CN110311725B - Modular design method for backup ring of satellite-borne transponder - Google Patents

Modular design method for backup ring of satellite-borne transponder Download PDF

Info

Publication number
CN110311725B
CN110311725B CN201910630135.9A CN201910630135A CN110311725B CN 110311725 B CN110311725 B CN 110311725B CN 201910630135 A CN201910630135 A CN 201910630135A CN 110311725 B CN110311725 B CN 110311725B
Authority
CN
China
Prior art keywords
backup
switch
backup ring
connection
sub
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
CN201910630135.9A
Other languages
Chinese (zh)
Other versions
CN110311725A (en
Inventor
王碧茹
赵光
李静涛
高鹏
李殷乔
杨丽
佟金成
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.)
China Academy of Space Technology CAST
Original Assignee
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 China Academy of Space Technology CAST filed Critical China Academy of Space Technology CAST
Priority to CN201910630135.9A priority Critical patent/CN110311725B/en
Publication of CN110311725A publication Critical patent/CN110311725A/en
Application granted granted Critical
Publication of CN110311725B publication Critical patent/CN110311725B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04BTRANSMISSION
    • H04B1/00Details of transmission systems, not covered by a single one of groups H04B3/00 - H04B13/00; Details of transmission systems not characterised by the medium used for transmission
    • H04B1/74Details of transmission systems, not covered by a single one of groups H04B3/00 - H04B13/00; Details of transmission systems not characterised by the medium used for transmission for increasing reliability, e.g. using redundant or spare channels or apparatus
    • H04B1/745Details of transmission systems, not covered by a single one of groups H04B3/00 - H04B13/00; Details of transmission systems not characterised by the medium used for transmission for increasing reliability, e.g. using redundant or spare channels or apparatus using by-passing or self-healing methods
    • 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
    • H04B7/18515Transmission equipment in satellites or space-based relays
    • 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

Abstract

The invention discloses a modularized design method for a backup ring of a satellite-borne transponder, which comprises the following steps: (1) dividing the required backup ring to form each submodule needing to grow; (2) according to each submodule needing to be grown in the step (1), the basic module generates each required submodule through prolonged growth or derivative growth; (3) connecting all required sub-modules to form a backup ring; (4) and meeting the backup support of the backup ring according to the connection condition of the backup ring. The invention solves the design of a complex switch backup ring, and the design of the method is restricted to form a minimum backup ring, namely the number of total switches is minimum, and the number of switches passing through when switching from the master to the backup is minimum on the premise of meeting the requirements of users.

Description

Modular design method for backup ring of satellite-borne transponder
Technical Field
The invention belongs to the technical field of satellite-borne repeaters, and particularly relates to a modular design method for a backup ring of a satellite-borne repeater.
Background
Communication satellite transponders are the main load for the satellite to provide services to subscribers. Due to the non-maintainability of the satellite, the satellite equipment adopts backup design to improve the reliability of the satellite. The main backup device and the backup device are reasonably connected through the switch to form a backup ring, and the main backup device can be switched to backup through the switch when the main backup device fails.
During satellite design, a backup design is carried out on a high-power amplifier of a transponder, wherein a backup ring is N: K backup (N is more than or equal to K), the total number of the high-power amplifiers is N, the number of the masters is K, and the number of the backups is N-K. For example, the traveling wave tube amplifier has 8:6 backups, the high-power amplifier adopts a traveling wave tube form, and 8 traveling wave tubes are provided in total, wherein 6 traveling wave tubes are the main backup and 2 backups. The backup requirement of the user for the high power amplifier is
(1) Any N-K main share amplifiers can be switched to backup when failing, and the number of the total effective working amplifiers is not influenced;
(2) when the failure primary shares are switched to the corresponding first backup, the work of other paths is not influenced.
With the increasing number of repeaters and the increasing scale of the backup ring, it is important to optimize the design of the backup ring on the premise of satisfying the user requirements.
Disclosure of Invention
The technical problem solved by the invention is as follows: the design of the backup ring of the complex switch is restricted to form the minimum backup ring, namely the total switch number is minimum, and the number of switches passing through when switching from the master to the backup is minimum on the premise of meeting the requirements of a user.
The purpose of the invention is realized by the following technical scheme: a modular design method for a backup ring of a satellite-borne transponder comprises the following steps: (1) dividing the required backup ring to form each submodule needing to grow; (2) according to each submodule needing to be grown in the step (1), the basic module generates each required submodule through prolonged growth or derivative growth; (3) connecting all required sub-modules to form a backup ring; (4) and meeting the backup support of the backup ring according to the connection condition of the backup ring.
In the modularized design method of the satellite-borne transponder backup ring, in the step (1), an N: K backup ring can be divided into N-K submodules; the sub-module segmentation method comprises the following steps:
a) N-K ═ 1, undivided;
b) dividing N-K-2 into two submodules; wherein the content of the first and second substances,
if N and K are both odd, the two submodules are respectively
Figure BDA0002128462650000021
And
Figure BDA0002128462650000022
if N and K are both even numbers, the two sub-modules are of the same form
Figure BDA0002128462650000023
A sub-module;
c) N-K is more than or equal to 3 and is divided into N-K submodules.
In the modular design method of the backup ring of the satellite-borne transponder, in the step (2), for the backup ring with N: K, when N-K is less than or equal to 2, namely the number of the sub-modules forming the backup ring is less than or equal to 2, the extension growth is adopted; wherein, the extension growth is that a new main part connecting switch is added between the main part connecting switch and the backup connecting switch on the basis of a 4:3 basic module, and the cyclic operation is carried out in sequence to extend the branched chain; for any backup ring with N: K, the growth of a basic module can adopt derivative growth, namely, a transfer switch is added on a branched chain on the basis of a 4:3 basic module, two ports of the transfer switch are connected with a master connection switch and a backup connection switch on an original branched chain, and the other two ports of the transfer switch are respectively connected with a new master connection switch needing to be added.
In the modular design method of the backup ring of the satellite-borne transponder, a basic module is a 4:3 module or a 5:4 module; wherein, one 4:3 module has 3 main connection switches, 1 backup connection switch and no transfer switch; the main part connecting switch is provided with 4 ports, one port is used for being connected with the backup switch to form a backup ring basic module, one port is connected with the main part equipment, one port is used as an output port, and the rest ports are used as connecting ends and are used for being connected with the connecting ends of other sub-modules to form a larger backup ring; the backup switch is provided with four ports, one port is connected with the backup device, and the other three ports are respectively connected with other switches to form three branched chains; the 5:4 module has 3 main connection switches, 1 backup connection switch and a transfer switch. The main part connecting switch is provided with 4 ports, one port is used for being connected with the transfer switch to form a backup ring basic module, one port is connected with the main part equipment, one port is used as an output port, and the rest ports are used as connecting ends and are used for being connected with the connecting ends of other sub-modules to form a larger backup ring; the backup switch has four ports, one port is connected with the backup device, the other two ports are used as the connection and output end of the master device, and the remaining one port is connected with the transfer switch. The transfer switch is connected with the three main part connecting switches to form three branched chains, and the three branched chains and a backup connecting switch form an end chain.
In the modular design method for the backup ring of the satellite-borne transponder, in the step (3), the connecting the required sub-modules to form the backup ring includes: respectively taking two backup connection switches as starting points, selecting the connection ends of two sub-modules to be connected, and connecting according to an equal length principle, namely, the number of the switches at intervals between the backup connection switches in the sub-modules to which the connection ends belong is the same after the connection ends are connected until the connection of all the sub-module connection ends which can be connected with each other is finished; all the sub-modules are connected with other sub-modules, and all the connecting ends of one sub-module are not connected with another sub-module; if the total number of the connection terminals is an odd number, one and only one connection terminal remains after all the connection terminals are connected, and the connection terminals the load.
In the modular design method for the backup ring of the satellite-borne transponder, in the step (4), the connection condition of the backup ring is as follows: when N-K is more than 2, any 3 master connection switches can not be directly connected, namely every 2 master connection switches are connected with other master connection switches, and a transfer switch is added in the middle; when N-K is more than or equal to 5, when the 4:3 submodule is used, the number of the main share connecting switches connected with the same backup connecting switch cannot exceed 4, namely, a transfer switch needs to be added between the backup connecting switch and the main share connecting switch.
Compared with the prior art, the invention has the following beneficial effects:
the invention can solve the design of the complex switch backup ring, the design of the method is restricted to form the minimum backup ring, namely the minimum number of the total switches, and the minimum number of the switches passing through when switching from the master to the backup on the premise of meeting the requirements of users.
Drawings
Various other advantages and benefits will become apparent to those of ordinary skill in the art upon reading the following detailed description of the preferred embodiments. The drawings are only for purposes of illustrating the preferred embodiments and are not to be construed as limiting the invention. Also, like reference numerals are used to refer to like parts throughout the drawings. In the drawings:
FIG. 1 is a schematic structural diagram of a 4:3 base module provided by an embodiment of the present invention;
FIG. 2 is a schematic structural diagram of a 5:4 base module provided by an embodiment of the present invention;
FIG. 3 is a schematic diagram of the extended growth of a base module provided by an embodiment of the present invention;
FIG. 4 is a schematic illustration of the derivative growth of a base module provided by an embodiment of the present invention;
FIG. 5 is a schematic diagram of sub-module connections provided by an embodiment of the present invention;
FIG. 6 is a schematic diagram of the connection of 1 15:12 backup ring according to an embodiment of the present invention;
fig. 7 is a schematic connection diagram of another backup ring according to an embodiment of the present invention.
Detailed Description
Exemplary embodiments of the present disclosure will be described in more detail below with reference to the accompanying drawings. While exemplary embodiments of the present disclosure are shown in the drawings, it should be understood that the present disclosure may be embodied in various forms and should not be limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the scope of the disclosure to those skilled in the art. It should be noted that the embodiments and features of the embodiments may be combined with each other without conflict. The present invention will be described in detail below with reference to the embodiments with reference to the attached drawings.
The embodiment provides a modularized design method for a backup ring of a satellite-borne transponder, which comprises the following steps:
(1) dividing the required backup ring to form each submodule needing to grow;
(2) according to each submodule needing to be grown in the step (1), the basic module generates each required submodule through prolonged growth or derivative growth;
(3) connecting all required sub-modules to form a backup ring;
(4) and meeting the backup support of the backup ring according to the connection condition of the backup ring.
It should be understood that the backup ring required in step (1) is the backup ring formed in step (3), and specifically, the backup ring in step (1) is not formed yet.
The specific method comprises the following steps:
(1) backup ring partitioning
For an N: K backup ring, it can be split into N-K sub-modules. For example, an 8:6 backup ring may be split into 2 sub-modules.
The partitioning method of the sub-modules is as follows.
a) And (3) directly entering the second step without segmentation, wherein the N-K is 1.
b) N-K2 is divided into two submodules
If N, K is odd, the two submodules are respectively
Figure BDA0002128462650000051
And
Figure BDA0002128462650000052
for example, an 11:9 backup ring, would be split into two sub-modules, 6:5 and 5: 4.
If N, K is even, the two submodules are of equal form
Figure BDA0002128462650000053
And (5) sub-modules.
c) N-K is more than or equal to 3 and is divided into N-K submodules.
And dividing the submodules, wherein the factor to be considered is that the difference between the maximum submodule and the minimum submodule is less than or equal to 2 when the difference between the submodules is as small as possible.
For example, a 16:13 backup ring may be divided into two 6:5 sub-modules and a 4:3 sub-module. A 15:12 backup ring may be divided into three 5:4 backup rings, but into three modules of 6:5,5:4 and 4:3 to reduce the number of odd modules.
(2) Generating sub-modules
The generation basis of the sub-modules is 4:3 or 5:4 modules, which become the basic modules, as shown in fig. 1 and 2, respectively. Both modules can be the basis for all backup ring generation. The smaller backup ring is not discussed here.
For clarity of reference, the switch classes are named here as follows:
the master part is connected with the switch: a switch connected to the master device;
a backup connection switch: the switch connected with the backup device is still called as a backup connection switch even if the switch is also connected with the master device;
a transfer switch: the switches are connected only to other switches and not directly connected to the device.
As shown in fig. 1, from the 4:3 base module, one base module has 3 primary connection switches, 1 backup connection switch, and no transfer switch. The main connection switch is provided with 4 ports, one port is used for being connected with the backup switch to form a backup ring basic module, one port is connected with the main equipment, one port is used as an output port, and the other port is used as a connecting end and is used for being connected with the connecting ends of other sub-modules to form a larger backup ring. The backup switch has four ports, one port is connected with the backup device, and the other three ports are respectively connected with other switches to form three branched chains.
As shown in fig. 2, as seen from the 5:4 base module, there are 3 primary connection switches, 1 backup connection switch, and one transfer switch for one base module. The master connection switch is provided with 4 ports, one port is used for being connected with the transfer switch to form a backup ring basic module, one port is connected with the master device, one port is used as an output port, and the other port is used as a connecting end and is used for being connected with the connecting ends of other sub-modules to form a larger backup ring. The backup switch has four ports, one port is connected with the backup device, the other two ports are used as the connection and output end of the master device, and the remaining one port is connected with the transfer switch. The transfer switch is connected with the three main part connecting switches to form three branched chains, and the three branched chains and a backup connecting switch form an end chain.
And generating sub-modules of M: M-1. M: the submodule of M-1 is derived from the basic module, a specific method called growth. The growth regimes are divided into two, termed elongation growth and derivative growth, depending on the total number of backup loops.
And (3) prolonging growth: for the backup ring of N: K, when N-K is less than or equal to 2, namely the number of the sub-modules forming the backup ring is less than or equal to 2, the prolonged growth can be adopted. And the extension growth is that on the basis of a 4:3 basic module, a new main connection switch is added between the main connection switch and the backup connection switch, and the cyclic operation is performed in sequence to extend the branched chain. As shown in FIG. 3, a 5:4 building block was formed by using elongation growth for branch-1 of the 4:3 building block. Equal acceleration growth should be adopted for growth of each branched chain, for example, if a 7:6 submodule is to be formed, three main connecting switches should be added on a 4:3 basic module, and one switch should be added on each branched chain of the three branched chains.
The prolonged growth has the following characteristics:
the number of the connection ends of the base module is not increased, so that the number of the connection ends of one base module is still 3;
the number of switches in the backup ring is increased by the same amount as the increase of the scale of the backup ring;
with the increase of the scale of the sub-module of the backup ring, the number of switches for switching the equipment to backup is large.
And (3) derivative growth: for any N: K backup ring, the growth of the basic module can adopt derivative growth.
The derivation growth is that on the basis of a 4:3 basic module, a transfer switch is added on a branched chain, two ports of the transfer switch are connected with a master connection switch and a backup connection switch on the original branched chain, and the other two ports of the transfer switch are respectively connected with a new master connection switch needing to be added. As shown in FIG. 4, a 6:5 building block was formed by using derivatization growth for branch-1 of the 4:3 building block. An equal acceleration rate should be used for growth of each branch, for example, if a 10:9 basis module is to be formed, a derivative growth is required on each branch of the 4:3 basis module.
The characteristics of the derivative growth are as follows:
the number of the connecting ends of the basic module is 3+ the number of the transfer switches is 2, namely the more the derived counts are, the more the connecting ends are;
total number of base module switches, e.g. M: m-1 module with a number of switches of
Figure BDA0002128462650000071
The roundup operator is rounding up, for example, roundup (1.2) ═ 2.
The selection of the basic module, an N: K backup ring, can be divided into N-K basic modules M: M-1, so that even-scale submodules (M is even) are grown from 4:3 basic modules, and odd-scale submodules (M is odd) are generated from 5:4 basic modules.
(3) Submodule connection
After the required sub-modules are generated, the sub-modules need to be connected to form a backup ring.
The two backup connection switches are respectively taken as starting points, the connection ends of the two sub-modules are selected to be connected, and the connection ends are connected according to the equal length principle as much as possible, namely, the number of the switches at intervals between the backup connection switches in the sub-modules to which the connection ends belong is the same or similar as much as possible after the connection ends are connected until the connection of all the sub-module connection ends which can be connected with each other is finished. To illustrate the equal length principle, as shown in FIG. 5, assume that there is a 14:11 backup ring divided into two 4:3 sub-modules and a 6:5 sub-module. The connecting end-1 in the sub-module 1 is connected with the connecting end-1 in the sub-module 2 through a connecting wire 1. So that the backup connection switch in submodule 1 is spaced from the backup connection switch in submodule 2 by 2 switches. Similarly, the connection terminal-5 in the sub-module 1 is connected with the connection terminal-1 in the sub-module 3 by the connection line 2, and 2 switches are separated between the two backup connection switches. The connecting end-3 of the sub-module 1 is connected with the connecting end 3 of the sub-module 2 through a connecting wire 4, and the backup connecting switches of the modules are 3 switches at intervals.
All sub-modules should be connected to other sub-modules, and it cannot happen that all connection terminals of one sub-module are connected to another sub-module.
If the total number of the connection terminals is an odd number, one and only one connection terminal remains after all the connection terminals are connected, and the connection terminals the load.
If the number of switches in the backup ring is reduced, the submodules of the backup ring all adopt an extended growth mode.
(4) Checking backup support of a backup ring
When the number of the connecting ends of the sub-modules is less than the number of the sub-modules, the situation that the backup ring cannot support all backup switching occurs. For example, for 1 15:12 backup ring, if the connection mode of fig. 6 is used, the capability of taking over the work by the backup under any 3 primary HPA failures cannot be realized.
A transfer switch is added in the connection of the two sub-modules, so that the global backup capability of the backup ring can be realized. As shown in fig. 7, a connection switch is added at the connection end of 3 5:4 sub-modules, and the backup ring can meet the fault of any 3 main share amplifiers and can be replaced by the backup.
To satisfy the global support of the backup ring N: K, the following should be ensured when the backup ring is connected:
a. when N-K is more than 2, any 3 master connection switches can not be directly connected, namely every 2 master connection switches are connected with other master connection switches, and a transfer switch is added in the middle;
b. when N-K is more than or equal to 5, if the 4:3 submodule is used, the number of the main share connecting switches connected with the same backup connecting switch cannot exceed 4, namely a transfer switch needs to be added between the backup connecting switch and the main share connecting switch.
The embodiment can solve the design of the complex switch backup ring, and the design constraint of the method is to form the minimum backup ring, namely the total switch number is minimum, and the number of switches passing through when switching from the master to the backup is minimum on the premise of meeting the requirements of a user.
The above-described embodiments are merely preferred embodiments of the present invention, and general changes and substitutions by those skilled in the art within the technical scope of the present invention are included in the protection scope of the present invention.

Claims (5)

1. A modularized design method for a backup ring of a satellite-borne transponder is characterized by comprising the following steps:
(1) dividing the required backup ring to form each submodule needing to grow;
(2) according to each submodule needing to be grown in the step (1), the basic module generates each required submodule through prolonged growth or derivative growth;
(3) connecting all required sub-modules to form a backup ring;
(4) satisfying the backup support of the backup ring according to the backup ring connection condition;
in the step (2), for the backup ring of N: K, when N-K is less than or equal to 2, namely the number of the sub-modules forming the backup ring is less than or equal to 2, adopting the extension growth; wherein, the extension growth is that a new main part connecting switch is added between the main part connecting switch and the backup connecting switch on the basis of a 4:3 basic module, and the cyclic operation is carried out in sequence to extend the branched chain;
for any backup ring with N: K, the growth of a basic module can adopt derivative growth, namely, a transfer switch is added on a branched chain on the basis of a 4:3 basic module, two ports of the transfer switch are connected with a master connection switch and a backup connection switch on an original branched chain, and the other two ports of the transfer switch are respectively connected with a new master connection switch needing to be added;
wherein N is the total number of the high power amplifiers, K is the number of the masters, and N-K is the number of the backups.
2. The modular design method for the backup ring of the satellite-borne transponder according to claim 1, characterized in that: in the step (1), for an N: K backup ring, the N-K backup ring can be divided into N-K sub-modules; the sub-module segmentation method comprises the following steps:
a) N-K ═ 1, undivided;
b) dividing N-K-2 into two submodules; wherein the content of the first and second substances,
if N and K are both odd, the two submodules are respectively
Figure FDA0003173430040000011
And
Figure FDA0003173430040000012
if N and K are both even numbers, the two sub-modules are of the same form
Figure FDA0003173430040000013
A sub-module;
c) N-K is more than or equal to 3 and is divided into N-K submodules.
3. The modular design method for the backup ring of the satellite-borne transponder according to claim 1, characterized in that: the basic module is a 4:3 module or a 5:4 module; wherein the content of the first and second substances,
the 4:3 module has 3 main connection switches, 1 backup connection switch and no transfer switch; the main part connecting switch is provided with 4 ports, one port is used for being connected with the backup switch to form a backup ring basic module, one port is connected with the main part equipment, one port is used as an output port, and the rest ports are used as connecting ends and are used for being connected with the connecting ends of other sub-modules to form a larger backup ring; the backup switch is provided with four ports, one port is connected with the backup device, and the other three ports are respectively connected with other switches to form three branched chains;
the 5:4 module has 3 main part connecting switches, 1 backup connecting switch and a transfer switch; the main part connecting switch is provided with 4 ports, one port is used for being connected with the transfer switch to form a backup ring basic module, one port is connected with the main part equipment, one port is used as an output port, and the rest ports are used as connecting ends and are used for being connected with the connecting ends of other sub-modules to form a larger backup ring; the backup switch is provided with four ports, one port is connected with the backup device, the other two ports are used as the connection and output ends of the master device, and the remaining one port is connected with the transfer switch; the transfer switch is connected with the three main part connecting switches to form three branched chains, and the three branched chains and a backup connecting switch form an end chain.
4. The modular design method for the backup ring of the satellite-borne transponder according to claim 1, characterized in that: in step (3), connecting the required sub-modules to form a backup ring comprises: respectively taking two backup connection switches as starting points, selecting the connection ends of two sub-modules to be connected, and connecting according to an equal length principle, namely, the number of the switches at intervals between the backup connection switches in the sub-modules to which the connection ends belong is the same after the connection ends are connected until the connection of all the sub-module connection ends which can be connected with each other is finished; wherein the content of the first and second substances,
all sub-modules should be connected to other sub-modules, and it cannot happen that all connection ends of one sub-module are connected to another sub-module;
if the total number of the connection terminals is an odd number, one and only one connection terminal remains after all the connection terminals are connected, and the connection terminals the load.
5. The modular design method for the backup ring of the satellite-borne transponder according to claim 4, characterized in that: in step (4), the backup ring connection condition is:
when N-K is more than 2, any 3 master connection switches can not be directly connected, namely every 2 master connection switches are connected with other master connection switches, and a transfer switch is added in the middle;
when N-K is more than or equal to 5, when the 4:3 submodule is used, the number of the main share connecting switches connected with the same backup connecting switch cannot exceed 4, namely, a transfer switch needs to be added between the backup connecting switch and the main share connecting switch.
CN201910630135.9A 2019-07-12 2019-07-12 Modular design method for backup ring of satellite-borne transponder Active CN110311725B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201910630135.9A CN110311725B (en) 2019-07-12 2019-07-12 Modular design method for backup ring of satellite-borne transponder

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201910630135.9A CN110311725B (en) 2019-07-12 2019-07-12 Modular design method for backup ring of satellite-borne transponder

Publications (2)

Publication Number Publication Date
CN110311725A CN110311725A (en) 2019-10-08
CN110311725B true CN110311725B (en) 2021-12-07

Family

ID=68080184

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201910630135.9A Active CN110311725B (en) 2019-07-12 2019-07-12 Modular design method for backup ring of satellite-borne transponder

Country Status (1)

Country Link
CN (1) CN110311725B (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1328075A2 (en) * 2002-01-11 2003-07-16 Trw Inc. Redundancy switching for satellite payload
CN102104472A (en) * 2010-12-15 2011-06-22 中国空间技术研究院 Method for determining switch network
CN104407949A (en) * 2014-11-28 2015-03-11 中国航天科技集团公司第九研究院第七七一研究所 Spaceborne module-level redundant backup system and method
CN108631857A (en) * 2018-03-29 2018-10-09 西安空间无线电技术研究所 A kind of control method for automatically switching and system of communication satellite coverage backup ring
CN108683446A (en) * 2018-03-29 2018-10-19 西安空间无线电技术研究所 A kind of communication satellite coverage double frequency-band power amplifier backup ring and switching method
CN108964744A (en) * 2018-06-29 2018-12-07 西安空间无线电技术研究所 A kind of communication satellite coverage power amplifier backup ring Cascading Methods

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7369810B2 (en) * 2001-10-05 2008-05-06 The Boeing Company Satellite transponder architecture with integral redundancy and beam selection capabilities

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1328075A2 (en) * 2002-01-11 2003-07-16 Trw Inc. Redundancy switching for satellite payload
CN102104472A (en) * 2010-12-15 2011-06-22 中国空间技术研究院 Method for determining switch network
CN104407949A (en) * 2014-11-28 2015-03-11 中国航天科技集团公司第九研究院第七七一研究所 Spaceborne module-level redundant backup system and method
CN108631857A (en) * 2018-03-29 2018-10-09 西安空间无线电技术研究所 A kind of control method for automatically switching and system of communication satellite coverage backup ring
CN108683446A (en) * 2018-03-29 2018-10-19 西安空间无线电技术研究所 A kind of communication satellite coverage double frequency-band power amplifier backup ring and switching method
CN108964744A (en) * 2018-06-29 2018-12-07 西安空间无线电技术研究所 A kind of communication satellite coverage power amplifier backup ring Cascading Methods

Also Published As

Publication number Publication date
CN110311725A (en) 2019-10-08

Similar Documents

Publication Publication Date Title
US6047331A (en) Method and apparatus for automatic protection switching
JP2022093513A (en) Optical network management device
KR101527403B1 (en) Network node for an optical transport network
RU2684734C2 (en) Hitless rearrangement of a satellite-hosted switch via propagated synchronization
EP2958251B1 (en) Method and node for detecting subframe sequence error in inverse multiplexing
CN110725987A (en) Converter valve system
JPH0234079A (en) Method of linkage allocation and routing of signal link of common line signal system repeating station
EP3582507B1 (en) Intelligence-defined optical tunnel network system and network system control method
EP3582417B1 (en) Intelligence- defined optical tunnel network system controller and control method thereof
CN110311725B (en) Modular design method for backup ring of satellite-borne transponder
JPS63172589A (en) Inter-equipment communication control system
US7035539B2 (en) Interconnecting nodes in an optical communication system
EP3582506A1 (en) Intelligence - defined optical tunnel network system and network system control method
CN100584101C (en) Optical switching station and switching method for the same
CN102497245A (en) Clock synchronization method and clock management interface board
US9585032B2 (en) Method and arrangement for providing data plane redundancy
CN101997606A (en) Node management method and control plane
JPH0683245B2 (en) Efficient single-hop directional multi-channel system
US4009351A (en) Switching arrangement for telecommunication switching systems
US6463033B1 (en) Dual hubbed tree architecture for a communication network
EP3582509A1 (en) Intelligence-defined optical tunnel network system and network system control method
CN106716719B (en) Antenna, antenna system and base station
US11528085B2 (en) Fault tolerance method for any set of simultaneous link faults in dynamic WDM optical networks with wavelength continuity constraint
CN103401789A (en) Method and equipment for transmitting LSP (Link State Protocol Data Unit) messages
CN214672906U (en) Multiplexer public port device

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