CN112332903A - Congestion control method, device, terminal and medium for satellite link - Google Patents
Congestion control method, device, terminal and medium for satellite link Download PDFInfo
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Abstract
The application discloses a congestion control method, a congestion control device, a congestion control terminal and a congestion control medium for a satellite link. The method comprises the following steps: obtaining a Round Trip Time (RTT) value to be processed of a packet sent by a sending end in a satellite link; calculating a new gain coefficient of the satellite link based on the RTT value of the round trip time to be processed; determining a new transmission rate aiming at the transmitting end according to the new gain coefficient; and controlling the sending end to carry out data transmission processing according to the new sending rate so as to avoid the satellite link from being congested. The sending rate of the sending end meets the requirement of the satellite link, network congestion occurs as little as possible, the data packet is smoothly transmitted to the destination address, the problem that the satellite link is congested due to the fact that the sending rate of the sending end does not meet the requirement of the satellite link is avoided, the purpose of congestion control over the satellite link is achieved, and the efficiency of data transmission of the long-delay satellite link is improved.
Description
Technical Field
The present application relates to the field of communications technologies, and in particular, to a method, an apparatus, a terminal, and a medium for controlling congestion of a satellite link.
Background
Compared with a ground communication network, the satellite communication can ensure fast and stable data link transmission, the satellite link is also developed to a high-throughput stage at present, and the satellite communication is recently used as one of key support technologies of 5G backhaul at present. In the development stage of a high-flux satellite communication system, the long fertilizer pipeline effect caused by high delay and high bandwidth is more serious, and the problems are as follows: firstly, link utilization rate is low or even the link is unavailable under a serious condition; and secondly, the high-orbit satellite has the characteristics of long time delay, high error rate and link asymmetry.
In the related art, a tcp (transmission Control protocol) transmission protocol designed based on a ground network is generally used to Control congestion of a satellite communication link. Because the standard for judging congestion by the TCP protocol is that packet loss is called packet loss congestion, and a high error rate in a satellite link can cause misjudgment of the TCP protocol applied in a satellite communication link, the current satellite link congestion control algorithm has the following problems: the problem that a satellite communication link with a TCP protocol is low in transmission efficiency due to multiple data retransmission is solved; secondly, due to the high time delay characteristic of the satellite link, the ground terminal can receive the ACK acknowledgement only after sending data, which results in low utilization rate of the communication link due to the slow start phase in the satellite link for a long time.
Disclosure of Invention
In order to solve the technical problem of low utilization rate of the communication link, the application provides a method, a device, a terminal and a medium for controlling congestion of a satellite link.
According to a first aspect of the present application, there is provided a congestion control method for a satellite link, the method comprising:
obtaining a Round Trip Time (RTT) value to be processed of a packet sent by a sending end in a satellite link;
calculating a new gain coefficient of the satellite link based on the RTT value of the round trip time to be processed;
determining a new transmission rate aiming at the transmitting end according to the new gain coefficient;
and controlling the sending end to carry out data transmission processing according to the new sending rate so as to realize congestion control on the satellite link.
According to a second aspect of the present application, there is provided a congestion control apparatus for a satellite link, the apparatus comprising:
the time delay detection module is used for acquiring a round trip time RTT value to be processed, which is sent out by a sending end in a satellite link;
the gain calculation module is used for calculating a new gain coefficient of the satellite link based on the RTT value of the round trip time to be processed;
the rate calculation module is used for determining a new sending rate aiming at the sending end according to the new gain coefficient;
and the congestion control module is used for controlling the sending end to carry out data transmission processing according to the new sending rate so as to realize congestion control on the satellite link.
According to a third aspect of the present application, there is provided a terminal comprising: a memory, a processor and a computer program stored on the memory and executable on the processor, the processor when executing the computer program to implement the congestion control method for a satellite link as described above.
According to a fourth aspect of the present application, there is provided a computer-readable storage medium storing computer-executable instructions for performing the above-described method of congestion control of a satellite link.
The embodiment of the application calculates the new gain coefficient of the satellite link by acquiring the RTT value of the round trip time to be processed of the satellite link and based on the RTT value of the round trip time to be processed, determining a new sending rate aiming at the sending end according to the new gain coefficient, controlling the sending end to carry out data transmission processing according to the new sending rate, the way of the RTT value of the round trip time to be processed through the satellite link plays a role in adjusting the gain coefficient of the satellite link in real time through the RTT value, therefore, the effect of adjusting the sending rate of the sending end is achieved, the packet sending speed of the sending end is not higher than the packet receiving capacity of the receiving end, the network congestion phenomenon is generated as little as possible, the data packet is smoothly transmitted to the destination address, the problem that the satellite link is congested due to the fact that the sending rate of the sending end does not meet the requirement of the satellite link is avoided, the purpose of congestion control over the satellite link is achieved, and the data transmission efficiency of the long-delay satellite link is improved.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present application, the drawings used in the description of the embodiments of the present application will be briefly described below.
Fig. 1 is a schematic flowchart of a congestion control method for a satellite link according to an embodiment of the present disclosure;
fig. 2 is a schematic diagram of an orbital satellite network architecture of a congestion control method for a satellite link according to an embodiment of the present disclosure;
fig. 3 is a schematic diagram illustrating a comparison between delay and throughput of an orbiting satellite network architecture of a congestion control method for a satellite link according to an embodiment of the present disclosure; and
fig. 4 is a block diagram schematically illustrating a block diagram structure of a congestion control device for a satellite link according to an embodiment of the present disclosure.
Detailed Description
In order to make the objects, technical solutions and advantages of the present application more apparent, the present application is described in further detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the present application and are not intended to limit the present application.
It should be noted that although functional blocks are partitioned in a schematic diagram of an apparatus and a logical order is shown in a flowchart, in some cases, the steps shown or described may be performed in a different order than the partitioning of blocks in the apparatus or the order in the flowchart.
The terms referred to in this application will first be introduced and explained:
in the embodiment of the present application, Congestion control (Congestion control) refers to a technique that a station is in the dimension of the whole internet, so that network Congestion occurs as little as possible while all TCP connections in the network share a network channel maximally, and each participant in the network world is fair and efficient.
To make the objects, technical solutions and advantages of the present application more clear, embodiments of the present application will be described in further detail below with reference to the accompanying drawings.
According to an embodiment of the present application, there is provided a method for controlling congestion of a satellite link, as shown in fig. 1, the method includes steps S101 to S104.
Step S101: and obtaining the RTT value of the round trip time to be processed of the packet sent by the sending end in the satellite link.
Specifically, the terminal obtains a to-be-processed round trip time RTT value of a packet sent by a sending end in a satellite link.
In the embodiment of the application, the round trip time RTT value to be processed is used for representing the round trip time from the sending of a data packet to the receiving of an ack to the data packet. Specifically, the RTT may be calculated in a smooth manner.
In an embodiment of the present application, a satellite link is used to characterize a link for information transmission in a satellite communication system, including an originating earth station, an uplink, a satellite transponder, a downlink, and a receiving earth station.
Step S102: and calculating a new gain coefficient of the satellite link based on the RTT value of the round trip time to be processed.
In the embodiment of the present application, the gain factor refers to a parameter that affects the transmission rate of the data packet.
In particular, the new gain factor may be determined according to a preset gain factor algorithm. For example,
step S103: and determining a new sending rate aiming at the sending end according to the new gain coefficient.
In the embodiment of the present application, the new transmission rate is used to characterize the speed of the transmitting end of the satellite link transmitting data.
Step S104: and controlling the sending end to carry out data transmission processing according to the new sending rate so as to realize congestion control on the satellite link.
Specifically, the number of packets transmitted per unit time by the transmitting end is controlled.
The embodiment of the application obtains the RTT value of the round trip time to be processed of a sending end packet in a satellite link, calculates the new gain coefficient of the satellite link based on the RTT value of the round trip time to be processed, determines the new sending rate aiming at the sending end according to the new gain coefficient, and controls the sending end to carry out data transmission processing according to the new sending rate, and the method of adjusting the RTT value of the round trip time to be processed through the satellite link plays a role in adjusting the gain coefficient of the satellite link in real time through the RTT value, thereby achieving the effect of adjusting the sending rate of the sending end, ensuring that the packet sending rate of the sending end does not exceed the packet receiving capacity of a receiving party, causing network congestion as little as possible, smoothly transmitting a data packet to a destination address, avoiding the congestion of the satellite link caused by the sending rate of the sending end not conforming to the requirement of the satellite link, and, the efficiency of data transmission of the long-delay satellite link is improved.
In some embodiments, step S101 further comprises:
step S1011 (not shown in the figure): and acquiring a Round Trip Time (RTT) value to be processed based on a preset measurement period.
In the embodiment of the present application, the measurement period is set to be performed once every 10 seconds. In particular, the measurement period may also be set to other values, as may be required.
Specifically, the condition for executing step S101 may be set, that is, when a preset condition is satisfied, step S1011 is executed. For example, if the preset condition is a stable state of data transmission, the RTT value measurement processing is performed on the satellite link according to a preset measurement period only when it is detected that the transmitting end enters the stable state of data transmission.
In some embodiments, prior to step S1011, the method further comprises: detecting a data transmission state of a transmitting end; step S1011 further includes: if the data transmission state is a stable state of data transmission, detecting the satellite link; and determining the RTT value of the round trip time to be processed according to the detection processing result.
In the embodiment of the present application, the steady state means that the round-trip time from the sending of the data packet to the receiving of the ack is the same for the predetermined number of times or within the preset error range.
According to the embodiment of the application, unnecessary calculation consumption caused by the fact that the RTT value is detected in the non-stable state is avoided through the detection of the stable state, and the follow-up congestion control precision is improved.
In some embodiments, step S102 further comprises:
determining a maximum value of the reference round trip time RTT and a minimum value of the reference round trip time RTT;
calculating a first difference value between the maximum value of the reference round trip time RTT and the minimum value of the reference round trip time RTT;
calculating a second difference value between the maximum value of the reference round trip time RTT and the value of the round trip time RTT to be processed;
determining a new gain factor according to the ratio of the first difference value and the second difference value;
wherein the content of the first and second substances,
the maximum value of the reference round trip time RTT and the minimum value of the reference round trip time RTT are parameters obtained by detecting the satellite link before the round trip time RTT value to be processed is obtained.
Specifically, if the RTT value of the to-be-processed round trip time is obtained by first measurement, the maximum value of the RTT and the minimum value of the RTT are generally preset initial values; if the RTT value of the round trip time to be processed is obtained by the n +1 th measurement, the maximum value of the RTT of the reference round trip time and the minimum value of the RTT of the reference round trip time are obtained by the nth measurement.
Specifically, the maximum value of the reference round trip time RTT and the minimum value of the reference round trip time RTT obtained through previous measurement may be obtained by querying the local cache, so as to calculate the to-be-processed round trip time RTT obtained through the current measurement and the result obtained through the previous measurement.
For example, the gain factor μmay be calculated according to the following formula:
wherein RTTmax is the maximum value monitored in the initial stage of data transmission, RTTmin is the minimum value monitored in the initial stage of data transmission, and r is the maximum value monitored in the initial stage of data transmissionttAnd obtaining the value of the round trip time RTT to be processed for the measurement.
In some embodiments, step S103 further comprises: step S1031 and step S1032 (not shown in the figure),
step S1031: determining the gain coefficient threshold range to which the new gain coefficient belongs;
step S1032: and determining a new sending rate aiming at the sending end according to the rate calculation model corresponding to the gain coefficient threshold range to which the new gain coefficient belongs.
Specifically, a plurality of calculation models corresponding to the gain coefficient threshold ranges may be preset, the gain coefficient threshold range to which the new gain coefficient belongs may be determined by comparing the gain coefficient threshold ranges with the gain coefficient threshold ranges, and the calculation model corresponding to the gain coefficient threshold range to which the new gain coefficient belongs may be calculated to obtain the new transmission rate.
Specifically, the new gain coefficients may be compared with the respective gain coefficient threshold ranges one by one, or the new gain coefficients may be compared with the respective gain coefficient threshold ranges at the same time to determine the gain coefficient threshold range to which the new gain coefficient belongs.
In some embodiments, step S1032 includes at least one of the following sub-steps:
if the new gain coefficient is larger than 1.25, determining a new sending rate of a sending end aiming at the satellite link according to the product of the bandwidth BtlBW of the satellite link, the reference gain coefficient and 1.25;
and if the new gain coefficient is not less than 1 and not more than 1.25, determining a new sending rate aiming at the sending end according to the product of the bandwidth BtlBW of the satellite link, the reference gain coefficient and the new gain coefficient.
Specifically, the new transmission rate pacingRate can be calculated with reference to the formula (1) or (2):
pavingRate＝BtlBw×gain×μ 1≤μ≤1.25
pacingRate＝BtlBw×gain×1.25 μ>1.25；
wherein BtlBw is the bandwidth of the satellite link, and gain is the gain coefficient determined in the last measurement.
For example, if the current measurement is the first measurement, gain is the pre-configured initial gain coefficient; if the measurement is the second measurement, gain is the gain coefficient determined by the first measurement.
In some embodiments, step S104 further comprises:
determining the corresponding relation between the time of satellite link delay and throughput according to the new sending rate;
and controlling the sending end to transmit data based on the corresponding relation.
Specifically, the time interval between two adjacent data packet transmissions is controlled by querying the corresponding relationship, so that all TCP connections in the network share the network channel maximally, network congestion occurs as little as possible, and the data transmission efficiency is improved.
The satellite operating on the geosynchronous orbit satellite and the earth have the same rotation angular velocity and are called as a high orbit satellite, the problem is that the transmission delay is large, the transmission delay from the ground terminal to the orbit satellite changes along with the change of the position of the ground station, and the delay from the satellite to the receiving end on the ground is long. If the non-single-satellite transmission exists in the inter-satellite transmission process, the time delay can be larger, so that the round-trip time delay of data transmission through the orbit satellite reaches half a second, and the problem of satellite link congestion caused by the fact that the sending rate of a sending end is not appropriate under the condition of long time delay of a satellite link is solved. Therefore, the gain coefficient is recalculated by acquiring the RTT value of the satellite link in real time, the sending rate is determined again according to the recalculated gain coefficient, and the problem of congestion of the satellite link caused by large time delay is avoided by controlling the sending end to send the data packet.
Next, the simulation platform is used to simulate the congestion control method for the satellite link provided in the embodiment of the present application.
Firstly, configuring a simulation platform;
and secondly, simulating the congestion control method for the satellite link provided by the embodiment of the application by using a simulation platform.
The configuration of the simulation platform can refer to the following steps, and can be executed according to the following steps:
step one; and expanding a satellite simulation module on the open source network simulation platform, and compiling an orbit satellite operation environment script. When the method is applied, a simulation platform software allinone integrated package and a corresponding compiling dependent environment can be installed in a Linux-ubuntu18.04 system environment, the simulation platform software allinone integrated package enters an allinone folder, a contib directory is accessed, an expanded and written satelite module is added in the directory, data required by testing is input into a data folder, and preset data parameters such as track data are input. The input data parameters mainly comprise a physical channel satellite-channel and a physical-phy part which are suitable for satellite network simulation. The satellite-phy parameter setting involves the design and invocation of several parameter interfaces as follows: the noise problem interface of the beam receiving system calls SatHy GetRxNieseTemperatureDbk (); m _ acifWrtNoiseFactor; m _ ext noisedensitywhz; m _ errormode ═ SatPhyRxCarrierConf. Wherein params.m _ error model of the satellite orbit is SatPhyRxCarrierConf, which indicates the setting of the bit error rate in the channel.
Step two: the following parts are added to a socket.h of a modified network module in an alinone integrated package, so that the method supports the congestion control method for the satellite link provided by the embodiment of the application:
voidSetHandler(void*handler){m_handler＝handler；}
void*GetHandler(){return m_handler；void*m_handler；
and then adding a new congestion control algorithm and a header file thereof under the transmission control protocol folder, and after the addition is finished, modifying the cflags. And then creating a trace folder under the alinone folder for receiving the round-trip delay time and the data record of the congestion window of the ground terminal network equipment.
And then, completing the configuration of the simulation platform.
The steps of simulating the congestion control method for the satellite link provided by the embodiment of the present application by using the simulation platform may be performed according to the following steps:
(1): after the configuration of the simulation platform is completed according to the first step and the second step, a satellite communication scene is deployed on the simulation platform. Specifically, a network simulation node may be set first, and the node represents a ground terminal and a router in a communication link. A left node n0 is created as a ground transmitting terminal, two routing nodes n1 and n2, and a right node n3 is created as a ground receiving terminal. The creating method is NodeContainer Sats; create (4) resulting in an orbiting satellite network architecture as shown in fig. 2, comprising a ground terminal 101, a ground terminal 102, a GEO satellite 200 and a gateway station 300.
(2): after a node of a network topology is established, a physical layer and a satellite link channel are configured, and a bit error rate model SatGeoHelper helper class is set in network equipment;
the specific setting mode of the satellite link parameters is as follows:
PointToPointhelper SatLink; setdeviceattribute ("DataRate", StringValue ("Mbps"); satlink setchannelattattribute ("Delay", StringValue ("ms")), and set satellite transmission Delay and transmission rate.
Setting error codes in the network equipment drive:
SatPhyRxCarrierConf::ErrorModel em(SatPhyRxCarrierConf::EM_AVI)；
Config::SetDefault("ns3::SatUtHelper::FwdLinkErrorModel",EnumValue(em))；
Config::SetDefault("ns3::SatGwHelper::RtnLinkErrorModel",EnumValue(em))；
and creating an application program transceiving model, setting an OnOff model supported by an open source simulation platform, and setting a destination address and a port for sending by using an OnOffHelper helper class.
TCP data reception is performed using the PacketSink model.
Specifically, the received TCP packets are counted and the throughput is calculated and printed within the TCP protocol. According to the congestion control method for the satellite link provided by the embodiment of the application, the packet sending speed of the ground terminal 101 serving as a sending end does not exceed the packet receiving capacity of the ground terminal 102 serving as a receiving end, and the network congestion phenomenon occurs as less as possible. Specifically, the relationship between throughput and time under different delay conditions calculated by the congestion control method for a satellite link provided in the embodiment of the present application is shown in fig. 3.
According to the method, the satellite simulation module is expanded in the test platform, the satellite simulation model is created according to the method, and the simulation result is output to the trace folder.
In another embodiment of the present application, there is provided a congestion control apparatus for a satellite link, as shown in fig. 4, the apparatus 40 includes: a delay detection module 401, a gain calculation module 402, a rate calculation module 403, and a congestion control module 404.
The time delay detection module 401 is configured to obtain a to-be-processed round trip time RTT value of a packet sent by a sending end in a satellite link;
a gain calculation module 402, configured to calculate a new gain coefficient of the satellite link based on the round trip time RTT value to be processed;
a rate calculating module 403, configured to determine a new sending rate for the sending end according to the new gain factor;
and a congestion control module 404, configured to control the sending end to perform data transmission processing according to the new sending rate, so as to implement congestion control on the satellite link.
The embodiment of the application obtains the value of the Round Trip Time (RTT) to be processed of a sending end packet in a satellite link, calculates the new gain coefficient of the satellite link based on the value of the RTT to be processed, determines the new sending rate aiming at the sending end according to the new gain coefficient, and controls the sending end to carry out data transmission processing according to the new sending rate, and the method plays a role of adjusting the gain coefficient of the satellite link in real time through the RTT value of the round trip time to be processed of the satellite link, thereby achieving the effect of adjusting the sending rate of the sending end, ensuring that the packet sending rate of the sending end does not exceed the packet receiving capacity of a receiving party, causing network congestion as little as possible, smoothly transmitting the data packet to a destination address, avoiding the satellite link from being congested because the sending rate of the sending end does not accord with the requirement of the satellite link, and realizing the purpose of congestion control of the, the efficiency of data transmission of the long-delay satellite link is improved.
Further, the delay detection module comprises:
and the period detection submodule is used for acquiring the RTT value of the satellite link to be processed based on a preset measurement period.
Further, before the step of obtaining the to-be-processed round trip time RTT value of the satellite link based on the preset measurement period, the delay detection module further includes: the sending state detection submodule is used for detecting the data sending state of the sending end; the period detection submodule comprises: the detection execution unit is used for detecting the satellite link if the data transmission state is a stable data transmission state; and the detection value determining unit is used for determining the RTT value of the round trip time to be processed according to the detection processing result.
Further, the gain calculation module includes:
a reference detection value determining submodule for determining a maximum value of a reference round trip time RTT and a minimum value of the reference round trip time RTT;
the first calculation submodule is used for calculating a first difference value between the maximum value of the round trip time RTT and the minimum value of the round trip time RTT;
the second calculation submodule is used for calculating a second difference value between the maximum value of the round trip time RTT and the round trip time RTT value;
the third calculation submodule is used for determining a new gain coefficient according to the ratio of the first difference value to the second difference value;
wherein the content of the first and second substances,
the maximum value of the reference round trip time RTT and the minimum value of the reference round trip time RTT are parameters obtained by detecting the satellite link before the round trip time RTT value to be processed is obtained.
Further, the rate calculation module includes:
the coefficient range determining submodule is used for determining the gain coefficient threshold range to which the new gain coefficient belongs;
and the speed determining submodule is used for determining a new sending speed aiming at the sending end according to the speed calculation model corresponding to the gain coefficient threshold range.
Further, the speed determination submodule includes at least one of the following:
a first determining unit, configured to determine, if the new gain factor is greater than 1.25, a new transmission rate of a transmitting end for the satellite link according to a product of a bandwidth BtlBW of the satellite link, the reference gain factor, and 1.25;
and the second determining unit is used for determining a new sending rate of the sending end aiming at the satellite link according to the product of the bandwidth BtlBW of the satellite link, the reference gain coefficient and the new gain coefficient if the new gain coefficient is not less than 1 and not more than 1.25.
Further, the congestion control module comprises:
the corresponding relation determining submodule is used for determining the corresponding relation between the time of satellite link delay and throughput according to the new sending rate;
and the congestion control submodule is used for controlling the sending end to carry out data transmission processing based on the corresponding relation.
The congestion control device for a satellite link according to this embodiment may execute the congestion control method for a satellite link according to this embodiment, and the implementation principles are similar, and are not described here again.
Another embodiment of the present application provides a terminal, including: a memory, a processor and a computer program stored on the memory and executable on the processor, the processor when executing the computer program to implement the above described method of congestion control of a satellite link.
In particular, the processor may be a CPU, general purpose processor, DSP, ASIC, FPGA or other programmable logic device, transistor logic device, hardware component, or any combination thereof. Which may implement or perform the various illustrative logical blocks, modules, and circuits described in connection with the disclosure. A processor may also be a combination of computing functions, e.g., comprising one or more microprocessors, a DSP and a microprocessor, or the like.
In particular, the processor is coupled to the memory via a bus, which may include a path for communicating information. The bus may be a PCI bus or an EISA bus, etc. The bus may be divided into an address bus, a data bus, a control bus, etc.
The memory may be, but is not limited to, a ROM or other type of static storage device that can store static information and instructions, a RAM or other type of dynamic storage device that can store information and instructions, an EEPROM, a CD-ROM or other optical disk storage, optical disk storage (including compact disk, laser disk, optical disk, digital versatile disk, blu-ray disk, etc.), magnetic disk storage media or other magnetic storage devices, or any other medium that can be used to carry or store desired program code in the form of instructions or data structures and that can be accessed by a computer.
Optionally, the memory is used for storing codes of computer programs for executing the scheme of the application, and the processor is used for controlling the execution. The processor is configured to execute the application program codes stored in the memory to implement the actions of the congestion control device for a satellite link provided by the above-mentioned embodiments.
Yet another embodiment of the present application provides a computer-readable storage medium storing computer-executable instructions for performing the above-mentioned method for congestion control of a satellite link.
The above-described embodiments of the apparatus are merely illustrative, and the units illustrated as separate components may or may not be physically separate, may be located in one place, or may be distributed over a plurality of network units. Some or all of the modules may be selected according to actual needs to achieve the purpose of the solution of the present embodiment.
One of ordinary skill in the art will appreciate that all or some of the steps, systems, and methods disclosed above may be implemented as software, firmware, hardware, and suitable combinations thereof. Some or all of the physical components may be implemented as software executed by a processor, such as a central processing unit, digital signal processor, or microprocessor, or as hardware, or as an integrated circuit, such as an application specific integrated circuit. Such software may be distributed on computer readable media, which may include computer storage media (or non-transitory media) and communication media (or transitory media). The term computer storage media includes volatile and nonvolatile, removable and non-removable media implemented in any method or technology for storage of information such as computer readable instructions, data structures, program modules or other data, as is well known to those of ordinary skill in the art. Computer storage media includes, but is not limited to, RAM, ROM, EEPROM, flash memory or other memory technology, CD-ROM, Digital Versatile Disks (DVD) or other optical disk storage, magnetic cassettes, magnetic tape, magnetic disk storage or other magnetic storage devices, or any other medium which can be used to store the desired information and which can accessed by a computer. In addition, communication media typically embodies computer readable instructions, data structures, program modules or other data in a modulated data signal such as a carrier wave or other transport mechanism and includes any information delivery media as known to those skilled in the art.
While the present invention has been described with reference to the preferred embodiments, it will be understood by those skilled in the art that various changes in form and details may be made therein without departing from the spirit and scope of the invention as defined by the appended claims.
Claims (10)
1. A method for congestion control of a satellite link, comprising:
obtaining a Round Trip Time (RTT) value to be processed of a packet sent by a sending end in a satellite link;
calculating a new gain coefficient of the satellite link based on the RTT value of the round trip time to be processed;
determining a new transmission rate for the transmitting end according to the new gain coefficient;
and controlling the sending end to carry out data transmission processing according to the new sending rate so as to realize congestion control on the satellite link.
2. The method according to claim 1, wherein the step of obtaining the to-be-processed round trip time RTT value of a packet sent from a sending end in the satellite link comprises:
and acquiring the RTT value of the round trip time to be processed based on a preset measurement period.
3. The method of claim 2,
before the step of obtaining the to-be-processed round trip time RTT value based on the preset measurement period, the method further includes:
detecting the data transmission state of the transmitting end;
the step of obtaining the to-be-processed round trip time RTT value based on a preset measurement period includes:
if the data transmission state is a stable data transmission state, detecting the satellite link;
and determining the RTT value of the round trip time to be processed according to the detection processing result.
4. The method according to claim 1, wherein said step of calculating a new gain factor based on said pending round trip time RTT value comprises:
determining a maximum value of the reference round trip time RTT and a minimum value of the reference round trip time RTT;
calculating a first difference value between the maximum round trip time RTT value and the minimum round trip time RTT value;
calculating a second difference value between the maximum round trip time RTT value and the round trip time RTT value to be processed;
determining the new gain coefficient according to the ratio of the first difference value and the second difference value;
wherein the content of the first and second substances,
the maximum value of the reference round trip time RTT and the minimum value of the reference round trip time RTT are parameters obtained by detecting the satellite link before the round trip time RTT value to be processed is obtained.
5. The method of claim 1, wherein the determining a new transmission rate for the transmitting end according to the new gain factor comprises:
determining a gain coefficient threshold range to which the new gain coefficient belongs;
and determining a new sending rate aiming at the sending end according to the rate calculation model corresponding to the gain coefficient threshold range.
6. The method according to claim 5, wherein the step of determining a new transmission rate for the transmitter according to the rate calculation model corresponding to the gain factor threshold range comprises at least one of the following sub-steps:
if the new gain factor is greater than 1.25, determining the new sending rate aiming at the sending end according to the product of the bandwidth BtlBW of the satellite link, the reference gain factor and 1.25;
and if the new gain coefficient is not less than 1 and not more than 1.25, determining the new sending rate aiming at the sending end according to the product of the bandwidth BtlBW of the satellite link, the reference gain coefficient and the new gain coefficient.
7. The method according to claim 1, wherein the step of controlling the sending end to perform data transmission processing according to the new sending rate comprises:
determining the corresponding relation between the time of satellite link delay and throughput according to the new sending rate;
and controlling the sending end to carry out data transmission processing based on the corresponding relation.
8. A congestion control apparatus for a satellite link, comprising:
the time delay detection module is used for acquiring a round trip time RTT value to be processed, which is sent out by a sending end in a satellite link;
the gain calculation module is used for calculating a new gain coefficient of the satellite link based on the RTT value of the round trip time to be processed;
the rate calculation module is used for determining a new sending rate aiming at the sending end according to the new gain coefficient;
and the congestion control module is used for controlling the sending end to carry out data transmission processing according to the new sending rate so as to realize congestion control on the satellite link.
9. A terminal, comprising: memory, processor and computer program stored on the memory and executable on the processor, characterized in that the processor executes the computer program to implement the method of any of claims 1 to 7.
10. A computer-readable storage medium storing computer-executable instructions for performing the method of any one of claims 1 to 7.
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN112929078A (en) * | 2021-03-17 | 2021-06-08 | 中科院计算技术研究所南京移动通信与计算创新研究院 | Data transmission control method and device based on synchronous orbit satellite communication system |
| CN113014505A (en) * | 2021-03-30 | 2021-06-22 | 北京邮电大学 | Transmission control method for time delay differentiation in high dynamic topology satellite network |
| CN114039654A (en) * | 2021-12-08 | 2022-02-11 | 重庆邮电大学 | Routing method based on load balancing and oriented to large-scale LEO satellite network |
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| CN109639340B (en) * | 2018-12-11 | 2021-05-28 | 成都天奥信息科技有限公司 | TCP acceleration method suitable for satellite link |
| CN110120921B (en) * | 2019-05-13 | 2022-07-01 | 深圳市赛为智能股份有限公司 | Congestion avoidance method, apparatus, computer device and storage medium |
| CN111314960B (en) * | 2020-02-19 | 2023-04-07 | 东南大学 | Social awareness-based collaborative caching method in fog wireless access network |
| CN111683393B (en) * | 2020-05-25 | 2021-12-17 | 华中科技大学 | Adaptive congestion control method for dynamically adjusting gain coefficient |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112929078A (en) * | 2021-03-17 | 2021-06-08 | 中科院计算技术研究所南京移动通信与计算创新研究院 | Data transmission control method and device based on synchronous orbit satellite communication system |
| CN112929078B (en) * | 2021-03-17 | 2022-12-27 | 南京中科晶上通信技术有限公司 | Data transmission control method and device based on synchronous orbit satellite communication system |
| CN113014505A (en) * | 2021-03-30 | 2021-06-22 | 北京邮电大学 | Transmission control method for time delay differentiation in high dynamic topology satellite network |
| CN113014505B (en) * | 2021-03-30 | 2022-10-14 | 北京邮电大学 | Transmission control method for time delay differentiation in high dynamic topology satellite network |
| CN114039654A (en) * | 2021-12-08 | 2022-02-11 | 重庆邮电大学 | Routing method based on load balancing and oriented to large-scale LEO satellite network |
| CN114039654B (en) * | 2021-12-08 | 2023-07-25 | 重庆邮电大学 | Routing method based on load balancing for large-scale LEO satellite network |
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