JPH01200732A - Satellite repeating system - Google Patents
Satellite repeating systemInfo
- Publication number
- JPH01200732A JPH01200732A JP2370288A JP2370288A JPH01200732A JP H01200732 A JPH01200732 A JP H01200732A JP 2370288 A JP2370288 A JP 2370288A JP 2370288 A JP2370288 A JP 2370288A JP H01200732 A JPH01200732 A JP H01200732A
- Authority
- JP
- Japan
- Prior art keywords
- intermediate frequency
- frequency band
- satellite
- earth station
- switch matrix
- 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.)
- Pending
Links
Landscapes
- Radio Relay Systems (AREA)
Abstract
Description
【発明の詳細な説明】
(産業上の利用分野)
本発明は、衛星通信において、衛星搭載中継器を効率よ
く使用すると共に、高信頼度を達成する衛星中継方式に
関するものである。DETAILED DESCRIPTION OF THE INVENTION (Field of Industrial Application) The present invention relates to a satellite relay system that efficiently uses a satellite-mounted repeater and achieves high reliability in satellite communications.
(従来の技術)
衛星通信方式においては、高アンテナ利得が得られ、か
つ、周波数の再使用が可能なマルチビーム方式の適用が
有利と々る。従来のマルチビーム方式の構成例を第1図
に示す。+a−+cはマルチビームアンテナが照射する
サービスゾーン、f。(Prior Art) In a satellite communication system, it is advantageous to apply a multi-beam system that provides high antenna gain and allows frequency reuse. An example of the configuration of a conventional multi-beam system is shown in FIG. +a-+c is the service zone irradiated by the multi-beam antenna, and f.
〜f6は受信周波数、F1〜F6は送信周波数、1は地
球局、2は送受信用マルチビームアンテナ、3は分波器
、4は受信器、5は送信器、6は合波器、7はMXMス
イッチマトリクス、8はスイッチマトリクスの制御回路
を示す。地球局から送信された信号は、2のマルチビー
ムアンテナおよび3の分波器を経て、4の受信器によっ
て共通の中間周波数に変換増幅され、7のM刈■スイッ
チマド’Jクスにより切替接続された後、5の送信器に
よシ送信周波数に変換増幅され、6の合波器および2の
マルチビームアンテナを経て、地球局に向けて送信され
る。第2図はスイッチマトリクスの1フレーム内の接続
状態例を示してお沙、8のスイッチマトリクスの制御回
路はこの接続状態を回路内に記憶し、これによって7の
スイッチマトリクスの制御を行う。接続状態は地上から
のコマンドによシ可変である。第1図における各地球局
は、自局の送信周波数と目的局の受信周波数が接続され
ているタイミングに同期してバースト信号を送信する。~f6 is the receiving frequency, F1 to F6 are the transmitting frequencies, 1 is the earth station, 2 is the multi-beam antenna for transmitting and receiving, 3 is the demultiplexer, 4 is the receiver, 5 is the transmitter, 6 is the multiplexer, 7 is the MXM switch matrix, 8 indicates a control circuit of the switch matrix. The signal transmitted from the earth station passes through the multi-beam antenna (2) and the branching filter (3), is converted to a common intermediate frequency by the receiver (4), and is amplified.Then, the signal is switched and connected by the M-type switch (7). After that, it is converted and amplified to a transmission frequency by a transmitter 5, and transmitted to the earth station via a multiplexer 6 and a multi-beam antenna 2. FIG. 2 shows an example of the connection state of the switch matrix within one frame.The control circuit of the switch matrix 8 stores this connection state in the circuit, and controls the switch matrix 7 accordingly. The connection status can be changed by commands from the ground. Each earth station in FIG. 1 transmits a burst signal in synchronization with the timing at which its own station's transmission frequency and the target station's reception frequency are connected.
このようなマルチビーム方式では、搭載アンテナの利得
が高いため、伝送容量の向上や地球局の小型化が可能で
あり、寸だ、ビーム間で周波数の再使用が可能である。In such a multi-beam system, the gain of the on-board antenna is high, so it is possible to improve transmission capacity and downsize the earth station, and it is possible to reuse frequencies between beams.
(発明が解決しようとする課題)
しかし、各ビーム間でトラヒックが均衡している場合は
よいが、特定のビームにトラヒックが集中した場合、他
のビームの中継器が空いていたとしてもその中継器を利
用することができないため4S軽状態となるという欠点
を有していた。まだ、1ビームでも故障するとシステム
が不完全となるため、特に、高出力増幅器を使用する下
9回線側では信頼性の確保が大きな問題であった。(Problem to be solved by the invention) However, it is fine if the traffic is balanced among each beam, but if traffic is concentrated on a specific beam, even if the repeaters for other beams are vacant, the relay It had the disadvantage that it was in a 4S light state because it could not use the equipment. However, if even one beam fails, the system becomes incomplete, so ensuring reliability was a major problem, especially on the lower nine lines, which use high-power amplifiers.
本発明は、前記のようなマルチビーム方式において、衛
星搭載中継器における幅端状態を緩和すると共に、高信
頼度を実現する衛星中継方式を提供することにある。An object of the present invention is to provide a satellite relay system that alleviates the width edge condition of a satellite-mounted repeater and achieves high reliability in the multi-beam system as described above.
(課題を解決するだめの手段)
本発明の特徴は、上り回線にマルチビーム方式を適用し
、送信器の高出力化でE I RP (Equival
entisotropicallyRadiated
power) (実効放射電力)の向上が可能な下り
回線にはシングルビーム方式を適用すると共に、トラヒ
ックの鰯鯖が発生しにくいシングルビーム側の送信器台
数Nを受信器台数Mより少なくシ、全地球局間の相互接
続を実現するだめに、各送受信器間をMXNスイッチマ
トリクスにより接続したととを最も主要な特徴としてい
る。(Means for Solving the Problem) The feature of the present invention is to apply a multi-beam method to the uplink and increase the output of the transmitter to increase E I RP (Equival
entisotropicallyRadiated
In addition to applying the single beam system to the downlink where it is possible to improve the effective radiated power (effective radiation power), the number of transmitters N on the single beam side, where traffic congestion is less likely to occur, is smaller than the number of receivers M, and the total The most important feature is that each transmitter/receiver is connected by an MXN switch matrix in order to realize interconnection between earth stations.
(実施例)
第3図は本発明の詳細な説明する図であって、ナa〜4
cは受信用マルチビームアンテナが照射するサービスゾ
ーン、+、Aは送信用シングルビームアンテナが照射す
るサービスゾーン、f1〜f6は受信周波数、F1〜F
4は送信周波数、1は地球局、9は受信用マルチビーム
アンテナ、10は送信用シングルビームアンテナ、3は
分波器、4は受信器、5は送信器、6は合波器、7′は
MxNスイッチマトリクス、8はスイッチマトリクスの
制御回路を示す。地球局から送信された信号は、2のマ
ルチビームアンテナおよび3の分波器を経て、4の受信
器によって共通の中間周波数に変換増幅され、7′の八
/11 X Nスイッチマトリクスによシ切替接続され
た後、5の送信器により送信周波数に変換増幅され、6
の合板器および2のマルチビームアンテナを経て、地球
局に向けて送信される。第4図はスイッチマトリクスの
1フレーム内の接続状に、弓例を示しており、8のスイ
ッチマトリクスの制御回路はこの接続状態を回路内に記
憶し、これによって7′のスイッチマトリクスの制御を
行う。接続状態は地上からのコマンドにより可変である
。(Example) FIG. 3 is a diagram illustrating the present invention in detail.
c is the service zone illuminated by the receiving multi-beam antenna, +, A is the service zone illuminated by the transmitting single beam antenna, f1 to f6 are the receiving frequencies, F1 to F
4 is a transmission frequency, 1 is an earth station, 9 is a multi-beam antenna for reception, 10 is a single beam antenna for transmission, 3 is a demultiplexer, 4 is a receiver, 5 is a transmitter, 6 is a multiplexer, 7' indicates an MxN switch matrix, and 8 indicates a control circuit for the switch matrix. The signal transmitted from the earth station passes through 2 multi-beam antennas and 3 branching filters, is converted to a common intermediate frequency by 4 receivers, and is amplified by a 7'8/11 X N switch matrix. After being switched and connected, it is converted and amplified to the transmission frequency by the transmitter 5, and
The signal is transmitted to the earth station via a plywood and two multi-beam antennas. Figure 4 shows an example of a bow in the connection state of the switch matrix within one frame, and the control circuit of the switch matrix 8 stores this connection state within the circuit, thereby controlling the switch matrix 7'. conduct. The connection status can be changed by commands from the ground.
第3図における各地球局は、自局の送信周波数と目的局
の受信周波数が接続されているタイミングに同期してバ
ースト信号を送信する。このような構成では、各受信地
球局は受信周波数さえ変更すれば全送信器から受信する
ことができるだめ、受信器(第3図では6台)に対して
少数の送信器(第3図では4台)であっても十分トラヒ
ックの変動に対する柔軟性を確保することができる。さ
らに、何台かの送信器が故障したとしても残シすべての
送信器から受信することができるため信頼性の点でも有
利となる。一般に、受信器は低電力で動作するため、消
費電力、重量、信頼性とも大きな負担とならないが、送
信器は消し#:電力、重量、故障率が大きいため、上記
の構成は、送信器を効率的に利用できる点で大きな効果
を有している。Each earth station in FIG. 3 transmits a burst signal in synchronization with the timing at which its own station's transmission frequency and the target station's reception frequency are connected. In such a configuration, each receiving earth station can receive from all transmitters by changing the receiving frequency, so a small number of transmitters (6 in Fig. 3) are used for the receivers (6 in Fig. 3). Even with 4 units), sufficient flexibility can be ensured against traffic fluctuations. Furthermore, even if some transmitters fail, reception can be received from all remaining transmitters, which is advantageous in terms of reliability. In general, the receiver operates with low power, so it does not impose a large burden on power consumption, weight, or reliability. It has a great effect in that it can be used efficiently.
(発明の効果)
以上説明したように、マルチビーム方式は大容量化、地
球局の小型化、周波数の有効利用という点で有効である
が、中継器の効率利用、信頼性という点で欠点を有して
いた。本発明では、中継器の効率利用、信頼性があ1り
負担と々らない受信側のみマルチビーム方式を適用し、
送信側については、各地球局間の相互接続性を維持しつ
つ送信器の台数を低減したシングルビーム方式とするこ
とによって、中継器の効率利用、信頼性の向上を可能と
した。これにより、システム全体として高効率で信頼性
の高い衛星中継方式を笑現することが可能となる。(Effects of the Invention) As explained above, the multi-beam system is effective in terms of increasing capacity, downsizing the earth station, and effectively using frequencies, but it has drawbacks in terms of efficient use of repeaters and reliability. had. In the present invention, the multi-beam method is applied only to the receiving side, which is efficient in using repeaters, reliable, and does not impose a large burden.
On the transmitting side, by adopting a single beam system that reduces the number of transmitters while maintaining interconnectivity between each earth station, it is possible to use repeaters more efficiently and improve reliability. This makes it possible to realize a satellite relay system that is highly efficient and reliable as a whole system.
第1図はマルチビームを使用する従来の衛星通信方式の
システム構成図、第2図は第1図におけるサテライトス
イッチの動作図、第3図は本発明のシステム構成図、第
4図は本発明におけるスイッチマトリクスの]フレーム
内の接続状態を示す図である。
1・・地球局、
2・・送受信用マルチビームアンテナ、3 分波器、
4・受f言器、
5・・・送信器、
6 ・合波器、
7・・・MXMサテライトスイッチ、
7′・・・B/L X Nサテライトスイッチ(M>N
)、8・・サテライトスイッチの制御回路、9 ・受信
用マルチビームアンテナ、
10・・送信用マルチビームアンテナ、=ll−a〜+
−C・・マルチビームアンテナが照身」するサービスゾ
ーン
+A・・シングルビームアンテナが照射するサービスゾ
ーン。Fig. 1 is a system configuration diagram of a conventional satellite communication system using multi-beams, Fig. 2 is an operation diagram of the satellite switch in Fig. 1, Fig. 3 is a system configuration diagram of the present invention, and Fig. 4 is a system configuration diagram of the present invention. FIG. 3 is a diagram showing the connection state within a frame of a switch matrix in FIG. 1...Earth station, 2...Multi-beam antenna for transmission and reception, 3. Brancher, 4. Receiver, 5...Transmitter, 6.Multiplexer, 7...MXM satellite switch, 7' ...B/L X N satellite switch (M>N
), 8... Satellite switch control circuit, 9 - Receiving multi-beam antenna, 10... Transmitting multi-beam antenna, =ll-a~+
-C: Service zone illuminated by the multi-beam antenna +A: Service zone illuminated by the single beam antenna.
Claims (1)
通信を中継する衛星中継方式において、衛星上に、複数
のビームで該サービスエリアを照射する受信用アンテナ
と受信信号を共通の中間周波数帯に変換増幅するM台の
受信器と該中間周波数帯の信号を相異なる送信信号に変
換増幅するN(M>N)台の送信器とシングルビームで
該サービスエリアを照射する送信用アンテナを備え、前
記受信器と送信器の間を相互に切替接続する中間周波数
帯M×Nスイッチマトリクスと地上からの監視制御信号
に基づいて一定のフレーム周期で該中間周波数帯スイッ
チマトリクスの切替接続状態の制御を行う制御回路を備
え、サービスエリア内の任意の地球局間の通信を中継す
ることを特徴とする衛星中継方式。In a satellite relay method that uses satellites to relay communications between earth stations within a service area, a receiving antenna that illuminates the service area with multiple beams and a receiving signal on the satellite are placed in a common intermediate frequency band. Equipped with M receivers that convert and amplify signals in the intermediate frequency band, N (M>N) transmitters that convert and amplify signals in the intermediate frequency band into different transmission signals, and a transmitting antenna that illuminates the service area with a single beam. , an intermediate frequency band M×N switch matrix that mutually switches and connects the receiver and transmitter, and control of the switching connection state of the intermediate frequency band switch matrix at a constant frame period based on a monitoring control signal from the ground; A satellite relay system that is equipped with a control circuit that performs this, and is characterized by relaying communications between arbitrary earth stations within a service area.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2370288A JPH01200732A (en) | 1988-02-05 | 1988-02-05 | Satellite repeating system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2370288A JPH01200732A (en) | 1988-02-05 | 1988-02-05 | Satellite repeating system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH01200732A true JPH01200732A (en) | 1989-08-11 |
Family
ID=12117706
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2370288A Pending JPH01200732A (en) | 1988-02-05 | 1988-02-05 | Satellite repeating system |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH01200732A (en) |
-
1988
- 1988-02-05 JP JP2370288A patent/JPH01200732A/en active Pending
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