JPH03286629A - Communication system - Google Patents
Communication systemInfo
- Publication number
- JPH03286629A JPH03286629A JP8493390A JP8493390A JPH03286629A JP H03286629 A JPH03286629 A JP H03286629A JP 8493390 A JP8493390 A JP 8493390A JP 8493390 A JP8493390 A JP 8493390A JP H03286629 A JPH03286629 A JP H03286629A
- Authority
- JP
- Japan
- Prior art keywords
- station
- signal
- pilot
- level
- transmission
- 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
- 238000004891 communication Methods 0.000 title claims abstract description 35
- 230000005540 biological transmission Effects 0.000 claims abstract description 37
- 238000005259 measurement Methods 0.000 description 4
- 238000001514 detection method Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000002238 attenuated effect Effects 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
Landscapes
- Radio Relay Systems (AREA)
Abstract
Description
【発明の詳細な説明】
[庁業上の利用分野]
本発明は、第1及び第2の小型地球局を6゛シ、前記第
1及び前記第2の小型地球局か一つの通信衛星を介して
相互に通信を行う通信方式に関する。[Detailed Description of the Invention] [Field of Industrial Application] The present invention provides a first and a second small earth station, and a communication satellite between the first and second small earth stations. The present invention relates to a communication method for mutually communicating through a communication network.
[従来の技術]
小型地球局間の通信衛星を介して行う通信は、自局及び
通信相手方の気象条件、地理的、機能的条件等の差異に
より、受信レベルが様々に変化する。従って、小型地球
局において、最適な受信状態にするためには、一般に、
該小型地球局の受信機に、AGC(自動利得調整)回路
やリミタ回路を使用している。[Prior Art] In communications between small earth stations via communication satellites, reception levels vary depending on differences in weather conditions, geographic conditions, functional conditions, etc. between the local station and the communication partner. Therefore, in order to achieve optimal reception conditions at a small earth station, generally
The receiver of the small earth station uses an AGC (automatic gain control) circuit and a limiter circuit.
[発明か解決しようとする課題]
しかし、これら受信機側におけるAGCやリミタ処理は
、受信レベルの補正こそすれ、受f!機入力端における
信号対雑音電力比の改善をすることは不可能であった。[Problem to be solved by the invention] However, these AGC and limiter processing on the receiver side only correct the reception level, and the reception f! It was not possible to improve the signal-to-noise power ratio at the machine input end.
本発明の課題は、信号対雑音電力比の改善をすることか
可能な通信方式を提供することにある。An object of the present invention is to provide a communication system that can improve the signal-to-noise power ratio.
[課題を解決するための手段]
本発明によれば、
第1及び第2の地球局を有し、前記第1及び前記第2の
地球局が一つの通信衛星を介して相互に通信を行う通信
方式において、
一定送信レベルのパイロット信号を、常時、送信するパ
イロット局を設け、
前記第1及び前記第2の地球局の各々は、前記パイロッ
ト信号か前記通信衛星にて折り返されたパイロット折り
返し信号と、自局が送信した送信信号が前記通信衛星に
て折り返された自局折り返し信号とを受信し、前記パイ
ロット折り返し信号の受信レベルから前記自局折り返し
信号の受信レヘルを減算して得られた差が、予め定めら
れた差に等しくなるように、自局の前記送信信号の送信
レベルを調整する送信レベル調整回路を有することを特
徴とする通信方式が得られる。[Means for Solving the Problems] According to the present invention, there is provided a first and second earth station, and the first and second earth stations communicate with each other via one communication satellite. In the communication system, a pilot station is provided that always transmits a pilot signal at a constant transmission level, and each of the first and second earth stations transmits either the pilot signal or a pilot return signal returned by the communication satellite. and a local station return signal in which the transmission signal transmitted by the own station is looped back by the communication satellite, and is obtained by subtracting the reception level of the own station return signal from the reception level of the pilot return signal. A communication system is obtained that is characterized by having a transmission level adjustment circuit that adjusts the transmission level of the transmission signal of its own station so that the difference is equal to a predetermined difference.
[作用]
本発明では、地球局からの上り回線上で、例えば、降雨
減衰などによるレベル変動があった場合、送信電力を増
加することてレベル変動を補償する。[Operation] In the present invention, when there is a level fluctuation due to rain attenuation, for example, on the uplink from the earth station, the level fluctuation is compensated for by increasing the transmission power.
従って、上り回線における信号対雑音電力比は一定に保
たれ、従来の受信機側におけるレベル補償に比べ受信特
性を改善できる。Therefore, the signal-to-noise power ratio in the uplink is kept constant, and reception characteristics can be improved compared to conventional level compensation on the receiver side.
[実施例]
次に、本発明の実施例について、図面を参照して説明す
る。[Example] Next, an example of the present invention will be described with reference to the drawings.
第1図を参照すると、本発明の一実施例による通信方式
は、第1及び第2の小型地球局11及び12を有し、第
1及び第2の小型地球局11及び12が通信衛星13を
介して相互に通信を行う。Referring to FIG. 1, the communication system according to one embodiment of the present invention has first and second small earth stations 11 and 12, and the first and second small earth stations 11 and 12 are connected to a communication satellite 13. communicate with each other via.
もちろん、第1及び第2の小型地球局11及び12と通
信衛星13を介して通信可能な第3及び第4の小型地球
局が存在しても良い。Of course, there may also be third and fourth small earth stations that can communicate with the first and second small earth stations 11 and 12 via the communication satellite 13.
パイロット局14は、通信衛星13に対して一ツ設ケら
れ、一定送信レベルのパイロット信号を、常時、送信す
る。One pilot station 14 is provided for each communication satellite 13, and always transmits a pilot signal at a constant transmission level.
第1及び第2の小型地球局11及び12の各々は、前記
パイロット信号が通信衛星13にて折り返されたパイロ
ット折り返し信号と、自局か送信した送信信号か通信衛
星13にて折り返された自局折り返し信号とを受信し、
前記パイロット折り返し信号の受信レベルから前記自局
折り返し信号の受信レヘルを減算して得られた差が、予
め定められた基準レヘル差20に等しくなるように、自
局の前記送信信号の送信レベルを調整する後述の送信レ
ヘル調整回路(第2図の10)を有している。Each of the first and second small earth stations 11 and 12 receives a pilot return signal in which the pilot signal is returned by the communication satellite 13, and a transmission signal transmitted by the own station or an own return signal obtained by returning the pilot signal by the communication satellite 13. receive the station return signal,
The transmission level of the transmission signal of the own station is set such that the difference obtained by subtracting the reception level of the own station return signal from the reception level of the pilot return signal is equal to a predetermined reference level difference 20. It has a transmission level adjustment circuit (10 in FIG. 2) which will be described later for adjustment.
なお、本実施例では、前記通信方式としてTDMA方式
を想定しており、小型地球局11及び12やパイロット
局14は、信号送信の際に、送信元コードを含むユニー
クワードを送信しており、受信局では、受信信号から前
記ユニークワードを検出することにより、受信信号の発
信元か識別できるものとする。In this embodiment, the TDMA method is assumed as the communication method, and the small earth stations 11 and 12 and the pilot station 14 transmit a unique word including a source code when transmitting a signal. The receiving station can identify the source of the received signal by detecting the unique word from the received signal.
第2図を参照すると、小型地球局11及び12の各々に
おける前記送信レベル調整回路10は、受信回路15と
、受信レベル検出回路16と、レベル差測定回路17と
、送信レベル設定回路18と、送信回路19とを有して
いる。Referring to FIG. 2, the transmission level adjustment circuit 10 in each of the small earth stations 11 and 12 includes a reception circuit 15, a reception level detection circuit 16, a level difference measurement circuit 17, a transmission level setting circuit 18, It has a transmitting circuit 19.
各小型地球局では、受信回路15て受信される各バース
ト信号のうち、前記パイロット折り返し信号の受信レベ
ル及び前記自局折り返し信号の受信レベルを受信レベル
検出回路16で検出する。In each small earth station, a reception level detection circuit 16 detects the reception level of the pilot return signal and the own station return signal among the burst signals received by the reception circuit 15.
レベル差測定回路17は、前記パイロット折り返し信号
の受信レベルから前記自局折り返し信号の受信レベルを
減算して得られた差を、測定レベル差として出力する。The level difference measurement circuit 17 subtracts the reception level of the local station return signal from the reception level of the pilot return signal and outputs the difference obtained as a measured level difference.
送信レベル設定回路18は、レベル差測定回路17て得
られたレヘル差と、予め定められた基準レヘル差20と
を、比較し、比較結果を基に自局送信レヘルを増域して
送信回路1つの出力レベルを規定する。The transmission level setting circuit 18 compares the level difference obtained by the level difference measurement circuit 17 with a predetermined reference level difference 20, increases the own station's transmission level based on the comparison result, and sets the transmitting circuit. Defines one output level.
即ち、送信回路19は、前記測定レヘル差が基準レヘル
差20に比べて、小さいときは、自局送信レヘルを増加
させ、逆の場合は、1局送信レベルを減少させる。換言
すれば、送信回路19は、前記測定レベル差が基準レベ
ル差20になるように自局送信レベルを制御する。That is, when the measured level difference is smaller than the reference level difference 20, the transmitting circuit 19 increases the own station transmission level, and in the opposite case, decreases the one station transmission level. In other words, the transmission circuit 19 controls the transmission level of its own station so that the measured level difference becomes the reference level difference 20.
なお、パイロット局14は、自局装置の送信レベル変動
や自局周辺の降雨減衰などによるレベル変動を予め補償
しているものとする。It is assumed that the pilot station 14 compensates in advance for level fluctuations due to transmission level fluctuations of its own station equipment, rain attenuation around the own station, and the like.
その結果、小型地球局11或いは12から送信され、通
信衛星13にて折り返された信号の小型地球局での受信
レベルは、いかなる地球局から見てもパイロット信号を
基準に一定のレベル差となる。As a result, the reception level at the small earth station of the signal transmitted from the small earth station 11 or 12 and returned by the communication satellite 13 will have a certain level difference based on the pilot signal, no matter what earth station it is looking at. .
再び第1図を参照して、本実施例の通信方式の動作を説
明する。パイロット局14は、通信の有無にかかわらず
、常にパイロット信号の送信を行っている。今、小型地
球局11及び12が通信しているものとすると、小型地
球局11は前述の送信レベル調整回路10で自局の送信
レベルを調整しているため、小型地球局12からみると
、小型地球局11から通信衛星13を介して小型地球局
12か受信した受信信号は、パイロット信号を基準に、
ある一定レベルとなっている。Referring again to FIG. 1, the operation of the communication system of this embodiment will be explained. The pilot station 14 always transmits pilot signals regardless of the presence or absence of communication. Assuming that the small earth stations 11 and 12 are currently communicating, the small earth station 11 adjusts its own transmission level using the above-mentioned transmission level adjustment circuit 10, so from the perspective of the small earth station 12, The received signal received by the small earth station 12 from the small earth station 11 via the communication satellite 13 is based on the pilot signal.
It is at a certain level.
この時、小型地球局11の周辺で降雨減衰があると、小
型地球局11の上り信号は通信衛星13に到達するまで
に減衰をうけるが、小型地球局11は前述の送信レベル
調整回路10で自局の送信電力を増加するので、折り返
し信号がパイロット信号を基準に一定レベルに保たれる
。At this time, if there is rain attenuation around the small earth station 11, the upstream signal of the small earth station 11 will be attenuated before reaching the communication satellite 13. Since the transmission power of the own station is increased, the return signal is maintained at a constant level with respect to the pilot signal.
従って、小型地球局12から見れば小型地球局11の周
辺の降雨減衰の影響は全くなく、信号対雑音電力比も一
定である。Therefore, from the perspective of the small earth station 12, there is no effect of rain attenuation around the small earth station 11, and the signal-to-noise power ratio is also constant.
[発明の効果]
以上説明したように、本発明によれば、地球局からの上
り回線上てレベル変動があっても、上り回線における信
号対雑音電力比は一定に保たれ、従来の受信機側におけ
るレベル補償に比べ受信特性を改善できる。[Effects of the Invention] As explained above, according to the present invention, even if there is a level fluctuation on the uplink from the earth station, the signal-to-noise power ratio on the uplink is kept constant, and the conventional receiver The reception characteristics can be improved compared to level compensation on the side.
第1図は本発明の一実施例による通信方式のブロック図
、第2図は第1図の通信方式の小型地球局の各々におけ
る送信レベル調整回路のブロック図である。
11及び12は小型地球局、13は通信衛星、14はパ
イロット局、10は送信レベル調整回路、15は受信回
路、16は受信レベル検出回路、17はレベル差測定回
路、18は送信レベル設定回路、19は送信回路、20
は基準レベル差。
jll 図
1N2図
1つ
8FIG. 1 is a block diagram of a communication system according to an embodiment of the present invention, and FIG. 2 is a block diagram of a transmission level adjustment circuit in each of the small earth stations of the communication system of FIG. 1. 11 and 12 are small earth stations, 13 is a communication satellite, 14 is a pilot station, 10 is a transmission level adjustment circuit, 15 is a reception circuit, 16 is a reception level detection circuit, 17 is a level difference measurement circuit, and 18 is a transmission level setting circuit. , 19 is a transmitting circuit, 20
is the reference level difference. jll Figure 1N2 Figure 1 8
Claims (1)
2の地球局が一つの通信衛星を介して相互に通信を行う
通信方式において、 一定送信レベルのパイロット信号を、常時、送信するパ
イロット局を設け、 前記第1及び前記第2の地球局の各々は、前記パイロッ
ト信号が前記通信衛星にて折り返されたパイロット折り
返し信号と、自局が送信した送信信号が前記通信衛星に
て折り返された自局折り返し信号とを受信し、前記パイ
ロット折り返し信号の受信レベルから前記自局折り返し
信号の受信レベルを減算して得られた差が、予め定めら
れた差に等しくなるように、自局の前記送信信号の送信
レベルを調整する送信レベル調整回路を有することを特
徴とする通信方式。[Claims] A communication system comprising: 1, a first earth station, and a second earth station, wherein the first earth station and the second earth station communicate with each other via one communication satellite, comprising: a constant transmission level; A pilot station is provided that always transmits a pilot signal, and each of the first and second earth stations transmits a pilot return signal obtained by returning the pilot signal by the communication satellite, and a pilot return signal transmitted by the own station. A difference obtained by subtracting the reception level of the own station return signal from the reception level of the pilot return signal by receiving the transmission signal and the return signal of the own station returned by the communication satellite is determined in advance. A communication system comprising a transmission level adjustment circuit that adjusts the transmission level of the transmission signal of its own station so that the difference is equal to the difference.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP8493390A JPH03286629A (en) | 1990-04-02 | 1990-04-02 | Communication system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP8493390A JPH03286629A (en) | 1990-04-02 | 1990-04-02 | Communication system |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH03286629A true JPH03286629A (en) | 1991-12-17 |
Family
ID=13844484
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP8493390A Pending JPH03286629A (en) | 1990-04-02 | 1990-04-02 | Communication system |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH03286629A (en) |
-
1990
- 1990-04-02 JP JP8493390A patent/JPH03286629A/en active Pending
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