CN103647664A - Distributed simulation system for deep space multi-relay satellite communication - Google Patents

Distributed simulation system for deep space multi-relay satellite communication Download PDF

Info

Publication number
CN103647664A
CN103647664A CN201310680254.8A CN201310680254A CN103647664A CN 103647664 A CN103647664 A CN 103647664A CN 201310680254 A CN201310680254 A CN 201310680254A CN 103647664 A CN103647664 A CN 103647664A
Authority
CN
China
Prior art keywords
data
federal member
deep space
transmission
relay satellite
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.)
Granted
Application number
CN201310680254.8A
Other languages
Chinese (zh)
Other versions
CN103647664B (en
Inventor
杨志华
张钦宇
谭奇
袁鹏
宋昊阳
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.)
Shenzhen Graduate School Harbin Institute of Technology
Original Assignee
Shenzhen Graduate School Harbin Institute of Technology
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 Shenzhen Graduate School Harbin Institute of Technology filed Critical Shenzhen Graduate School Harbin Institute of Technology
Priority to CN201310680254.8A priority Critical patent/CN103647664B/en
Publication of CN103647664A publication Critical patent/CN103647664A/en
Application granted granted Critical
Publication of CN103647664B publication Critical patent/CN103647664B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Abstract

The invention provides a distributed simulation system for deep space multi-relay satellite communication. The system employs a structure based on a high-level architecture (HLA) standard and has reusability and interoperability; the system can realize data communication among multiple protocols and different simulation system platforms, and solves the problems of incapability of identifying data among the different protocols and non-standardized interfaces of simulation systems; the system can realize real-time and real transmission of each data packet, the transmission effects are obvious, and the performance analysis is high; through externally connected software, real transmission scenes can be simulated, and real-time dynamic communication environment data is provided; through two relay federal members, multiple relays are simulated and multi-node segment data transmission for a deep space DTN is demonstrated, and through multi-relay multi-hop segment transmission, transmission efficiency in a deep space long distance and long time delay environment is improved; and an acquisition scheduling module is taken as a control center of a simulation platform, on one hand, real-time related data of current simulation platform operation is acquired and displayed in real time, and on the other hand, effective analysis can be performed on acquired data, and related decisions are made. The simulation system provided by the invention has three characteristics of interrupted connection, storage forwarding and keep transmission, thereby being well adaptive to the transmission characteristics of a space DTN.

Description

Distributing emulation system towards the many repeater satellite communications of deep space
Technical field
The invention belongs to deep space communication emulation field, relate to a kind of distributing emulation system towards the many repeater satellite communications of deep space.
Background technology
Deep space communication is the important leverage that survey of deep space task is implemented smoothly, and it is faced with and the distinct difficult problem of communicating by letter of traditional terrestrial wireless communication, for example: long transmission distance, path loss is large, and propagation delay is long, the frequent interruption in chain Louis etc.
Because survey of deep space experiment is difficult for carrying test, good emulation platform can, the communication link under accurate simulating deep space environment, analyzes and tests relevant technology and theory, is the necessary guarantee that deep space communication research is carried out.
Current more popular following four sections of network simulators:
1) NS2:NS2 (Network Simulator version 2) network simulator is a kind of OO network simulator.NS2 software is furnished with simulation process dynamic watcher, can after simulation run finishes, dynamically watch the running of emulation, observes the data of following the tracks of.NS2 is powerful, and extensibility is strong, and execution efficiency is high, has been widely used in the emulation of local area network (LAN), wide area network, wireless mobile network and satellite network.
2) OMNeT++:OMNeT++ is a kind of Discrete Event Simulator, possesses insertion type simulation kernel and powerful graphical interfaces interface, can run on a plurality of operating system platforms, possesses programming, and the functions such as debugging and tracking support are also supported distributed parallel emulation.
3) DTNsim:DTNsim is the discrete event simulator of writing with Java language, and the message stores while being used for the middle Transmission of analog D TN (Distributed Transient Network, the transient network of distribution) or failure forwards.DTNsim also supports the burst of message to transmit.If encounter connection closed in a message transport process, and had the success of message burst to be received by node, this node will be waited for the arrival of remaining message burst so.
4) ONE:ONE is applicable to the Routing Protocol of DTN network environment and the simulator that application study is analyzed, and has the feature of discrete event driving, object-oriented and Reality simulation network environment.ONE integrates mobility model, DTN route and visual graphical interfaces, is very easy to expand, and a large amount of analytical model and report the tests can be provided.
Although there is very outstanding simulation performance in Zhe Si money simulation software, when the data communication package of emulation survey of deep space, exist the shortcoming that cannot go beyond:
1) NS2 lacks DTN network environment is well supported.Meanwhile, when NS2 carries out multinode emulation, can not transmit real data, this causes carrying out the transmission of True Data.
2) OMNET++ needs user oneself to realize specific function.Meanwhile, when the extensive node of NS2 experiment simulation, can not transmit True Data, can only transmitting data information.
3) DTNsim is specially for the simulator of DTN Environment Design.But it just merely pays close attention to the emulation of route.Meanwhile, when multinode emulation, can not carry out the transmission of True Data.
4) ONE network simulator has only been realized the BP part of DTN agreement, when carrying out multinode emulation, just transmits virtual data (information of data message), can not realize True Data transmission and can not embody data flow.
In sum, NS2 and OMNET++ network simulator lack DTN network environment good support, need user specifically to develop.Although and DTNsim and ONE network simulator are to be the simulator of DTN Environment Design specially, have defect separately.And when multinode emulation, it all can only simulate virtual data transmission, can not carry out True Data transmission, can not meet the requirement of deep space protocol emulation, cannot realize deep space protocol emulation.
For example, Chinese patent literature 1 (CN102821159 A) has been recorded a kind of distributing emulation system towards deep space communication, this system comprises functional simulation assembly, simulated environment generation and more New Parent, simulation performance analysis and record component, wherein, functional simulation assembly comprises probe satellite federal member, relay satellite federal member, speed control federal member, ground station's federal member, simulated environment generation and more New Parent comprise deep space environment federal member, and simulation performance analysis and record component comprise data acquisition federal member.Although, document 1 mentioned relay satellite federal member can have a plurality of,, document 1 does not provide a plurality of relay satellite federal members and how to realize the multi-hop communication emulation based on a plurality of intermediate satellites.
Deep space communication is because the path loss that overlength distance communication causes is very huge, and propagation delay time is long.Under prior art condition, the transmission of non-relay end-to-end link cannot meet the demands, and current space DTN network has: many relayings, long delay, frequently interrupt, the feature such as file keeping transmission, by utilizing many via nodes, the segmentation transfer of data that cooperated.
Summary of the invention
In order to solve the problems of the prior art, the present invention proposes a kind of distributing emulation system towards the many repeater satellite communications of deep space, the transmission of many via nodes of energy simulation demo segmentation collaboration data, analog link frequently interrupt, realize the platform of file transfer protocol (FTP), thereby can be in the many relay transmission of ground demonstration deep space file, for deep space multinode transport communication scheme provides technical support.
The present invention is achieved through the following technical solutions:
A distributing emulation system towards the many repeater satellite communications of deep space, comprising: survey of deep space federal member, relay satellite federal member I, relay satellite federal member II, ground station's federal member, deep space environment federal member and collection scheduling federal member;
Wherein, survey of deep space federal member, for realizing Data Collection, and the agreement of emulation as required processes data, then sends to relay satellite federal member;
Relay satellite federal member I and relay satellite federal member II, for realizing the data relay transmission of data communication process;
Ground station's federal member, as the receiving terminal of detection data, for receiving the data of relay satellite federal member transmission, realizes the Recovery processing of data;
Deep space environment federal member, for generating deep space environment data and by the mode of broadcast, in real time the described deep space environment data in each federal member in whole analogue system being upgraded;
Data acquisition scheduling federal member, selects record storage and many via nodes transmission route of the data parameter of simulation process for realizing.
Under the scheduling of data acquisition scheduling federal member, by relay satellite federal member I and relay satellite federal member II, alternately realize different a plurality of via nodes in each jumping.
Further, described under the scheduling of data acquisition scheduling federal member, by relay satellite federal member I and relay satellite federal member II, alternately realizing different a plurality of via nodes in each jumping is specially: member is according to definite scene information in data acquisition scheduling, is broadcast to each data module; Relay satellite federal member I and relay satellite federal member II receive after scene information, carry out the coupling of corresponding scene; Collection scheduling federal member is by link information between each node of gathering simulation scene and determine accordingly transmission route, thereby determines and respectively jump selected node on a plurality of nodes, reinforms to relay satellite federal member I and relay satellite federal member II.
Further, the data parameter in described simulation process comprises link information between node, the current transmission progress of data and Route Selection.
Further, described deep space environment federal member kit software STK generation via satellite deep space environment data.
Further, the described distributing emulation system towards the many repeater satellite communications of deep space adopts C++ code to realize.
The invention has the beneficial effects as follows: the distributing emulation system 1 towards the many repeater satellite communications of deep space of the present invention) adopted the structure based on High Level Architecture (HLA) standard, there is reusability and interoperability; 2) can realize between multi-protocols, the data communication between different Simulation System Platforms, has solved data None-identified, the nonstandard problem of each analogue system interface between different agreement; 3) unusual analogue system simulation virtual data transmission, analogue system of the present invention is packed to Data Division waiting for transmission, truly transmits in real time each packet, and laser propagation effect is obvious, and performance evaluation is strong; 4) be different from traditional value that provides a few parameters, analogue system of the present invention provides real-time dynamic communication environmental data by the true transmitting scene of external software emulation.For example, the loss of the real-time distance of communicating by letter, real-time link state, live signal etc., have avoided tradition to get the mistake of can not ignore that valued methods brings; 5) analogue system of the present invention is by a plurality of relayings of the federal simulation of two relayings, and demonstration is towards the multinode segment data transmission of deep space DTN network.By multi-hop (the many relayings of every jumping) segment transmissions, improve the efficiency of transmission under deep space middle and long distance, long delay environment.6) analogue system collection scheduling module of the present invention is as the control centre of emulation platform, on the one hand, the real-time related data (such as the percentage that current data transmits, the link information between each data transmitter etc.) that gathers current emulation platform operation, shows in real time; On the other hand, the data that gather are effectively analyzed, made relevant decision-making (such as control data transmission situation), make whole platform carry out effectively really data transmission; 7) analogue system of the present invention possesses interrupted connection, storage forwarding and certainly transmits three large characteristics, and this is the fine space DTN Internet Transmission characteristic that adapted to also.
Accompanying drawing explanation
Fig. 1 is the structure chart of the distributing emulation system of the many repeater satellite communications of deep space of the present invention;
Fig. 2 is that two trunk modules of the present invention are simulated the implementation procedure of many relayings;
Fig. 3 is delaying type CFDP protocol transmission model schematic diagram;
Fig. 4 is the distributing emulation system workflow diagram of the many repeater satellite communications of deep space of the present invention;
Fig. 5 is the data acquisition scheduler module work schematic diagram of system of the present invention.
Embodiment
Below in conjunction with accompanying drawing explanation and embodiment, the present invention is further described.
Difficult point of emulation deep space DTN Internet Transmission is to provide in real time emulation link data.Analogue system of the present invention is introduced external deep space scenario simulation software satellite kit (STK), and configuration needs the deep space scene of emulation, automatically produces in real time the information such as each internodal link information and tracks variation, for emulation provides true link information.
Distributed Simulation Platform based on HLA, analogue system multinode analog communication process of the present invention, index extraction and dynamically demonstration in real time.As shown in Figure 1, analogue system of the present invention consists of five federal members, respectively: survey of deep space federal member, relay satellite federal member (2), ground station's federal member, deep space environment federal member and collection scheduling federal member.A plurality of via nodes of wherein, jumping by alternately simulation difference of two relaying federal members (I, II) complete transfer of data.
Each federal member of analogue system of the present invention is as follows:
Survey of deep space federal member: realize Data Collection, and the agreement of emulation as required or encoding scheme process to data, then send, backward target is relay satellite federal member (n).Effect in whole analogue system is: 1. the collection of detection data; 2. according to concrete agreement or encoding scheme, data are processed; 3. data flow transmitting terminal, backward contact is relay satellite federal member.
Relay satellite federal member (I, II): the transmission trunking in communication process, the effect of relay satellite federal member is: realize the effect of signal amplification forwarding 1.; 2. embody the performance of each relay satellite, state; 3. data flow intermediate link, final forward direction node is probe satellite federal member, final backward node is ground station's federal member (multistage).
Ground station's federal member: be detection data receiving terminal in whole analogue system, realize the Recovery processing work of detection data.The effect of ground station's federal member is: 1. data flow recover detection data according to corresponding coding or agreement in receiving system; 2. the terminal of data flow in system, its forward direction node is relay satellite federal member.
Deep space environment federal member: play very important effect in whole analogue system, it has guaranteed, whole simulation process carries out in real deep space environment, and this federal member is complementary member, does not participate in the transmission of data flow in analogue system directly.Deep space environment federal member generates after these deep space environment data, in real time these data is upgraded in whole artificial network.The effect of deep space environment federal member is: produce in real time deep space environment data and by the mode of broadcast, make each federal member in system carry out real-time update to data.
Data acquisition scheduling federal member: realize record storage and the multinode transmission route of simulation process data parameter are selected, the control member that this federal member is system emulation, does not participate in flowing of emulated data stream directly.For example link information, the current transmission progress of data and Route Selection between node.The effect of data acquisition scheduling federal member is: realize the pick up and store to analogue system performance data 1.; 2. the encoding scheme of pair emulation or the protocol scheme performance in emulation is given and preliminary judgement.
Highlight the realization of many via nodes of emulation networking transmission below, mainly comprise following three aspects:
The realization of (1) two trunk module
In order to embody True Data, flow, be easy to simulation demo platform subsequent development (such as increasing hardware channel module), each via node should be realized separately (as a computer is realized a node), runs into like this difficult point: during many via nodes of emulation, need to expend great amount of hardware resources.The present invention proposes to utilize two trunk module simulations to realize the transfer of data of a plurality of via nodes, completes emulation.Two trunk modules are identical in essence, serve as different roles during just due to simulation multinode.Just in single, then say and should have: store and forward function, and adjust in real time message transmission rate according to the characteristic of link; The function with simulation multinode.
Accompanying drawing 2 is that two trunk modules are simulated many relayings implementation procedure.Simulating scenes is that Mars sends data, and the store and forward through Mars repeater satellite (2, A and B)-moon repeater satellite (C)-earth repeater satellite (D), finally arrives earth base station.Total process is divided into four sections of transmission, supposes that red link is for determining Route Selection (being Mars-A-C-D-earth).
Utilize two trunk modules (I and II) to simulate whole trunk network (A, B, C and D), complete many via nodes segmentation cooperation transmission.Specific implementation process: the operation of deep space communication scene, probe satellite (mars exploration car) sends data to Mars repeater satellite A, now with trunk module I simulation A, receives data; Store and forward, to down hop moon repeater satellite node C, now receives data with trunk module II simulation C, and store and forward is to down hop earth repeater satellite node D; Now, trunk module I holds two duties, in simulation A, simulates earth repeater satellite D, receives the data of sending from a upper node C, and store and forward is to down hop earth base station, and final earth base station receives data and completes whole deep space communication emulation.The advantage of such scheme is: compare with directly realizing many relayings, save hardware resource; With with the simulation of single trunk module, compare, embody True Data and flow, be easy to subsequent expansion.
(2) realization of deep space environment module
The topological diagram information of deep space environment module based on receiving, configures the true transmitting scene of corresponding deep space.By simulating deep space real scene, for platform provides deep space link information in real time, mainly comprise: the link in deep space DTN network between each object is communicated with situation (link break-make), link-quality (error rate) and link range etc. in real time.
Utilize STK simulate whole from mars exploration car through junction network, finally arrive each celestial body of link level simulation of earth base station and its satellite etc.This deep space environment scene comprises:
Celestial body, has Mars and the earth, is respectively used to carry mars exploration car and earth base station;
Satellite, by a certain amount of Mars repeater satellite, moon repeater satellite and earth repeater satellite, has formed junction network, is responsible for data to carry out store and forward;
Mars exploration car and earth base station, transmission and last reception of being responsible for data.
Below the deep space environment scene that has substantially just contained required emulation, wherein celestial body, mars exploration car and earth base station are fixed, and for each scene, are the same.Because the kind of repeater satellite and the difference of quantity have brought up the difference of last deep space environment DTN network scenarios, thereby also brought up emulation platform can emulation arbitrarily (based on truth, should be within the specific limits) deep space environment of relay scene, strengthened the extensibility of emulation platform.
(3) realization of collection scheduling module
Be unableing to do without in order reasonably of many relayings multi-hop segment transmissions dispatched.Based on to the current transmission link information of Real-time Collection and transmission progress analysis, specified data transmission route, ensures that multinode relay transmission effectively reliably completes.Analogue system of the present invention provides Route Selection interface, can be for freely realizing specific routing algorithm.
Collection scheduling module, as the core of analogue system of the present invention, has center leading position.On the one hand, be responsible for gathering the real-time related data (such as the percentage that current data transmits, the link information between each data transmitter etc.) of current emulation platform operation, show in real time; On the other hand, the data that gather are effectively analyzed, made relevant decision-making (such as control data transmission situation), make whole platform carry out effectively really data transmission.
Collection scheduling module mainly realizes by following four aspects:
A. according to topological structure, automatically set up corresponding real scene, emulation deep space communication environment, provides link information in real time.
B. scheduler module is according to the link information and the data transmission state that gather, position relationship between real-time update topology diagram and each object.
C. according to current topological structure figure, determine in real time transmission route, complete scheduled transmission.Because via node receives data, receive and send out (receive after data at once store and forward to down hop via node), so selecting route is determining at the very start, the routing strategy that this platform is taked is: first, select next-hop node have link as transmission node, but, when down hop has the node of link, have when a plurality of, chosen distance nearest as transmission node.Certainly, complicated routing algorithm also can be realized in analogue system of the present invention.
D. gather current data transmission progress and transmission rate, show in real time.
Under the scheduling of data acquisition scheduling federal member, by relay satellite federal member I and relay satellite federal member II alternately realize each jump in different a plurality of via nodes be specially: data acquisition scheduling member according to definite scene information (be mainly the scene information of trunk network, as " 3-2-4; "), be broadcast to each data module.Relay satellite federal member I and relay satellite federal member II receive after scene information, carry out the coupling of corresponding scene: the via node that is positioned at odd positions corresponding to relay satellite federal member I simulation, as " 3 " and " 4 "; Corresponding, the via node that is positioned at even number position corresponding to relay satellite federal member II simulation, as " 2 ", thereby determines the attribute in relay satellite federal member I and II simulation multi-hop relay on the whole.And then, collection scheduling federal member is by link information between each node of gathering simulation scene (link break-make and distance etc.), according to this, determine that (selection of transmission route algorithm can independently define transmission route, here the segment transmissions of simple 1 pair 1 of selecting, selects the node of first selecting to be communicated with from down hop link; If it is a plurality of that the node that link is communicated with has, that nearest node of chosen distance), thus determine and respectively jump selected node on a plurality of nodes, reinform to relaying I and II.Part, relay satellite federal member I and relay satellite federal member II have just determined the concrete node identity of the own nodal community of realizing like this.Thereby under the scheduling of data acquisition scheduling federal member, by relay satellite federal member I and relay satellite federal member II, alternately realize different a plurality of via nodes in each jumping and simulate.
The emulation CFDP agreement of take is example, simple declaration simulation process:
CFDP agreement is flexible, the efficient space channel Data Transport Protocol that international space data system Advisory Board (CCSDS) suggestion is used.CFDP is the file storage based on actual, and agreement can be used at inter-entity transmission data block.Analogue system of the present invention adopts and postpones negative type CFDP agreement, and its transporting mechanism as shown in Figure 3.
The workflow of analogue system of the present invention as shown in Figure 4.This flow chart is to take the file transfer protocol (FTP) (delaying type CFDP) of CCSDS suggestion to design as artificial tasks.
Analogue system of the present invention is used C++, interface to realize with MFC.Simulating scenes is:
Figure 834286DEST_PATH_IMAGE002
From accompanying drawing 5, can clearly see in data acquisition scheduling federation, real-time update simulation space DTN network topology structure (upper left), show each section of link of current transmission route link information (under) and gather display image data real-time Transmission progress (upper right).
Emulation conclusion:
U analogue system has successfully completed the emulation of CFDP agreement, and actual emulation number of retransmissions is consistent with theoretical value.
U learns through Multi simulation running, in deep space communication transfer of data, utilizes many relayings multi-hop networking transmission, higher than the efficiency of the point-to-point transmission of single relaying.
Distributing emulation system towards the communication of many repeater satellites of deep space of the present invention has the following advantages: 1) adopted the structure based on High Level Architecture (HLA) standard, had the feature of reusability and interoperability.Reusability can guarantee, within the relatively the shortest time, with minimum cost, to develop satisfactory analogue system.Interoperability, can guarantee to carry out real-time cooperation and communication between each function of system member; 2) can realize between multi-protocols, the data communication between different Simulation System Platforms, has solved data None-identified, the nonstandard problem of each analogue system interface between different agreement; 3) unusual analogue system simulation virtual data transmission, analogue system of the present invention is packed to Data Division waiting for transmission, truly transmits in real time each packet, and laser propagation effect is obvious, and performance evaluation is strong; 4) be different from traditional value that provides a few parameters, analogue system of the present invention provides real-time dynamic communication environmental data by the true transmitting scene of external software emulation.For example, the loss of the real-time distance of communicating by letter, real-time link state, live signal etc., have avoided tradition to get the mistake of can not ignore that valued methods brings; 5) analogue system of the present invention is by a plurality of relayings of the federal simulation of two relayings, and demonstration is towards the multinode segment data transmission of deep space DTN network.By multi-hop (the many relayings of every jumping) segment transmissions, improve the efficiency of transmission under deep space middle and long distance, long delay environment.6) analogue system collection scheduling module of the present invention is as the control centre of emulation platform, on the one hand, the real-time related data (such as the percentage that current data transmits, the link information between each data transmitter etc.) that gathers current emulation platform operation, shows in real time; On the other hand, the data that gather are effectively analyzed, made relevant decision-making (such as control data transmission situation), make whole platform carry out effectively really data transmission; 7) analogue system of the present invention possesses interrupted connection, storage forwarding and certainly transmits three large characteristics, and this is the fine space DTN Internet Transmission characteristic that adapted to also.
Above content is in conjunction with concrete preferred implementation further description made for the present invention, can not assert that specific embodiment of the invention is confined to these explanations.For general technical staff of the technical field of the invention, without departing from the inventive concept of the premise, can also make some simple deduction or replace, all should be considered as belonging to protection scope of the present invention.

Claims (5)

1. towards a distributing emulation system for the many repeater satellite communications of deep space, it is characterized in that: this system comprises: survey of deep space federal member, relay satellite federal member I, relay satellite federal member II, ground station's federal member, deep space environment federal member and collection scheduling federal member; Wherein,
Survey of deep space federal member, for realizing Data Collection, and the agreement of emulation as required processes data, then sends to relay satellite federal member;
Relay satellite federal member I and relay satellite federal member II, for realizing the data relay transmission of data communication process;
Ground station's federal member, as the receiving terminal of detection data, for receiving the data of relay satellite federal member transmission, realizes the Recovery processing of data;
Deep space environment federal member, for generating deep space environment data and by the mode of broadcast, in real time the described deep space environment data in each federal member in whole analogue system being upgraded;
Data acquisition scheduling federal member, selects record storage and many via nodes transmission route of the data parameter of simulation process for realizing;
Wherein, under the scheduling of data acquisition scheduling federal member, by relay satellite federal member I and relay satellite federal member II, alternately realize different a plurality of via nodes in each jumping.
2. distributing emulation system according to claim 1, it is characterized in that: described under the scheduling of data acquisition scheduling federal member, by relay satellite federal member I and relay satellite federal member II, alternately realizing different a plurality of via nodes in each jumping is specially: member is according to definite scene information in data acquisition scheduling, is broadcast to each data module; Relay satellite federal member I and relay satellite federal member II receive after scene information, carry out the coupling of corresponding scene; Collection scheduling federal member is by link information between each node of gathering simulation scene and determine accordingly transmission route, thereby determines and respectively jump selected node on a plurality of nodes, reinforms to relay satellite federal member I and relay satellite federal member II.
3. distributing emulation system according to claim 1, is characterized in that: the data parameter in described simulation process comprises link information between node, the current transmission progress of data and Route Selection.
4. distributing emulation system according to claim 1, is characterized in that: described deep space environment federal member via satellite kit software STK produces deep space environment data.
5. distributing emulation system according to claim 1, is characterized in that: the described distributing emulation system towards the many repeater satellite communications of deep space adopts C++ code to realize.
CN201310680254.8A 2013-12-13 2013-12-13 Towards the distributing emulation system of many repeater satellite communications of deep space Active CN103647664B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201310680254.8A CN103647664B (en) 2013-12-13 2013-12-13 Towards the distributing emulation system of many repeater satellite communications of deep space

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201310680254.8A CN103647664B (en) 2013-12-13 2013-12-13 Towards the distributing emulation system of many repeater satellite communications of deep space

Publications (2)

Publication Number Publication Date
CN103647664A true CN103647664A (en) 2014-03-19
CN103647664B CN103647664B (en) 2017-06-06

Family

ID=50252825

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201310680254.8A Active CN103647664B (en) 2013-12-13 2013-12-13 Towards the distributing emulation system of many repeater satellite communications of deep space

Country Status (1)

Country Link
CN (1) CN103647664B (en)

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105227457A (en) * 2015-10-28 2016-01-06 哈尔滨工业大学深圳研究生院 Towards the protocol Data Unit cross-layer optimizing method under DTN dynamic link
CN105357039A (en) * 2015-10-27 2016-02-24 中国船舶重工集团公司第七二二研究所 Simulation method and device for delay tolerant network
CN106850431A (en) * 2016-12-21 2017-06-13 航天东方红卫星有限公司 A kind of optimal route selection method of many attributes for being applied to low rail Information Network
CN107294593A (en) * 2017-06-21 2017-10-24 哈尔滨工业大学深圳研究生院 Deep space downlink multi-hop transmission method and system based on GEO backbone's relayings
CN108639380A (en) * 2018-03-29 2018-10-12 北京空间技术研制试验中心 Lunar surface sniffing robot
CN109214042A (en) * 2018-07-20 2019-01-15 北京航空航天大学 A kind of method that artificial intelligence program person writes data relaying load source code
CN109495157A (en) * 2018-11-15 2019-03-19 西安空间无线电技术研究所 A kind of full duplex high-throughput bidirectional ARQ communication system and method based on CCSDS agreement
CN109890044A (en) * 2019-03-15 2019-06-14 上海微小卫星工程中心 Complicated Satellite system simulation real-time network communication system
CN110677190A (en) * 2019-10-09 2020-01-10 大连大学 Static processing and caching method for space-ground integrated intelligent network node
CN111812966A (en) * 2020-07-02 2020-10-23 北京航天飞行控制中心 Multi-spacecraft-based time difference between heaven and earth determining method, determining device and processor
CN113746737A (en) * 2021-09-03 2021-12-03 哈尔滨工业大学 AODV protocol-based multi-node ad hoc network transmission simulation method and simulation system
CN116488712A (en) * 2023-06-21 2023-07-25 凯睿星通信息科技(南京)股份有限公司 Non-real-time relay communication method based on improved store-and-forward protocol

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6002360A (en) * 1997-03-07 1999-12-14 Trw Inc. Microsatellite array and related method
CN101155088A (en) * 2007-09-17 2008-04-02 北京航空航天大学 Satellite network protocol simulation system and method
CN101404547A (en) * 2008-11-21 2009-04-08 中国科学院软件研究所 Satellite network simulation system
CN101741627A (en) * 2008-11-14 2010-06-16 电子科技大学 Double-engine distribution type peer-to-peer network simulation system architecture
CN102413483A (en) * 2011-11-02 2012-04-11 北京理工大学 Constellation cooperation high-capacity all-weather communication method based on celestial body relay
CN102694632A (en) * 2012-04-19 2012-09-26 哈尔滨工业大学深圳研究生院 Deep space file transfer method based on relay store-forward
CN102821159A (en) * 2012-08-20 2012-12-12 哈尔滨工业大学深圳研究生院 Distributed simulation system for deep space communication
CN102882643A (en) * 2012-09-21 2013-01-16 哈尔滨工业大学深圳研究生院 Data transfer rate control method based on deep space communication

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6002360A (en) * 1997-03-07 1999-12-14 Trw Inc. Microsatellite array and related method
CN101155088A (en) * 2007-09-17 2008-04-02 北京航空航天大学 Satellite network protocol simulation system and method
CN101741627A (en) * 2008-11-14 2010-06-16 电子科技大学 Double-engine distribution type peer-to-peer network simulation system architecture
CN101404547A (en) * 2008-11-21 2009-04-08 中国科学院软件研究所 Satellite network simulation system
CN102413483A (en) * 2011-11-02 2012-04-11 北京理工大学 Constellation cooperation high-capacity all-weather communication method based on celestial body relay
CN102694632A (en) * 2012-04-19 2012-09-26 哈尔滨工业大学深圳研究生院 Deep space file transfer method based on relay store-forward
CN102821159A (en) * 2012-08-20 2012-12-12 哈尔滨工业大学深圳研究生院 Distributed simulation system for deep space communication
CN102882643A (en) * 2012-09-21 2013-01-16 哈尔滨工业大学深圳研究生院 Data transfer rate control method based on deep space communication

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105357039A (en) * 2015-10-27 2016-02-24 中国船舶重工集团公司第七二二研究所 Simulation method and device for delay tolerant network
CN105357039B (en) * 2015-10-27 2019-01-18 中国船舶重工集团公司第七二二研究所 A kind of emulation mode and device of time delay tolerant network
CN105227457A (en) * 2015-10-28 2016-01-06 哈尔滨工业大学深圳研究生院 Towards the protocol Data Unit cross-layer optimizing method under DTN dynamic link
CN105227457B (en) * 2015-10-28 2018-10-16 哈尔滨工业大学深圳研究生院 Towards the protocol Data Unit cross-layer optimizing method under DTN dynamic links
CN106850431A (en) * 2016-12-21 2017-06-13 航天东方红卫星有限公司 A kind of optimal route selection method of many attributes for being applied to low rail Information Network
CN106850431B (en) * 2016-12-21 2020-05-12 航天东方红卫星有限公司 Multi-attribute optimal routing method applied to low-orbit information network
CN107294593A (en) * 2017-06-21 2017-10-24 哈尔滨工业大学深圳研究生院 Deep space downlink multi-hop transmission method and system based on GEO backbone's relayings
CN107294593B (en) * 2017-06-21 2020-05-01 哈尔滨工业大学深圳研究生院 Deep space downlink multi-hop transmission method and system based on GEO backbone relay
CN108639380A (en) * 2018-03-29 2018-10-12 北京空间技术研制试验中心 Lunar surface sniffing robot
CN109214042A (en) * 2018-07-20 2019-01-15 北京航空航天大学 A kind of method that artificial intelligence program person writes data relaying load source code
CN109214042B (en) * 2018-07-20 2023-04-07 北京航空航天大学 Method for writing data relay load source code by artificial intelligence programmer
CN109495157A (en) * 2018-11-15 2019-03-19 西安空间无线电技术研究所 A kind of full duplex high-throughput bidirectional ARQ communication system and method based on CCSDS agreement
CN109495157B (en) * 2018-11-15 2021-09-03 西安空间无线电技术研究所 Full-duplex high-throughput rate bidirectional ARQ communication system and method based on CCSDS protocol
CN109890044A (en) * 2019-03-15 2019-06-14 上海微小卫星工程中心 Complicated Satellite system simulation real-time network communication system
CN110677190A (en) * 2019-10-09 2020-01-10 大连大学 Static processing and caching method for space-ground integrated intelligent network node
CN111812966A (en) * 2020-07-02 2020-10-23 北京航天飞行控制中心 Multi-spacecraft-based time difference between heaven and earth determining method, determining device and processor
CN113746737A (en) * 2021-09-03 2021-12-03 哈尔滨工业大学 AODV protocol-based multi-node ad hoc network transmission simulation method and simulation system
CN113746737B (en) * 2021-09-03 2022-06-14 哈尔滨工业大学 AODV protocol-based multi-node ad hoc network transmission simulation method and simulation system
CN116488712A (en) * 2023-06-21 2023-07-25 凯睿星通信息科技(南京)股份有限公司 Non-real-time relay communication method based on improved store-and-forward protocol
CN116488712B (en) * 2023-06-21 2023-09-12 凯睿星通信息科技(南京)股份有限公司 Non-real-time relay communication method based on improved store-and-forward protocol

Also Published As

Publication number Publication date
CN103647664B (en) 2017-06-06

Similar Documents

Publication Publication Date Title
CN103647664B (en) Towards the distributing emulation system of many repeater satellite communications of deep space
Cheng et al. A comprehensive simulation platform for space-air-ground integrated network
CN106571956B (en) Satellite networking routing protocol simulation system and method
CN111314166B (en) Multi-node comprehensive simulation system and method
CN101404547B (en) Satellite network simulation system
CN104865844B (en) A kind of Information Network comprehensive assessment demenstration method based on distributed platform
CN105871487B (en) A kind of system integration project demonstration and verification system towards satellite mobile communication
US8352223B1 (en) Network communications testbed
CN112327667B (en) Semi-physical simulation element design method for large-scale unmanned cluster network
CN105357039B (en) A kind of emulation mode and device of time delay tolerant network
CN106921523B (en) Data transmission method based on GEO/LEO satellite network
CN108337036A (en) A kind of inter-satellite link analogue system based on navigation satellite constellation
CN105915304A (en) System-level simulation demonstration verification method facing satellite mobile communication
CN108737141B (en) Satellite link intermittent and delayed simulation method
CN112115589B (en) VR-Force and OPNET based joint simulation system and method
CN105227483A (en) Based on the low complex degree Load Balance Routing Algorithms of LEO satellite network
CN109067453A (en) The elastic routing algorithm of the unpredictable interruption of satellite DTN network based on space-time graph model
CN113315569A (en) Satellite reliability routing method and system with weighted link survival time
CN110674584B (en) Multi-aircraft joint simulation system
Zema et al. The CUSCUS simulator for distributed networked control systems: Architecture and use-cases
CN102821159B (en) Towards the distributing emulation system of deep space communication
Sánchez-Carmona et al. Filling in the missing link between simulation and application in opportunistic networking
CN110149140A (en) The retransmission method of satellite opportunistic network
CN115913426A (en) Virtual-real cooperative world integrated scene simulation system
CN103745049A (en) Novel multi-factor tactical internet connection reliability simulation method

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant