的星间链路、卫星与地面之间的星地链路,具体的,地面与卫星通信时的星地上行链路、卫星与地面通信时的星地下行链路。上述各种链路中均会存在一些影响网络传输性能的外界因素,例如,星间链路阶段,由于卫星轨道、卫星姿态漂移和星上热环境变化等因素的影响,会使得光束瞄准角度存在一定的偏差;星地上行链路或者星地下行链路阶段,由于大气湍流等因素的影响,会使得接收端接收到的激光信号的光束质量变差等。In the above-mentioned satellite communication network, there are various transmission links, such as: the inter-satellite link between satellites, the satellite-ground link between the satellite and the ground, specifically, the satellite-ground uplink when the ground communicates with the satellite, The satellite-to-ground downlink when the satellite communicates with the ground. There are some external factors that affect the network transmission performance in the above-mentioned various links. For example, in the inter-satellite link stage, due to the influence of factors such as satellite orbit, satellite attitude drift, and on-board thermal environment changes, the beam aiming angle will exist. A certain deviation; in the satellite-to-ground uplink or satellite-to-ground downlink stage, due to the influence of atmospheric turbulence and other factors, the beam quality of the laser signal received by the receiving end will deteriorate, etc.

同时,采用上述卫星通信网络进行数据传输时,可能存在多种通信任务,不同通信任务中涉及的传输链路的种类也不同,因此,针对不同的通信任务,如何采取合适的补偿方法,以提高网络传输的性能,是一个亟待解决的问题。At the same time, when the above-mentioned satellite communication network is used for data transmission, there may be various communication tasks, and the types of transmission links involved in different communication tasks are also different. Therefore, for different communication tasks, how to adopt appropriate compensation methods to improve The performance of network transmission is an urgent problem to be solved.

发明内容SUMMARY OF THE INVENTION

本发明实施例的目的在于提供一种面向多任务的卫星通信网络自适应补偿方法和装置,以提高网络传输的性能。具体技术方案如下:The purpose of the embodiments of the present invention is to provide a multi-task-oriented satellite communication network adaptive compensation method and device, so as to improve the performance of network transmission. The specific technical solutions are as follows:

第一方面,本发明实施例提供了一种面向多任务的卫星通信网络自适应补偿方法,包括:In a first aspect, an embodiment of the present invention provides a multi-task-oriented satellite communication network adaptive compensation method, including:

获取当前通信任务的任务类型;Get the task type of the current communication task;

根据所述任务类型,确定总体补偿方案;其中,所述总体补偿方案包括:与所述当前通信任务中涉及的各传输链路分别对应的子补偿方案;所述各传输链路为激光链路或者微波链路;Determine an overall compensation scheme according to the task type; wherein, the overall compensation scheme includes: sub-compensation schemes corresponding to each transmission link involved in the current communication task; each transmission link is a laser link or microwave links;

通信过程中,分别在所述各传输链路阶段,采用与所述各传输链路对应的子补偿方案进行通信补偿。During the communication process, at each transmission link stage, the sub-compensation scheme corresponding to each transmission link is used to perform communication compensation.

进一步的,所述任务类型包括:第一任务类型、第二任务类型、第三任务类型、第四任务类型以及第五任务类型;Further, the task types include: a first task type, a second task type, a third task type, a fourth task type, and a fifth task type;

所述第一任务类型为:第一地面用户通过所述卫星通信网络中的低地球轨道LEO卫星或者中地球轨道MEO卫星接入地球同步轨道GEO卫星,并通过所述GEO卫星向第二地面用户发送数据的任务类型;The first task type is: a first ground user accesses a geosynchronous orbit GEO satellite through a low earth orbit LEO satellite or a medium earth orbit MEO satellite in the satellite communication network, and communicates with the second ground user through the GEO satellite. The type of task that sent the data;

所述第二任务类型为:第三地面用户通过所述LEO卫星或者所述MEO卫星向第四地面用户发送数据的任务类型;The second task type is: a task type in which the third ground user sends data to the fourth ground user through the LEO satellite or the MEO satellite;

所述第三任务类型为:第五地面用户通过所述GEO卫星向第六地面用户发送数据的任务类型;The third task type is: a task type in which the fifth ground user sends data to the sixth ground user through the GEO satellite;

所述第四任务类型为:所述GEO卫星通过所述LEO卫星或者所述MEO卫星向第七地面用户发送数据的任务类型;The fourth task type is: a task type in which the GEO satellite sends data to the seventh ground user through the LEO satellite or the MEO satellite;

所述第五任务类型为:所述GEO卫星直接向第八地面用户发送数据的任务类型;The fifth task type is: the task type in which the GEO satellite directly sends data to the eighth ground user;

当所述当前通信任务的任务类型为所述第一任务类型、所述第二任务类型或者所述第三任务类型中的任一任务类型时,所述当前通信任务中涉及的各传输链路分别为:星地上行链路、星间链路以及星地下行链路;When the task type of the current communication task is any one of the first task type, the second task type or the third task type, each transmission link involved in the current communication task They are: satellite-to-ground uplink, inter-satellite link and satellite-to-ground downlink;

当所述当前通信任务的任务类型为所述第四任务类型时,所述当前通信任务中涉及的各传输链路分别为:星间链路和星地下行链路;When the task type of the current communication task is the fourth task type, each transmission link involved in the current communication task is: an inter-satellite link and a satellite-ground downlink;

当所述当前通信任务的任务类型为所述第五任务类型时,所述当前通信任务中涉及的传输链路为:星地下行链路。When the task type of the current communication task is the fifth task type, the transmission link involved in the current communication task is: satellite-ground downlink.

进一步的,与所述星地上行链路对应的子补偿方案包括:基于自适应编码技术的第一子补偿方案、基于概率整形技术的第二子补偿方案、基于功率自适应控制技术的第三子补偿方案以及基于激光光束瞄准角补偿技术的第四子补偿方案;Further, the sub-compensation schemes corresponding to the satellite-ground uplink include: a first sub-compensation scheme based on adaptive coding technology, a second sub-compensation scheme based on probability shaping technology, and a third sub-compensation scheme based on power adaptive control technology. Sub-compensation scheme and the fourth sub-compensation scheme based on laser beam aiming angle compensation technology;

与所述星间链路对应的子补偿方案包括:基于粗跟踪误差补偿技术的第五子补偿方案和基于光束瞄准偏差补偿技术的第六子补偿方案;The sub-compensation schemes corresponding to the inter-satellite link include: a fifth sub-compensation scheme based on the coarse tracking error compensation technology and a sixth sub-compensation scheme based on the beam aiming deviation compensation technology;

与所述星地下行链路对应的子补偿方案包括:所述第一子补偿方案、所述第二子补偿方案、所述第三子补偿方案以及所述第四子补偿方案。The sub-compensation scheme corresponding to the satellite-ground downlink includes: the first sub-compensation scheme, the second sub-compensation scheme, the third sub-compensation scheme, and the fourth sub-compensation scheme.

进一步的,所述第三子补偿方案包括:第一功率子补偿方案和第二功率子补偿方案;其中,所述第一功率子补偿方案中不存在功率补偿上限;所述第二功率子补偿方案中存在功率补偿上限;Further, the third sub-compensation scheme includes: a first power sub-compensation scheme and a second power sub-compensation scheme; wherein, there is no power compensation upper limit in the first power sub-compensation scheme; the second power sub-compensation scheme There is an upper limit of power compensation in the scheme;

与所述星地上行链路对应的第三子补偿方案为所述第一功率子补偿方案;the third sub-compensation scheme corresponding to the satellite-ground uplink is the first power sub-compensation scheme;

与所述星地下行链路对应的第三子补偿方案为所述第二功率子补偿方案。The third sub-compensation scheme corresponding to the satellite-ground downlink is the second power sub-compensation scheme.

第二方面,本发明实施例提供了一种面向多任务的卫星通信网络自适应补偿装置,包括:In a second aspect, an embodiment of the present invention provides a multi-task-oriented satellite communication network adaptive compensation device, including:

任务类型获取模块,用于获取当前通信任务的任务类型;The task type acquisition module is used to obtain the task type of the current communication task;

总体补偿方案确定模块,用于根据所述任务类型,确定总体补偿方案;其中,所述总体补偿方案包括:与所述当前通信任务中涉及的各传输链路分别对应的子补偿方案;所述各传输链路为激光链路或者微波链路;an overall compensation scheme determination module, configured to determine an overall compensation scheme according to the task type; wherein the overall compensation scheme includes: sub-compensation schemes corresponding to each transmission link involved in the current communication task; the Each transmission link is a laser link or a microwave link;

通信补偿模块,用于通信过程中,分别在所述各传输链路阶段,采用与所述各传输链路对应的子补偿方案进行通信补偿。The communication compensation module is used to perform communication compensation by adopting the sub-compensation scheme corresponding to each transmission link in each transmission link stage in the communication process.

进一步的,所述任务类型包括:第一任务类型、第二任务类型、第三任务类型、第四任务类型以及第五任务类型;Further, the task types include: a first task type, a second task type, a third task type, a fourth task type, and a fifth task type;

所述第一任务类型为:第一地面用户通过所述卫星通信网络中的低地球轨道LEO卫星或者中地球轨道MEO卫星接入地球同步轨道GEO卫星,并通过所述GEO卫星向第二地面用户发送数据的任务类型;The first task type is: a first ground user accesses a geosynchronous orbit GEO satellite through a low earth orbit LEO satellite or a medium earth orbit MEO satellite in the satellite communication network, and communicates with the second ground user through the GEO satellite. The type of task that sent the data;

所述第二任务类型为:第三地面用户通过所述LEO卫星或者所述MEO卫星向第四地面用户发送数据的任务类型;The second task type is: a task type in which the third ground user sends data to the fourth ground user through the LEO satellite or the MEO satellite;

所述第三任务类型为:第五地面用户通过所述GEO卫星向第六地面用户发送数据的任务类型;The third task type is: a task type in which the fifth ground user sends data to the sixth ground user through the GEO satellite;

所述第四任务类型为:所述GEO卫星通过所述LEO卫星或者所述MEO卫星向第七地面用户发送数据的任务类型;The fourth task type is: a task type in which the GEO satellite sends data to the seventh ground user through the LEO satellite or the MEO satellite;

所述第五任务类型为:所述GEO卫星直接向第八地面用户发送数据的任务类型;The fifth task type is: the task type in which the GEO satellite directly sends data to the eighth ground user;

当所述当前通信任务的任务类型为所述第一任务类型、所述第二任务类型或者所述第三任务类型中的任一任务类型时,所述当前通信任务中涉及的各传输链路分别为:星地上行链路、星间链路以及星地下行链路;When the task type of the current communication task is any one of the first task type, the second task type or the third task type, each transmission link involved in the current communication task They are: satellite-to-ground uplink, inter-satellite link and satellite-to-ground downlink;

当所述当前通信任务的任务类型为所述第四任务类型时,所述当前通信任务中涉及的各传输链路分别为:星间链路和星地下行链路;When the task type of the current communication task is the fourth task type, each transmission link involved in the current communication task is: an inter-satellite link and a satellite-ground downlink;

当所述当前通信任务的任务类型为所述第五任务类型时,所述当前通信任务中涉及的传输链路为:星地下行链路。When the task type of the current communication task is the fifth task type, the transmission link involved in the current communication task is: satellite-ground downlink.

进一步的,与所述星地上行链路对应的子补偿方案包括:基于自适应编码技术的第一子补偿方案、基于概率整形技术的第二子补偿方案、基于功率自适应控制技术的第三子补偿方案以及基于激光光束瞄准角补偿技术的第四子补偿方案;Further, the sub-compensation schemes corresponding to the satellite-ground uplink include: a first sub-compensation scheme based on adaptive coding technology, a second sub-compensation scheme based on probability shaping technology, and a third sub-compensation scheme based on power adaptive control technology. Sub-compensation scheme and the fourth sub-compensation scheme based on laser beam aiming angle compensation technology;

与所述星间链路对应的子补偿方案包括:基于粗跟踪误差补偿技术的第五子补偿方案和基于光束瞄准偏差补偿技术的第六子补偿方案;The sub-compensation schemes corresponding to the inter-satellite link include: a fifth sub-compensation scheme based on the coarse tracking error compensation technology and a sixth sub-compensation scheme based on the beam aiming deviation compensation technology;

与所述星地下行链路对应的子补偿方案包括:所述第一子补偿方案、所述第二子补偿方案、所述第三子补偿方案以及所述第四子补偿方案。The sub-compensation scheme corresponding to the satellite-ground downlink includes: the first sub-compensation scheme, the second sub-compensation scheme, the third sub-compensation scheme, and the fourth sub-compensation scheme.

进一步的,所述第三子补偿方案包括:第一功率子补偿方案和第二功率子补偿方案;其中,所述第一功率子补偿方案中不存在功率补偿上限;所述第二功率子补偿方案中存在功率补偿上限;Further, the third sub-compensation scheme includes: a first power sub-compensation scheme and a second power sub-compensation scheme; wherein, there is no power compensation upper limit in the first power sub-compensation scheme; the second power sub-compensation scheme There is an upper limit of power compensation in the scheme;

与所述星地上行链路对应的第三子补偿方案为所述第一功率子补偿方案;the third sub-compensation scheme corresponding to the satellite-ground uplink is the first power sub-compensation scheme;

与所述星地下行链路对应的第三子补偿方案为所述第二功率子补偿方案。The third sub-compensation scheme corresponding to the satellite-ground downlink is the second power sub-compensation scheme.

第三方面,本发明实施例提供了一种电子设备,包括处理器、通信接口、存储器和通信总线,其中,处理器,通信接口,存储器通过通信总线完成相互间的通信;In a third aspect, an embodiment of the present invention provides an electronic device, including a processor, a communication interface, a memory, and a communication bus, wherein the processor, the communication interface, and the memory communicate with each other through the communication bus;

存储器,用于存放计算机程序;memory for storing computer programs;

处理器,用于执行存储器上所存放的程序时,实现上述任一面向多任务的卫星通信网络自适应补偿方法的步骤。The processor is configured to implement the steps of any of the above-mentioned multi-task-oriented satellite communication network adaptive compensation methods when executing the program stored in the memory.

第四方面,本发明实施例还提供了一种计算机可读存储介质,所述计算机可读存储介质中存储有指令,当其在计算机上运行时,使得计算机执行上述任一所述的面向多任务的卫星通信网络自适应补偿方法。In a fourth aspect, an embodiment of the present invention further provides a computer-readable storage medium, where instructions are stored in the computer-readable storage medium, and when the computer-readable storage medium runs on a computer, the computer can execute any of the above-mentioned multi-oriented An adaptive compensation method for satellite communication networks for missions.

第五方面,本发明实施例还提供了一种包含指令的计算机程序产品,当其在计算机上运行时,使得计算机执行上述任一所述的面向多任务的卫星通信网络自适应补偿方法。In a fifth aspect, an embodiment of the present invention further provides a computer program product including instructions, which, when running on a computer, enables the computer to execute any of the above-mentioned multitasking-oriented satellite communication network adaptive compensation methods.

本发明实施例提供的一种面向多任务的卫星通信网络自适应补偿方法和装置,获取当前通信任务的任务类型;根据所述任务类型,确定总体补偿方案;其中,所述总体补偿方案包括:与所述当前通信任务中涉及的各传输链路分别对应的子补偿方案;所述各传输链路为激光链路或者微波链路;通信过程中,分别在所述各传输链路阶段,采用与所述各传输链路对应的子补偿方案进行通信补偿。本发明实施例中,根据当前通信任务的任务类型,确定出与当前通信任务中涉及的各传输链路分别对应的子补偿方案,并在各传输链路阶段,分别采用对应的子补偿方案进行通信补偿,因此,提高了网络传输的性能。A multi-task-oriented satellite communication network adaptive compensation method and device provided by an embodiment of the present invention acquires the task type of a current communication task; determines an overall compensation scheme according to the task type; wherein the overall compensation scheme includes: A sub-compensation scheme corresponding to each transmission link involved in the current communication task; each transmission link is a laser link or a microwave link; in the communication process, in each transmission link stage, the Communication compensation is performed on the sub-compensation schemes corresponding to the respective transmission links. In the embodiment of the present invention, according to the task type of the current communication task, a sub-compensation scheme corresponding to each transmission link involved in the current communication task is determined, and in each transmission link stage, the corresponding sub-compensation scheme is used to perform Communication compensation, therefore, improves the performance of network transmissions.

当然,实施本发明的任一产品或方法并不一定需要同时达到以上所述的所有优点。Of course, it is not necessary for any product or method of the present invention to achieve all of the advantages described above at the same time.

附图说明Description of drawings

为了更清楚地说明本发明实施例或现有技术中的技术方案,下面将对实施例或现有技术描述中所需要使用的附图作简单地介绍,显而易见地,下面描述中的附图仅仅是本发明的一些实施例,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,还可以根据这些附图获得其他的附图。In order to explain the embodiments of the present invention or the technical solutions in the prior art more clearly, the following briefly introduces the accompanying drawings that need to be used in the description of the embodiments or the prior art. Obviously, the accompanying drawings in the following description are only These are some embodiments of the present invention. For those of ordinary skill in the art, other drawings can also be obtained according to these drawings without creative efforts.

图1为卫星通信网络的体系架构图;Figure 1 is an architecture diagram of a satellite communication network;

图2为本发明实施例提供的面向多任务的卫星通信网络自适应补偿方法的一种流程示意图;2 is a schematic flowchart of a multitask-oriented satellite communication network adaptive compensation method provided by an embodiment of the present invention;

图3为本发明实施例提供的面向多任务的卫星通信网络自适应补偿装置的结构示意图;3 is a schematic structural diagram of a multitask-oriented satellite communication network adaptive compensation device provided by an embodiment of the present invention;

图4为本发明实施例提供的电子设备的结构示意图。FIG. 4 is a schematic structural diagram of an electronic device provided by an embodiment of the present invention.

具体实施方式Detailed ways

下面将结合本发明实施例中的附图,对本发明实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例仅仅是本发明一部分实施例,而不是全部的实施例。基于本发明中的实施例,本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

图2为本发明实施例提供的面向多任务的卫星通信网络自适应补偿方法的一种流程示意图,包括:2 is a schematic flowchart of a multitask-oriented satellite communication network adaptive compensation method provided by an embodiment of the present invention, including:

步骤201,获取当前通信任务的任务类型。Step 201, acquiring the task type of the current communication task.

步骤202,根据任务类型,确定总体补偿方案;其中,总体补偿方案包括:与当前通信任务中涉及的各传输链路分别对应的子补偿方案;各传输链路为激光链路或者微波链路。Step 202: Determine an overall compensation scheme according to the task type; wherein the overall compensation scheme includes: sub-compensation schemes corresponding to each transmission link involved in the current communication task; each transmission link is a laser link or a microwave link.

其中,地面固定用户既可以通过微波也可以通过激光与卫星通信,而地面移动用户则只能通过微波与卫星通信;卫星与卫星直接的星间链路为激光通信链路。Among them, fixed users on the ground can communicate with satellites either through microwaves or lasers, while mobile users on the ground can only communicate with satellites through microwaves; the direct inter-satellite links between satellites are laser communication links.

步骤203,通信过程中,分别在各传输链路阶段,采用与各传输链路对应的子补偿方案进行通信补偿。Step 203 , in the communication process, in each transmission link stage, the sub-compensation scheme corresponding to each transmission link is used to perform communication compensation.

在上述实施例中,可以根据当前通信任务的任务类型,确定出与当前通信任务中涉及的各传输链路分别对应的子补偿方案,并在各传输链路阶段,分别采用对应的子补偿方案进行通信补偿,因此,提高了网络传输的性能。In the above embodiment, the sub-compensation scheme corresponding to each transmission link involved in the current communication task can be determined according to the task type of the current communication task, and the corresponding sub-compensation scheme is adopted in each transmission link stage. Communication compensation is performed, therefore, the performance of network transmission is improved.

进一步的,在步骤201中获取的当前通信任务的任务类型可以包括如下五种:第一任务类型、第二任务类型、第三任务类型、第四任务类型以及第五任务类型;Further, the task types of the current communication task acquired in step 201 may include the following five types: the first task type, the second task type, the third task type, the fourth task type and the fifth task type;

具体的,第一任务类型为:第一地面用户通过卫星通信网络中的低地球轨道LEO卫星或者中地球轨道MEO卫星接入地球同步轨道GEO卫星,并通过GEO卫星向第二地面用户发送数据的任务类型;第二任务类型为:第三地面用户通过LEO卫星或者MEO卫星向第四地面用户发送数据的任务类型;第三任务类型为:第五地面用户通过GEO卫星向第六地面用户发送数据的任务类型;第四任务类型为:GEO卫星通过LEO卫星或者MEO卫星向第七地面用户发送数据的任务类型;第五任务类型为:GEO卫星直接向第八地面用户发送数据的任务类型。其中,第一地面用户可以为任一地面用户,第二地面用户可以为除第一地面用户之外的任一地面用户;第三地面用户可以为任一地面用户,第四地面用户可以为除第一地面用户之外的任一地面用户;第五地面用户可以为任一地面用户,第六地面用户可以为除第一地面用户之外的任一地面用户;第七地面用户可以为任一地面用户;第八地面用户也可以为任一地面用户。Specifically, the first task type is: a first ground user accesses a geosynchronous orbit GEO satellite through a low earth orbit LEO satellite or a medium earth orbit MEO satellite in the satellite communication network, and sends data to the second ground user through the GEO satellite Task type; the second task type is: the third ground user sends data to the fourth ground user through the LEO satellite or the MEO satellite; the third task type is: the fifth ground user sends data to the sixth ground user through the GEO satellite The fourth task type is: the GEO satellite sends data to the seventh ground user through the LEO satellite or the MEO satellite; the fifth task type is: the GEO satellite directly sends data to the eighth ground user. The first ground user may be any ground user, the second ground user may be any ground user except the first ground user; the third ground user may be any ground user, and the fourth ground user may be any ground user except the first ground user Any ground user except the first ground user; the fifth ground user can be any ground user, the sixth ground user can be any ground user except the first ground user; the seventh ground user can be any ground user Ground user; the eighth ground user can also be any ground user.

若当前通信任务的任务类型为第一任务类型、第二任务类型或者第三任务类型中的任一任务类型,当前通信任务中涉及的各传输链路分别为:星地上行链路、星间链路以及星地下行链路;If the task type of the current communication task is any one of the first task type, the second task type or the third task type, the transmission links involved in the current communication task are: satellite-ground uplink, inter-satellite link and satellite-to-ground downlink;

若当前通信任务的任务类型为第四任务类型,当前通信任务中涉及的各传输链路分别为:星间链路和星地下行链路;If the task type of the current communication task is the fourth task type, the transmission links involved in the current communication task are: inter-satellite link and satellite-ground downlink;

若当前通信任务的任务类型为第五任务类型,当前通信任务中涉及的传输链路为:星地下行链路。If the task type of the current communication task is the fifth task type, the transmission link involved in the current communication task is: satellite-ground downlink.

在步骤202中,根据任务类型,确定总体补偿方案时,先确定当前通信任务中涉及的传输链路,然后再根据传输链路确定对应的子补偿方案,从而组成总体补偿方案。In step 202, when determining the overall compensation scheme according to the task type, firstly determine the transmission link involved in the current communication task, and then determine the corresponding sub-compensation scheme according to the transmission link, so as to form the overall compensation scheme.

进一步的,与星地上行链路对应的子补偿方案包括:基于自适应编码技术的第一子补偿方案、基于概率整形技术的第二子补偿方案、基于功率自适应控制技术的第三子补偿方案以及基于激光光束瞄准角补偿技术的第四子补偿方案。Further, the sub-compensation scheme corresponding to the satellite-ground uplink includes: a first sub-compensation scheme based on adaptive coding technology, a second sub-compensation scheme based on probability shaping technology, and a third sub-compensation scheme based on power adaptive control technology. scheme and the fourth sub-compensation scheme based on laser beam aiming angle compensation technology.

具体的,星地上行链路,可以分为两个部分:地面用户到大气层部分;大气层到卫星部分。其中,在地面用户到大气层部分中,由于发射端处于地球表面大气中,接收端在远离地球表层大气的自由空间中,因此大气湍流对接收光场的影响表现为远场效应,在光束通过地球表面大气层过程中,远场效应会导致接收光强和光斑中心的随机起伏,即远场效应影响接收端激光信号的光束质量;同时,大气层干扰也会造成信道内传输信号的衰减;在大气层到卫星部分中,由于卫星轨道、卫星姿态漂移和星上热环境变化的影响,会导致光束瞄准角度存在偏差。因此,在星地上行链路,需要分别从光束质量、传输信号衰减以及激光光束瞄准角度偏差这三个方面进行通信补偿。Specifically, the satellite-to-ground uplink can be divided into two parts: the part from the ground user to the atmosphere; the part from the atmosphere to the satellite. Among them, in the part from the ground user to the atmosphere, since the transmitting end is in the earth's surface atmosphere, and the receiving end is in the free space far away from the earth's surface atmosphere, the influence of atmospheric turbulence on the receiving light field is manifested as a far-field effect. In the process of the surface atmosphere, the far-field effect will cause random fluctuations in the received light intensity and the center of the spot, that is, the far-field effect affects the beam quality of the laser signal at the receiving end; at the same time, atmospheric interference will also cause the attenuation of the transmitted signal in the channel; In the satellite part, due to the influence of satellite orbit, satellite attitude drift and on-board thermal environment changes, the beam aiming angle will be deviated. Therefore, in the satellite-to-ground uplink, it is necessary to perform communication compensation from three aspects: beam quality, transmission signal attenuation, and laser beam aiming angle deviation.

为了提高通信质量,可以使用基于自适应编码技术的第一子补偿方案:在发射端采用低密度奇偶校验码信道编码技术进行信道编码,并在接收到通过BP(BackPropagation,误差后向传播)算法进行译码。由于低密度奇偶校验码信道编码技术可以实现自适应信号速率调整,因此,可以有效地提高系统的抗干扰能力,从而改善通信质量。对于低密度奇偶校验码信道编码技术和BP算法的具体实现过程,可以参考相关现有技术,此处不再赘述。In order to improve the communication quality, the first sub-compensation scheme based on adaptive coding technology can be used: the channel coding technology of low-density parity check code is used at the transmitting end for channel coding, and BP (BackPropagation, error backward propagation) is used at the receiving end. algorithm to decode. Since the low-density parity-check code channel coding technology can realize adaptive signal rate adjustment, it can effectively improve the anti-interference ability of the system, thereby improving the communication quality. For the specific implementation process of the low-density parity-check code channel coding technology and the BP algorithm, reference may be made to the related prior art, which will not be repeated here.

为了提高信息传输的容量,可以使用基于概率整形技术的第二子补偿方案:在发射端采用基于恒定构成分布匹配器的概率整形方案,具体的:将要发送的二进制数据经过恒定构成分布匹配器变为符号数据,将其作均匀分布的二进制映射,再进行FEC(ForwardErrorCorrection,前向纠错)编码,然后再对应高阶调制编码,当通过光通信信道后,在接收端依次作高阶调制解码、FEC解码、二进制转符号映射、恒定构成分布匹配器解调,最后得到原始数据。上述使得输入符号遵循信道最优匹配分布,使得互信息更接近理论信道容量。当对高阶调制技术作概率整形时,发射端内层信号概率高,往外概率越来越低,当光信噪比超过某一定值时,其互信息更接近于理论信道容量,同时在相同发射光功率情况下,使用概率整形的光通信系统误码率低于使用均匀分布的光通信系统误码率。In order to improve the capacity of information transmission, a second sub-compensation scheme based on probability shaping technology can be used: a probability shaping scheme based on a constant composition distribution matcher is used at the transmitting end, specifically: the binary data to be sent is transformed into a constant composition distribution matcher. For symbol data, make it into a uniformly distributed binary map, and then perform FEC (Forward Error Correction, forward error correction) coding, and then correspond to high-order modulation and coding. , FEC decoding, binary to symbol mapping, constant composition distribution matcher demodulation, and finally get the original data. The above makes the input symbols follow the optimal matching distribution of the channel, so that the mutual information is closer to the theoretical channel capacity. When probabilistic shaping is performed on high-order modulation techniques, the inner signal probability of the transmitter is high, and the outward probability is lower and lower. When the optical signal-to-noise ratio exceeds a certain value, the mutual information is closer to the theoretical channel capacity. Under the condition of transmitting optical power, the bit error rate of the optical communication system using probability shaping is lower than that of the optical communication system using uniform distribution.

为了补偿传输信号的衰减,可以使用基于功率自适应控制技术的第三子补偿方案,主要过程为:指根据信道内传输信号的衰减情况,适当的提高发端的发送功率,用以补偿由降雨、大气湍流等因素造成的信号衰减,从而使接收端信号的功率保持在一定范围内。In order to compensate the attenuation of the transmission signal, the third sub-compensation scheme based on the power adaptive control technology can be used. The signal attenuation caused by factors such as atmospheric turbulence keeps the power of the signal at the receiving end within a certain range.

进一步的,第三子补偿方案包括:第一功率子补偿方案和第二功率子补偿方案;其中,第一功率子补偿方案中不存在功率补偿上限;第二功率子补偿方案中存在功率补偿上限。Further, the third sub-compensation scheme includes: a first power sub-compensation scheme and a second power sub-compensation scheme; wherein, there is no power compensation upper limit in the first power sub-compensation scheme; and a power compensation upper limit exists in the second power sub-compensation scheme .

在星地上行链路中,发射端为地面用户,因此,发射功率不受限,即:不存在功率补偿上限,因此,可以使用第一功率子补偿方案进行功率补偿。具体的:接收端对接收到的信号进行SINR(Signal to Interference plus Noise Ratio,信号与干扰加噪声比)测量估计,根据功率控制算法生成对应的功率控制指令,并将相应的TPC按照一定的数据格式与基带数据组帧调制,进而,通过下行链路传输到发射端,发射端对接收的调制信号进行解调还原得到基带数据,并按照通信协议所规定的数据帧格式提取出相应的功控指令TPC,根据指令产生相应的增益调节量,进而对上行链路调制信号的发射功率进行相应的调整。In the satellite-ground uplink, the transmitting end is a ground user, so the transmit power is not limited, that is, there is no upper limit of power compensation, therefore, the first power sub-compensation scheme can be used for power compensation. Specifically: the receiving end performs SINR (Signal to Interference plus Noise Ratio, Signal to Interference plus Noise Ratio) measurement and estimation on the received signal, generates a corresponding power control command according to a power control algorithm, and calculates the corresponding TPC according to certain data. The format and baseband data are framed and modulated, and then transmitted to the transmitter through the downlink. The transmitter demodulates and restores the received modulated signal to obtain baseband data, and extracts the corresponding power control according to the data frame format specified by the communication protocol. The TPC is instructed, and the corresponding gain adjustment amount is generated according to the instruction, and then the transmit power of the uplink modulated signal is adjusted accordingly.

为了降低激光光束瞄准角度偏差,可以使用基于激光光束瞄准角补偿技术的第四子补偿方案:首先根据卫星坐标系与激光通信终端参考坐标系光束瞄准偏角和捕获完成时刻的瞄准角度位置,计算得到终端在轨光束瞄准偏差,然后采用坐标修正矩阵,将得到的光束瞄准偏差修正角度上注到卫星光通信终端,对终端瞄准偏差进行修正。In order to reduce the deviation of the laser beam aiming angle, the fourth sub-compensation scheme based on the laser beam aiming angle compensation technology can be used. The aiming deviation of the terminal on-orbit beam is obtained, and then a coordinate correction matrix is used to inject the obtained beam aiming deviation correction angle to the satellite optical communication terminal to correct the terminal aiming deviation.

进一步的,与星间链路对应的子补偿方案包括:基于粗跟踪误差补偿技术的第五子补偿方案和基于光束瞄准偏差补偿技术的第六子补偿方案;Further, the sub-compensation scheme corresponding to the inter-satellite link includes: a fifth sub-compensation scheme based on the coarse tracking error compensation technology and a sixth sub-compensation scheme based on the beam aiming deviation compensation technology;

具体的,由于星间链路的信道环境是深空,卫星平台振动、星间的相对运动、系统内部电子和机械噪声等因素,会导致卫星瞄准在粗跟踪过程中产生角度误差;同时,光通信终端与卫星平台的耦合运动,也会导致光束瞄准偏差,因此,在星间链路,需要分别从粗跟踪误差和光束瞄准偏差两个方面进行通信补偿。Specifically, since the channel environment of the inter-satellite link is deep space, the vibration of the satellite platform, the relative motion between the satellites, the electronic and mechanical noise inside the system and other factors will cause the satellite aiming to produce angular errors during the rough tracking process; The coupling motion between the communication terminal and the satellite platform will also lead to the beam aiming deviation. Therefore, in the inter-satellite link, it is necessary to perform communication compensation from two aspects, the coarse tracking error and the beam aiming deviation.

为了降低粗跟踪误差,可以使用基于粗跟踪误差补偿技术的第五子补偿方案,基于粗跟踪误差补偿技术,确定最佳束散角。当信息传输率一定时,随着链路距离的增大错误概率逐渐增大,随着跟瞄误差角抖动方差的增大错误概率逐渐增大,随着发射功率的增大错误概率逐渐减小,最佳束散角的选择可以使对应的错误概率达到最小;在一定错误概率要求下,最佳束散角的选择可以使对应的信息传输率达到最大;在一定信息传输率下,选择最佳束散角可以使对应的错误概率达到最小;在一定错误概率要求下,选择最佳束散角可以使对应的信息传输率达到最大,对于最佳束散角的具体确定方法,可以参考相关现有技术,此处不再赘述。In order to reduce the coarse tracking error, a fifth sub-compensation scheme based on the coarse tracking error compensation technology can be used to determine the optimal beam divergence angle based on the coarse tracking error compensation technology. When the information transmission rate is constant, the error probability gradually increases with the increase of the link distance, the error probability gradually increases with the increase of the tracking error angle jitter variance, and the error probability gradually decreases with the increase of the transmit power. , the selection of the optimal beam divergence angle can minimize the corresponding error probability; under a certain error probability requirement, the selection of the optimal beam divergence angle can maximize the corresponding information transmission rate; under a certain information transmission rate, select the most The optimal beam divergence angle can minimize the corresponding error probability; under a certain error probability requirement, selecting the optimal beam divergence angle can maximize the corresponding information transmission rate. For the specific determination method of the optimal beam divergence angle, you can refer to the relevant The prior art is not repeated here.

为了降低光束瞄准偏差,可以使用基于光束瞄准偏差补偿技术的第六子补偿方案:具体的,在已知发射端卫星和接收端卫星的轨道运动模型的基础上,根据瞄准角预测算法预测两个卫星之间的瞄准角,由于耦合运动将使目标卫星的位置偏离预测位置,产生瞄准偏差,为补偿耦合运动带来的瞄准偏差,可以修正二维转台的转角,从而完成瞄准过程中由于耦合运动导致的瞄准偏差的补偿。In order to reduce the beam aiming deviation, the sixth sub-compensation scheme based on the beam aiming deviation compensation technology can be used: Specifically, on the basis of the known orbital motion models of the transmitting-end satellite and the receiving-end satellite, the aiming angle prediction algorithm predicts two The aiming angle between satellites, due to the coupling motion will make the position of the target satellite deviate from the predicted position, resulting in aiming deviation. In order to compensate for the aiming deviation caused by the coupling motion, the rotation angle of the two-dimensional turntable can be corrected, so as to complete the aiming process due to the coupling motion. Compensation for the resulting aiming bias.

进一步的,与星地下行链路对应的子补偿方案包括:上述第一子补偿方案、上述第二子补偿方案、上述第三子补偿方案以及上述第四子补偿方案。Further, the sub-compensation scheme corresponding to the satellite-ground downlink includes: the above-mentioned first sub-compensation scheme, the above-mentioned second sub-compensation scheme, the above-mentioned third sub-compensation scheme, and the above-mentioned fourth sub-compensation scheme.

由于在星地下行链路中,发射端为卫星,因此,发射功率并不是无限的,在调整时需要考虑卫星发射功率的上限。因此,针对上述第三子补偿方案,在星地下行链路中,可以使用第二功率子补偿方案进行功率补偿。具体的:地面用户接收端对接收到的卫星信号进行SINR测量估计,根据功率控制算法产生对应的量化功率控制指令TPC,并将相应的TPC按照一定的数据格式与基带数据组帧调制;进而,通过上行链路传输到卫星,卫星对接收的调制信号进行解调还原得到基带数据,并按照通信协议所规定的数据帧格式提取出相应的功控指令TPC,根据指令产生相应的增益调节量,进而对下行链路调制信号的发射功率进行相应的调整,由于卫星端发射功率不是无限的,因此在调整时需要考虑发射功率有上限。Since in the satellite-to-ground downlink, the transmitter is a satellite, so the transmit power is not infinite, and the upper limit of the satellite transmit power needs to be considered when adjusting. Therefore, for the above-mentioned third sub-compensation scheme, in the satellite-ground downlink, the second power sub-compensation scheme can be used to perform power compensation. Specifically: the ground user receiving end performs SINR measurement and estimation on the received satellite signal, generates a corresponding quantized power control command TPC according to a power control algorithm, and modulates the corresponding TPC with baseband data in a frame according to a certain data format; further, Through the uplink transmission to the satellite, the satellite demodulates and restores the received modulated signal to obtain baseband data, and extracts the corresponding power control command TPC according to the data frame format specified by the communication protocol, and generates the corresponding gain adjustment amount according to the command. Then, the transmit power of the downlink modulated signal is adjusted accordingly. Since the transmit power of the satellite terminal is not infinite, it is necessary to consider the upper limit of the transmit power when adjusting.

综上,若当前通信任务的任务类型为第一任务类型、第二任务类型或者第三任务类型中的任一任务类型,其涉及的各传输链路分别为:星地上行链路、星间链路以及星地下行链路。此时,可以确定出总体补偿方案为:在星地上行链路阶段,同时采用上述第一子补偿方案、第二子补偿方案、第三子补偿方案以及第四子补偿方案进行通信补偿,其中,第三子补偿方案具体为第一功率子补偿方案;在星间链路阶段,同时采用上述第五子补偿方案和上述第六子补偿方案进行通信补偿;在星地下行链路阶段,同时采用上述第一子补偿方案、上述第二子补偿方案、上述第三子补偿方案以及上述第四子补偿方案进行通信补偿,其中,第三子补偿方案具体为第二功率子补偿方案。To sum up, if the task type of the current communication task is any one of the first task type, the second task type or the third task type, the transmission links involved are: satellite-ground uplink, inter-satellite link and satellite-to-ground downlink. At this time, it can be determined that the overall compensation scheme is: in the satellite-ground uplink phase, the above-mentioned first sub-compensation scheme, second sub-compensation scheme, third sub-compensation scheme and fourth sub-compensation scheme are used for communication compensation, wherein , the third sub-compensation scheme is specifically the first power sub-compensation scheme; in the inter-satellite link stage, the above fifth sub-compensation scheme and the above sixth sub-compensation scheme are used for communication compensation; in the satellite-ground downlink stage, simultaneously The communication compensation is performed using the first sub-compensation scheme, the second sub-compensation scheme, the third sub-compensation scheme, and the fourth sub-compensation scheme, wherein the third sub-compensation scheme is specifically the second power sub-compensation scheme.

若当前通信任务的任务类型为第四任务类型,其涉及的各传输链路分别为:星间链路和星地下行链路。此时,可以确定出总体补偿方案为:在星间链路阶段,同时采用上述第五子补偿方案和上述第六子补偿方案进行通信补偿;在星地下行链路阶段,同时采用上述第一子补偿方案、上述第二子补偿方案、上述第三子补偿方案以及上述第四子补偿方案进行通信补偿,其中,第三子补偿方案具体为第二功率子补偿方案。If the task type of the current communication task is the fourth task type, the respective transmission links involved are: an inter-satellite link and a satellite-ground downlink. At this time, it can be determined that the overall compensation scheme is: in the inter-satellite link phase, the fifth sub-compensation scheme and the sixth sub-compensation scheme above are used for communication compensation; in the satellite-ground downlink phase, the first sub-compensation scheme above is used simultaneously. The sub-compensation scheme, the second sub-compensation scheme, the third sub-compensation scheme, and the fourth sub-compensation scheme perform communication compensation, wherein the third sub-compensation scheme is specifically the second power sub-compensation scheme.

若当前通信任务的任务类型为第五任务类型,其涉及的各传输链路则为:星地下行链路。此时,可以确定出总体补偿方案为:在星地下行链路阶段,同时采用上述第一子补偿方案、上述第二子补偿方案、上述第三子补偿方案以及上述第四子补偿方案进行通信补偿,其中,第三子补偿方案具体为第二功率子补偿方案。If the task type of the current communication task is the fifth task type, each transmission link involved is: satellite-ground downlink. At this time, it can be determined that the overall compensation scheme is: in the satellite-ground downlink phase, the above-mentioned first sub-compensation scheme, the above-mentioned second sub-compensation scheme, the above-mentioned third sub-compensation scheme, and the above-mentioned fourth sub-compensation scheme are simultaneously used for communication. compensation, wherein the third sub-compensation scheme is specifically the second power sub-compensation scheme.

基于同一发明构思,根据本发明上述实施例提供的面向多任务的卫星通信网络自适应补偿方法,相应地,本发明实施例还提供了一种面向多任务的卫星通信网络自适应补偿装置,该装置的结构示意图如图3所示,包括:Based on the same inventive concept, according to the multi-task-oriented satellite communication network adaptive compensation method provided by the above-mentioned embodiments of the present invention, correspondingly, the present invention also provides a multi-task-oriented satellite communication network adaptive compensation device, which The schematic structural diagram of the device is shown in Figure 3, including:

任务类型获取模块301,用于获取当前通信任务的任务类型;A task type acquisition module 301, for acquiring the task type of the current communication task;

总体补偿方案确定模块302,用于根据任务类型,确定总体补偿方案;其中,总体补偿方案包括:与当前通信任务中涉及的各传输链路分别对应的子补偿方案;各传输链路为激光链路或者微波链路;The overall compensation scheme determination module 302 is configured to determine the overall compensation scheme according to the task type; wherein, the overall compensation scheme includes: sub-compensation schemes corresponding to each transmission link involved in the current communication task; each transmission link is a laser chain road or microwave link;

通信补偿模块303,用于通信过程中,分别在各传输链路阶段,采用与各传输链路对应的子补偿方案进行通信补偿。The communication compensation module 303 is used to perform communication compensation in each transmission link stage by adopting the sub-compensation scheme corresponding to each transmission link in the communication process.

进一步的,任务类型包括:第一任务类型、第二任务类型、第三任务类型、第四任务类型以及第五任务类型;Further, the task types include: a first task type, a second task type, a third task type, a fourth task type, and a fifth task type;

第一任务类型为:第一地面用户通过卫星通信网络中的低地球轨道LEO卫星或者中地球轨道MEO卫星接入地球同步轨道GEO卫星,并通过GEO卫星向第二地面用户发送数据的任务类型;The first task type is: a task type in which the first ground user accesses the geosynchronous orbit GEO satellite through a low earth orbit LEO satellite or a medium earth orbit MEO satellite in the satellite communication network, and sends data to the second ground user through the GEO satellite;

第二任务类型为:第三地面用户通过LEO卫星或者MEO卫星向第四地面用户发送数据的任务类型;The second task type is: the task type in which the third ground user sends data to the fourth ground user through the LEO satellite or the MEO satellite;

第三任务类型为:第五地面用户通过GEO卫星向第六地面用户发送数据的任务类型;The third task type is: the task type in which the fifth ground user sends data to the sixth ground user through the GEO satellite;

第四任务类型为:GEO卫星通过LEO卫星或者MEO卫星向第七地面用户发送数据的任务类型;The fourth task type is: the task type in which the GEO satellite sends data to the seventh ground user through the LEO satellite or the MEO satellite;

第五任务类型为:GEO卫星直接向第八地面用户发送数据的任务类型;The fifth task type is: the task type in which the GEO satellite directly sends data to the eighth ground user;

若当前通信任务的任务类型为第一任务类型、第二任务类型或者第三任务类型中的任一任务类型,当前通信任务中涉及的各传输链路分别为:星地上行链路、星间链路以及星地下行链路;If the task type of the current communication task is any one of the first task type, the second task type or the third task type, the transmission links involved in the current communication task are: satellite-ground uplink, inter-satellite link and satellite-to-ground downlink;

若当前通信任务的任务类型为第四任务类型,当前通信任务中涉及的各传输链路分别为:星间链路和星地下行链路;If the task type of the current communication task is the fourth task type, the transmission links involved in the current communication task are: inter-satellite link and satellite-ground downlink;

若当前通信任务的任务类型为第五任务类型,当前通信任务中涉及的传输链路为:星地下行链路。If the task type of the current communication task is the fifth task type, the transmission link involved in the current communication task is: satellite-ground downlink.

进一步的,与星地上行链路对应的子补偿方案包括:基于自适应编码技术的第一子补偿方案、基于概率整形技术的第二子补偿方案、基于功率自适应控制技术的第三子补偿方案以及基于激光光束瞄准角补偿技术的第四子补偿方案;Further, the sub-compensation scheme corresponding to the satellite-ground uplink includes: a first sub-compensation scheme based on adaptive coding technology, a second sub-compensation scheme based on probability shaping technology, and a third sub-compensation scheme based on power adaptive control technology. scheme and the fourth sub-compensation scheme based on laser beam aiming angle compensation technology;

与星间链路对应的子补偿方案包括:基于粗跟踪误差补偿技术的第五子补偿方案和基于光束瞄准偏差补偿技术的第六子补偿方案;The sub-compensation schemes corresponding to the inter-satellite link include: the fifth sub-compensation scheme based on the coarse tracking error compensation technology and the sixth sub-compensation scheme based on the beam aiming deviation compensation technology;

与星地下行链路对应的子补偿方案包括:第一子补偿方案、第二子补偿方案、第三子补偿方案以及第四子补偿方案。The sub-compensation schemes corresponding to the satellite-ground downlink include: a first sub-compensation scheme, a second sub-compensation scheme, a third sub-compensation scheme, and a fourth sub-compensation scheme.

进一步的,第三子补偿方案包括:第一功率子补偿方案和第二功率子补偿方案;其中,第一功率子补偿方案中不存在功率补偿上限;第二功率子补偿方案中存在功率补偿上限;Further, the third sub-compensation scheme includes: a first power sub-compensation scheme and a second power sub-compensation scheme; wherein, there is no power compensation upper limit in the first power sub-compensation scheme; and a power compensation upper limit exists in the second power sub-compensation scheme ;

与星地上行链路对应的第三子补偿方案为第一功率子补偿方案;The third sub-compensation scheme corresponding to the satellite-ground uplink is the first power sub-compensation scheme;

与星地下行链路对应的第三子补偿方案为第二功率子补偿方案。The third sub-compensation scheme corresponding to the satellite-ground downlink is the second power sub-compensation scheme.

图3所示实施例中,根据当前通信任务的任务类型,确定出与当前通信任务中涉及的各传输链路分别对应的子补偿方案,并在各传输链路阶段,分别采用对应的子补偿方案进行通信补偿,因此,提高了网络传输的性能。In the embodiment shown in FIG. 3 , according to the task type of the current communication task, a sub-compensation scheme corresponding to each transmission link involved in the current communication task is determined, and in each transmission link stage, the corresponding sub-compensation scheme is adopted respectively. The scheme performs communication compensation, therefore, improving the performance of network transmission.

本发明实施例还提供了一种电子设备,如图4所示,包括处理器401、通信接口402、存储器403和通信总线404,其中,处理器401,通信接口402,存储器403通过通信总线404完成相互间的通信,An embodiment of the present invention further provides an electronic device, as shown in FIG. 4 , including a processor 401 , a communication interface 402 , a memory 403 and a communication bus 404 , wherein the processor 401 , the communication interface 402 , and the memory 403 pass through the communication bus 404 complete communication with each other,

存储器403,用于存放计算机程序;a memory 403 for storing computer programs;

处理器401,用于执行存储器403上所存放的程序时,实现如下步骤:When the processor 401 is used to execute the program stored in the memory 403, the following steps are implemented:

获取当前通信任务的任务类型;Get the task type of the current communication task;

根据任务类型,确定总体补偿方案;其中,总体补偿方案包括:与当前通信任务中涉及的各传输链路分别对应的子补偿方案;各传输链路为激光链路或者微波链路;Determine the overall compensation scheme according to the task type; wherein, the overall compensation scheme includes: sub-compensation schemes corresponding to each transmission link involved in the current communication task; each transmission link is a laser link or a microwave link;

通信过程中,分别在各传输链路阶段,采用与各传输链路对应的子补偿方案进行通信补偿。During the communication process, at each transmission link stage, the sub-compensation scheme corresponding to each transmission link is used to perform communication compensation.

进一步的,还可以包括本发明实施例提供的上述面向多任务的卫星通信网络自适应补偿方法中的其他处理流程,在此不再进行详细描述。Further, other processing procedures in the above-mentioned multi-task-oriented satellite communication network adaptive compensation method provided in the embodiment of the present invention may also be included, which will not be described in detail here.

上述被电子设备提到的通信总线可以是外设部件互连标准(PeripheralComponent Interconnect,简称PCI)总线或扩展工业标准结构(Extended IndustryStandard Architecture,简称EISA)总线等。该通信总线可以分为地址总线、数据总线、控制总线等。为便于表示,图中仅用一条粗线表示,但并不表示仅有一根总线或一种类型的总线。The communication bus mentioned above by the electronic device may be a Peripheral Component Interconnect (PCI for short) bus or an Extended Industry Standard Architecture (Extended Industry Standard Architecture, EISA for short) bus or the like. The communication bus can be divided into an address bus, a data bus, a control bus, and the like. For ease of presentation, only one thick line is used in the figure, but it does not mean that there is only one bus or one type of bus.

通信接口用于上述电子设备与其他设备之间的通信。The communication interface is used for communication between the above electronic device and other devices.

存储器可以包括随机存取存储器(Random Access Memory,简称RAM),也可以包括非易失性存储器(non-volatile memory),例如至少一个磁盘存储器。可选的,存储器还可以是至少一个位于远离前述处理器的存储装置。The memory may include random access memory (Random Access Memory, RAM for short), and may also include non-volatile memory (non-volatile memory), such as at least one disk memory. Optionally, the memory may also be at least one storage device located away from the aforementioned processor.

上述的处理器可以是通用处理器,包括中央处理器(Central Processing Unit,简称CPU)、网络处理器(Network Processor,简称NP)等;还可以是数字信号处理器(Digital Signal Processing,简称DSP)、专用集成电路(Application SpecificIntegrated Circuit,简称ASIC)、现场可编程门阵列(Field-Programmable Gate Array,简称FPGA)或者其他可编程逻辑器件、分立门或者晶体管逻辑器件、分立硬件组件。The above-mentioned processor may be a general-purpose processor, including a central processing unit (Central Processing Unit, referred to as CPU), a network processor (Network Processor, referred to as NP), etc.; may also be a digital signal processor (Digital Signal Processing, referred to as DSP) , Application Specific Integrated Circuit (ASIC for short), Field-Programmable Gate Array (FPGA for short) or other programmable logic devices, discrete gate or transistor logic devices, and discrete hardware components.

在本发明提供的又一实施例中,还提供了一种计算机可读存储介质,该计算机可读存储介质中存储有指令,当其在计算机上运行时,使得计算机执行上述实施例中任一所述的面向多任务的卫星通信网络自适应补偿方法。In yet another embodiment provided by the present invention, a computer-readable storage medium is also provided, where instructions are stored in the computer-readable storage medium, when the computer-readable storage medium is run on a computer, the computer is made to execute any one of the above-mentioned embodiments. The multi-task-oriented satellite communication network adaptive compensation method.

在本发明提供的又一实施例中,还提供了一种包含指令的计算机程序产品,当其在计算机上运行时,使得计算机执行上述实施例中任一所述的面向多任务的卫星通信网络自适应补偿方法。In yet another embodiment provided by the present invention, there is also provided a computer program product containing instructions, which, when run on a computer, enables the computer to execute the multitasking-oriented satellite communication network described in any of the foregoing embodiments Adaptive compensation method.

在上述实施例中,可以全部或部分地通过软件、硬件、固件或者其任意组合来实现。当使用软件实现时,可以全部或部分地以计算机程序产品的形式实现。所述计算机程序产品包括一个或多个计算机指令。在计算机上加载和执行所述计算机程序指令时,全部或部分地产生按照本发明实施例所述的流程或功能。所述计算机可以是通用计算机、专用计算机、计算机网络、或者其他可编程装置。所述计算机指令可以存储在计算机可读存储介质中,或者从一个计算机可读存储介质向另一个计算机可读存储介质传输,例如,所述计算机指令可以从一个网站站点、计算机、服务器或数据中心通过有线(例如同轴电缆、光纤、数字用户线(DSL))或无线(例如红外、无线、微波等)方式向另一个网站站点、计算机、服务器或数据中心进行传输。所述计算机可读存储介质可以是计算机能够存取的任何可用介质或者是包含一个或多个可用介质集成的服务器、数据中心等数据存储设备。所述可用介质可以是磁性介质,(例如,软盘、硬盘、磁带)、光介质(例如,DVD)、或者半导体介质(例如固态硬盘Solid State Disk(SSD))等。In the above-mentioned embodiments, it may be implemented in whole or in part by software, hardware, firmware or any combination thereof. When implemented in software, it can be implemented in whole or in part in the form of a computer program product. The computer program product includes one or more computer instructions. When the computer program instructions are loaded and executed on a computer, all or part of the processes or functions described in the embodiments of the present invention are generated. The computer may be a general purpose computer, special purpose computer, computer network, or other programmable device. The computer instructions may be stored in or transmitted from one computer readable storage medium to another computer readable storage medium, for example, the computer instructions may be downloaded from a website site, computer, server or data center Transmission to another website site, computer, server, or data center is by wire (eg, coaxial cable, fiber optic, digital subscriber line (DSL)) or wireless (eg, infrared, wireless, microwave, etc.). The computer-readable storage medium may be any available medium that can be accessed by a computer or a data storage device such as a server, data center, etc. that includes an integration of one or more available media. The usable media may be magnetic media (eg, floppy disks, hard disks, magnetic tapes), optical media (eg, DVDs), or semiconductor media (eg, Solid State Disk (SSD)), among others.

需要说明的是,在本文中,诸如第一和第二等之类的关系术语仅仅用来将一个实体或者操作与另一个实体或操作区分开来,而不一定要求或者暗示这些实体或操作之间存在任何这种实际的关系或者顺序。而且,术语“包括”、“包含”或者其任何其他变体意在涵盖非排他性的包含,从而使得包括一系列要素的过程、方法、物品或者设备不仅包括那些要素,而且还包括没有明确列出的其他要素,或者是还包括为这种过程、方法、物品或者设备所固有的要素。在没有更多限制的情况下,由语句“包括一个……”限定的要素,并不排除在包括所述要素的过程、方法、物品或者设备中还存在另外的相同要素。It should be noted that, in this document, relational terms such as first and second are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any relationship between these entities or operations. any such actual relationship or sequence exists. Moreover, the terms "comprising", "comprising" or any other variation thereof are intended to encompass a non-exclusive inclusion such that a process, method, article or device that includes a list of elements includes not only those elements, but also includes not explicitly listed or other elements inherent to such a process, method, article or apparatus. Without further limitation, an element qualified by the phrase "comprising a..." does not preclude the presence of additional identical elements in a process, method, article or apparatus that includes the element.

本说明书中的各个实施例均采用相关的方式描述,各个实施例之间相同相似的部分互相参见即可,每个实施例重点说明的都是与其他实施例的不同之处。尤其,对于装置、设备及存储介质实施例而言,由于其基本相似于方法实施例,所以描述的比较简单,相关之处参见方法实施例的部分说明即可。Each embodiment in this specification is described in a related manner, and the same and similar parts between the various embodiments may be referred to each other, and each embodiment focuses on the differences from other embodiments. In particular, for the apparatus, device, and storage medium embodiments, since they are basically similar to the method embodiments, the description is relatively simple, and reference may be made to some descriptions of the method embodiments for related parts.

以上所述仅为本发明的较佳实施例而已,并非用于限定本发明的保护范围。凡在本发明的精神和原则之内所作的任何修改、等同替换、改进等,均包含在本发明的保护范围内。The above descriptions are only preferred embodiments of the present invention, and are not intended to limit the protection scope of the present invention. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present invention are included in the protection scope of the present invention.

Claims (6)

1. A multitask-oriented satellite communication network adaptive compensation method is characterized by comprising the following steps:
acquiring a task type of a current communication task;
determining an overall compensation scheme according to the task type; wherein the overall compensation scheme comprises: sub-compensation schemes respectively corresponding to the transmission links involved in the current communication task; each transmission link is a satellite uplink, an inter-satellite link and a satellite downlink;
in the communication process, in each transmission link stage, a sub-compensation scheme corresponding to each transmission link is adopted for communication compensation;
the task types include: a first task type, a second task type, a third task type, a fourth task type, and a fifth task type;
the first task type is: a first ground user accesses a geosynchronous orbit GEO satellite through a low earth orbit LEO satellite or a medium earth orbit MEO satellite in the satellite communication network and sends a task type of data to a second ground user through the GEO satellite;
the second task type is: the task type of data sent by the third ground user to the fourth ground user through the LEO satellite or the MEO satellite;
the third task type is: the task type of the data sent by the fifth ground user to the sixth ground user through the GEO satellite;
the fourth task type is: the GEO satellite sends the task type of data to a seventh ground user through the LEO satellite or the MEO satellite;
the fifth task type is: the GEO satellite directly sends the task type of the data to an eighth ground user;
when the task type of the current communication task is any one of the first task type, the second task type, or the third task type, the transmission links involved in the current communication task are respectively: an above-satellite uplink, an inter-satellite link, and an above-satellite downlink;
when the task type of the current communication task is the fourth task type, the transmission links involved in the current communication task are respectively: an inter-satellite link and a satellite-to-ground downlink;
when the task type of the current communication task is the fifth task type, a transmission link involved in the current communication task is: a satellite-to-ground downlink;
the sub-compensation scheme corresponding to the satellite uplink comprises the following steps: a first sub-compensation scheme based on an adaptive coding technology, a second sub-compensation scheme based on a probability shaping technology, a third sub-compensation scheme based on a power adaptive control technology and a fourth sub-compensation scheme based on a laser beam aiming angle compensation technology;
the sub-compensation scheme corresponding to the inter-satellite link comprises the following steps: a fifth sub-compensation scheme based on a coarse tracking error compensation technique and a sixth sub-compensation scheme based on a beam aiming deviation compensation technique;
the sub-compensation scheme corresponding to the satellite-to-ground downlink comprises: the first sub-compensation scheme, the second sub-compensation scheme, the third sub-compensation scheme, and the fourth sub-compensation scheme.
2. The method of claim 1,
the third sub-compensation scheme comprises: a first power sub-compensation scheme and a second power sub-compensation scheme; wherein there is no upper limit of power compensation in the first power sub-compensation scheme; a power compensation upper limit exists in the second power sub-compensation scheme;
the third sub-compensation scheme corresponding to the uplink-to-satellite link is the first power sub-compensation scheme;
the third sub-compensation scheme corresponding to the satellite-to-ground downlink is the second power sub-compensation scheme.
3. A multitasking-oriented adaptive compensation device for a satellite communication network, comprising:
the task type acquisition module is used for acquiring the task type of the current communication task;
the overall compensation scheme determining module is used for determining an overall compensation scheme according to the task type; wherein the overall compensation scheme comprises: sub-compensation schemes respectively corresponding to the transmission links involved in the current communication task; each transmission link is a satellite uplink, an inter-satellite link and a satellite downlink;
the communication compensation module is used for performing communication compensation by adopting a sub-compensation scheme corresponding to each transmission link at each transmission link stage in the communication process;
the task types include: a first task type, a second task type, a third task type, a fourth task type, and a fifth task type;
the first task type is: a first ground user accesses a geosynchronous orbit GEO satellite through a low earth orbit LEO satellite or a medium earth orbit MEO satellite in the satellite communication network and sends a task type of data to a second ground user through the GEO satellite;
the second task type is: the task type of data sent by the third ground user to the fourth ground user through the LEO satellite or the MEO satellite;
the third task type is: the task type of the data sent by the fifth ground user to the sixth ground user through the GEO satellite;
the fourth task type is: the GEO satellite sends the task type of data to a seventh ground user through the LEO satellite or the MEO satellite;
the fifth task type is: the GEO satellite directly sends the task type of the data to an eighth ground user;
when the task type of the current communication task is any one of the first task type, the second task type, or the third task type, the transmission links involved in the current communication task are respectively: an above-satellite uplink, an inter-satellite link, and an above-satellite downlink;
when the task type of the current communication task is the fourth task type, the transmission links involved in the current communication task are respectively: an inter-satellite link and a satellite-to-ground downlink;
when the task type of the current communication task is the fifth task type, a transmission link involved in the current communication task is: a satellite-to-ground downlink;
the sub-compensation scheme corresponding to the satellite uplink comprises the following steps: a first sub-compensation scheme based on an adaptive coding technology, a second sub-compensation scheme based on a probability shaping technology, a third sub-compensation scheme based on a power adaptive control technology and a fourth sub-compensation scheme based on a laser beam aiming angle compensation technology;
the sub-compensation scheme corresponding to the inter-satellite link comprises the following steps: a fifth sub-compensation scheme based on a coarse tracking error compensation technique and a sixth sub-compensation scheme based on a beam aiming deviation compensation technique;
the sub-compensation scheme corresponding to the satellite-to-ground downlink comprises: the first sub-compensation scheme, the second sub-compensation scheme, the third sub-compensation scheme, and the fourth sub-compensation scheme.
4. The apparatus of claim 3, wherein the third sub-compensation scheme comprises: a first power sub-compensation scheme and a second power sub-compensation scheme; wherein there is no upper limit of power compensation in the first power sub-compensation scheme; a power compensation upper limit exists in the second power sub-compensation scheme;
the third sub-compensation scheme corresponding to the uplink-to-satellite link is the first power sub-compensation scheme;
the third sub-compensation scheme corresponding to the satellite-to-ground downlink is the second power sub-compensation scheme.
5. An electronic device is characterized by comprising a processor, a communication interface, a memory and a communication bus, wherein the processor and the communication interface are used for realizing mutual communication by the memory through the communication bus;
a memory for storing a computer program;
a processor for implementing the method steps of any of claims 1-2 when executing a program stored in the memory.
6. A computer-readable storage medium, characterized in that a computer program is stored in the computer-readable storage medium, which computer program, when being executed by a processor, carries out the method steps of any one of the claims 1-2.
CN201911375189.1A 2019-12-27 2019-12-27 Multitask-oriented satellite communication network adaptive compensation method and device Active CN111262615B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201911375189.1A CN111262615B (en) 2019-12-27 2019-12-27 Multitask-oriented satellite communication network adaptive compensation method and device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201911375189.1A CN111262615B (en) 2019-12-27 2019-12-27 Multitask-oriented satellite communication network adaptive compensation method and device

Publications (2)

Publication Number Publication Date
CN111262615A CN111262615A (en) 2020-06-09
CN111262615B true CN111262615B (en) 2020-12-01

Family

ID=70948534

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201911375189.1A Active CN111262615B (en) 2019-12-27 2019-12-27 Multitask-oriented satellite communication network adaptive compensation method and device

Country Status (1)

Country Link
CN (1) CN111262615B (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113824485B (en) * 2020-06-18 2022-09-02 大唐移动通信设备有限公司 Transmission signal compensation method, network side equipment and terminal
CN111970221B (en) * 2020-06-30 2022-06-03 南京信息工程大学 High noise immunity P-bit optical transmission method based on multi-probability distribution
CN113141206B (en) * 2021-04-20 2022-03-22 哈尔滨工业大学(威海) A method and system for adaptive communication between micro-nano constellation inter-satellite links

Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1744457A (en) * 2001-11-16 2006-03-08 Lg电子株式会社 Method for controlling transmission power of hs-scch in mobile communication system
WO2007027383A2 (en) * 2005-08-27 2007-03-08 Trimble Navigation Ltd. Method for augmenting radio positioning system using single fan laser
CN101192897A (en) * 2006-11-22 2008-06-04 上海科集信息技术有限公司 Satellite backward compensation system based on P2P technology
CN101562673A (en) * 2008-04-15 2009-10-21 中国电信股份有限公司 Method and system for asymmetric link compensation in P2P transmission
WO2012109269A1 (en) * 2011-02-08 2012-08-16 Globalstar, Inc. Satellite communication device for routing terrestrial signals through a satellite network
CN103312613A (en) * 2012-03-16 2013-09-18 中兴通讯股份有限公司 Service message forwarding method and device
CN103916177A (en) * 2014-01-23 2014-07-09 北京邮电大学 Building method of communication scheme and interlayer interstellar link based on GEO-IGSO/MEO double-layer satellite network
CN104038298A (en) * 2014-06-12 2014-09-10 北京邮电大学 Satellite network self-adaption joint spectrum sensing method based on link sensing
CN107508659A (en) * 2017-09-15 2017-12-22 哈尔滨工程大学 The adaptive code modulation method passed towards satellite navigation system inter-satellite link number
CN107579845A (en) * 2017-08-20 2018-01-12 西南电子技术研究所(中国电子科技集团公司第十研究所) Spatial information web services architectural framework
US10049104B2 (en) * 2016-11-04 2018-08-14 International Business Machines Corporation Message modifier responsive to meeting location availability
CN108809375A (en) * 2018-04-27 2018-11-13 上海交通大学 The extensive antenna system of low precision based on probability integer and its code modulating method
CN109787687A (en) * 2018-12-28 2019-05-21 长沙天仪空间科技研究院有限公司 A kind of portable receiver based on Intersatellite Optical Communication System

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9436170B2 (en) * 2012-04-16 2016-09-06 Eugenio Minvielle Appliances with weight sensors for nutritional substances
US20180152235A1 (en) * 2016-11-01 2018-05-31 Maxwell A. Smoot Methods and systems using an agile hub and smart connectivity broker for satellite communications
CN110247697B (en) * 2019-05-30 2021-12-07 西安空间无线电技术研究所 Method for improving frequency utilization rate of low-earth-orbit communication satellite system

Patent Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1744457A (en) * 2001-11-16 2006-03-08 Lg电子株式会社 Method for controlling transmission power of hs-scch in mobile communication system
WO2007027383A2 (en) * 2005-08-27 2007-03-08 Trimble Navigation Ltd. Method for augmenting radio positioning system using single fan laser
CN101192897A (en) * 2006-11-22 2008-06-04 上海科集信息技术有限公司 Satellite backward compensation system based on P2P technology
CN101562673A (en) * 2008-04-15 2009-10-21 中国电信股份有限公司 Method and system for asymmetric link compensation in P2P transmission
WO2012109269A1 (en) * 2011-02-08 2012-08-16 Globalstar, Inc. Satellite communication device for routing terrestrial signals through a satellite network
CN103312613A (en) * 2012-03-16 2013-09-18 中兴通讯股份有限公司 Service message forwarding method and device
CN103916177A (en) * 2014-01-23 2014-07-09 北京邮电大学 Building method of communication scheme and interlayer interstellar link based on GEO-IGSO/MEO double-layer satellite network
CN104038298A (en) * 2014-06-12 2014-09-10 北京邮电大学 Satellite network self-adaption joint spectrum sensing method based on link sensing
US10049104B2 (en) * 2016-11-04 2018-08-14 International Business Machines Corporation Message modifier responsive to meeting location availability
CN107579845A (en) * 2017-08-20 2018-01-12 西南电子技术研究所(中国电子科技集团公司第十研究所) Spatial information web services architectural framework
CN107508659A (en) * 2017-09-15 2017-12-22 哈尔滨工程大学 The adaptive code modulation method passed towards satellite navigation system inter-satellite link number
CN108809375A (en) * 2018-04-27 2018-11-13 上海交通大学 The extensive antenna system of low precision based on probability integer and its code modulating method
CN109787687A (en) * 2018-12-28 2019-05-21 长沙天仪空间科技研究院有限公司 A kind of portable receiver based on Intersatellite Optical Communication System

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
Adaptive modulation and coding techniques;Jinhui Huang;《IET Communications》;20161027;第10卷(第16期);第2091-2095页 *
卫星通信跨层资源管理算法研究;张荻;《中国优秀硕士学位论文全文库》;20180415;全文 *

Also Published As

Publication number Publication date
CN111262615A (en) 2020-06-09

Similar Documents

Publication Publication Date Title
CN111262615B (en) Multitask-oriented satellite communication network adaptive compensation method and device
JP5724031B2 (en) Method for decoding an optical data signal
US8942257B2 (en) Wireless network using feedback of side information and communication method using network coding
US8674758B2 (en) Method and apparatus for improved high order modulation
JP2001156711A (en) Wireless communication device and transmission power control method
JP2022507567A (en) Shifting in the sky wave system
JP2022507569A (en) Low-latency channel equalization using secondary channels
CN117595917B (en) Method, device and equipment for adjusting hybrid automatic repeat request (HARQ) parameters in network transmission of Network Technology (NTN)
JP5289672B2 (en) Method and apparatus for generating a channel estimate using a non-pilot portion of a signal
Kumar et al. Performance enhancement of multi channel multi beam FSO communication link with the application of Reed Solomon codes
CN114745051A (en) A control method and device for satellite-to-ground laser communication
Schieler et al. Data delivery performance of space-to-ground optical communication systems employing rate-constrained feedback protocols
US20240146500A1 (en) Method and apparatus for reconfigurable clock data recovery in fading environments
Giambene et al. Satellite forward VDES channel modeling and impact on higher‐layer performance
US9755784B2 (en) Receiver and decoding method thereof
El Moukalafe et al. Communication Optimization Approach for S-Band LEO CubeSat Link Budget
Stanescu et al. An Overview of Satellite Link Budget Sensitivity Based on Digital Modulation Schemes in Multi-Orbit Satellite Networks.
JP6891899B2 (en) Optical receiver and control method
CN107147434B (en) A MIMO transmit diversity method based on LDPC codes
Cheung End-to-end space system: Engineering considerations
Cheung et al. Link analysis for space communication links using ARQ protocol
US20250219876A1 (en) Receiver for adjusting log likelihood ratio and method of operating the same
Takenaka et al. Low-density generator matrix code for correcting errors with a small optical transponder
Dubey et al. Optimization of LDPC-coded power series MIMO/FSO link with hybrid-SIM based on machine learning in satellite downlink for 5G and beyond applications
US12009896B2 (en) System and method for improving connection stability via deceptive signal quality transmissions

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