JPH05335828A - Antenna for satellite communication for mobile body - Google Patents

Antenna for satellite communication for mobile body

Info

Publication number
JPH05335828A
JPH05335828A JP4142528A JP14252892A JPH05335828A JP H05335828 A JPH05335828 A JP H05335828A JP 4142528 A JP4142528 A JP 4142528A JP 14252892 A JP14252892 A JP 14252892A JP H05335828 A JPH05335828 A JP H05335828A
Authority
JP
Japan
Prior art keywords
output
azimuth
gyroscope
antenna
sensor
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
Application number
JP4142528A
Other languages
Japanese (ja)
Inventor
Yuuichi Shimobe
祐一 下部
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.)
NEC Corp
Original Assignee
NEC Corp
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 NEC Corp filed Critical NEC Corp
Priority to JP4142528A priority Critical patent/JPH05335828A/en
Publication of JPH05335828A publication Critical patent/JPH05335828A/en
Pending legal-status Critical Current

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  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Mobile Radio Communication Systems (AREA)
  • Radio Relay Systems (AREA)

Abstract

PURPOSE:To minimize line interruption and to simplify the structure of the equipment by deciding the azimuth by the earth magnetism and controlling the directivity of the antenna by a gyro scope so as to be in a prescribed azimuth thereby setting a communication line without a delay. CONSTITUTION:A computing element 3 compares the direction of the earth magnetism measured by an azimuth sensor 1 and a travelling direction of a mobile body measured by a gyro scope 2 prior to the system operation and an obtained azimuth is adopted when rates of change in the both are coincident over a prescribed time. Then the output of the sensor 1 and the output of the scope 2 are always compared and when a rate of a change in the output of the sensor 1 is larger, the output of the scope 2 is adopted to prevent malfunction due to disturbance in the earth magnetism and mechanical vibration. Furthermore, when a difference between the rate of changes in the output of the both is a prescribed value or below, the output of the sensor 1 is adopted to correct an accumulated error of the scope 2. Finally the output of the computing element 3 controls a driver 5 to direct the directive antenna 4 in a prescribed azimuth at all times.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は、移動体衛星通信に使用
され指向性アンテナの方位制御の機能を有する移動体衛
星通信用アンテナに関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a mobile satellite communication antenna used for mobile satellite communication and having a function of controlling the direction of a directional antenna.

【0002】[0002]

【従来の技術】従来の移動体用アンテナは無指向性か、
指向性を有する場合には受信電界強度が最大となるよう
にアンテナの指向性を制御している。移動体衛星通信で
は衛星が遠方にあるために、高利得のアンテナの使用が
通信品質の向上のために望ましいが、設置スペースやコ
ストから限界がある。
2. Description of the Related Art Is a conventional mobile antenna omnidirectional?
When the antenna has directivity, the antenna directivity is controlled so that the received electric field strength is maximized. In mobile satellite communication, the use of high-gain antennas is desirable for improving communication quality because the satellites are distant, but there is a limit in terms of installation space and cost.

【0003】一方、指向性アンテナは自動車等の移動体
の移動に従ってアンテナの指向性を常に衛星に向くよう
制御する必要があるので、アンテナから受信される電界
強度が最大となるように指向性を制御するのが一般的で
ある。しかしトンネルなどで電波の通路が遮蔽された場
合には、指向性の制御が出来なくなるので、遮蔽が解除
された状態になってから衛星を再捕捉して通信を行って
いた。
On the other hand, since the directional antenna needs to be controlled so that the directivity of the antenna is always directed toward the satellite in accordance with the movement of a moving body such as an automobile, the directivity is set so that the electric field strength received from the antenna becomes maximum. It is generally controlled. However, if the passage of the radio wave is blocked by a tunnel or the like, the directivity cannot be controlled, so the satellite was re-acquired and communication was performed after the shield was released.

【0004】[0004]

【発明が解決しようとする課題】上述したように従来の
移動体衛星通信アンテナは、衛星の再捕そくに時間がか
かる欠点がある。
As described above, the conventional mobile satellite communication antenna has a drawback that it takes time to reacquire satellites.

【0005】本発明の目的は、地磁気の乱れたところで
も、衛星からの電波の有無、伝搬路の遮蔽の有無にかか
わらず、アンテナの指向性を常に衛星に向けようとする
移動体の衛星通信アンテナを提供することにある。
The object of the present invention is to provide a satellite communication of a mobile body which always tries to direct the directivity of the antenna to the satellite regardless of the presence or absence of radio waves from the satellite and the presence or absence of shielding of the propagation path even when the geomagnetism is disturbed. To provide an antenna.

【0006】[0006]

【課題を解決するための手段】本発明の移動体衛星通信
用アンテナは移動体に搭載された指向性アンテナと、地
磁気により方位を測定する方位センサと、移動体の進行
方向を測定するジャイロスコープと、前記方位センサの
出力と前記ジャイロスコープの出力とを積算し比較する
演算器と、前記演算器からの出力によって指向性アンテ
ナを回転させる駆動装置とを有し、前記ジャイロスコー
プで移動体自身の進行方向を測定し、前記方位センサで
測定した地磁気の向きが安定している事を確認した上で
方位の決定をした後、前記ジャイロスコープの出力と前
記方位センサの出力との比較を行い前記方位センサの出
力の変化率と前記ジャイロスコープの出力の変化率との
差がある値以下の時には前記方位センサの出力を採用す
る事で、前記ジャイロスコープの累積誤差を補正する機
能を前記演算器に与える事で、前記方位センサの出力と
前記ジャイロスコープの出力との相互的な補正を行い、
移動体の向きによらず、常に一定の方位に前記指向性ア
ンテナの指向性が向く。
The antenna for mobile satellite communication according to the present invention is a directional antenna mounted on a mobile body, a direction sensor for measuring the direction by geomagnetism, and a gyroscope for measuring the traveling direction of the mobile body. And a computing unit that integrates and compares the output of the azimuth sensor and the output of the gyroscope, and a drive device that rotates a directional antenna by the output from the computing unit, and the moving body itself in the gyroscope. Of the gyroscope and the output of the azimuth sensor are compared after determining the azimuth after confirming that the direction of the geomagnetism measured by the azimuth sensor is stable. When the difference between the change rate of the output of the azimuth sensor and the change rate of the output of the gyroscope is less than or equal to a certain value, the output of the azimuth sensor is adopted, By providing the function of correcting the accumulated error Rosukopu the calculator performs mutual correction of the output of the output of the azimuth sensor gyroscope,
The directivity of the directional antenna is always oriented in a fixed direction regardless of the direction of the moving body.

【0007】[0007]

【実施例】次に本発明について図面を参照して説明す
る。
The present invention will be described below with reference to the drawings.

【0008】図1は本発明の一実施例のブロック図であ
る。図1の実施例は地磁気を用いた方位センサ1と、こ
の方位センサの出力とジャイロスコープ2の出力とを比
較する演算器3と、演算器3からの出力で指向性アンテ
ナ4を動かす駆動装置5とから構成される。
FIG. 1 is a block diagram of an embodiment of the present invention. In the embodiment shown in FIG. 1, an azimuth sensor 1 using geomagnetism, an arithmetic unit 3 for comparing the output of the azimuth sensor with the output of the gyroscope 2, and a driving device for moving the directional antenna 4 by the output from the arithmetic unit 3. 5 and.

【0009】次に本実施例の動作を説明する。まずこの
系を運用する前に、方位センサ1を用いて測定した地磁
気の向きと、ジャイロスコープ2を用いて測定した移動
体の進行方向とを演算器3で比較する。その結果、両者
の変化率が一定時間にわたって一致したときに、そこで
の地磁気が安定しているものと見なして、そのときに得
られた方位の値を採用する。
Next, the operation of this embodiment will be described. First, before operating this system, the calculator 3 compares the direction of the geomagnetism measured using the azimuth sensor 1 with the traveling direction of the moving body measured using the gyroscope 2. As a result, when the rates of change of both agree with each other for a certain period of time, it is considered that the geomagnetism there is stable, and the value of the azimuth obtained at that time is adopted.

【0010】その後、方位センサ1の出力とジャイロス
コープ2の出力とを常に比較し、方位センサ1の出力の
変化率が、ジャイロスコープ2によって得られた移動体
の進行方向の変化率に対して大きい場合には、ジャイロ
スコープ2の出力を採用する事で地磁気の乱れや機械的
振動による誤動作を防ぎ、また逆に、方位センサ1の出
力の変化率とジャイロスコープ2の出力の変化率との差
がある値以下の時には、方位センサ1の出力を採用し
て、ジャイロスコープ2の累積誤差を補正する。このよ
うな機能を演算器3に与える事で、方位センサ1の出力
とジャイロスコープ2の出力との相互的な補正を行う。
最終的に演算器3からの出力によって、駆動装置5を動
かし、指向性アンテナ4を常に一定の方位に向ける。
Thereafter, the output of the azimuth sensor 1 and the output of the gyroscope 2 are constantly compared, and the change rate of the output of the azimuth sensor 1 is compared with the change rate of the moving direction of the moving body obtained by the gyroscope 2. If it is larger, the output of the gyroscope 2 is adopted to prevent malfunction due to the disturbance of the earth's magnetism and mechanical vibration, and conversely, the change rate of the output of the azimuth sensor 1 and the change rate of the output of the gyroscope 2 are compared. When the difference is less than a certain value, the output of the azimuth sensor 1 is adopted to correct the accumulated error of the gyroscope 2. By giving the calculator 3 such a function, the output of the azimuth sensor 1 and the output of the gyroscope 2 are mutually corrected.
Finally, the drive unit 5 is moved by the output from the computing unit 3 and the directional antenna 4 is always oriented in a fixed direction.

【0011】なお、通信用の静止衛星は地上から3万キ
ロメートル程度離れており、通常の自動車等が移動する
数千キロメートルの範囲からは、ほぼ一定の方位に見え
ることになる。従って一定の方位に指向性を向けて置け
ば実用上差し支えない範囲で、通信衛星を捕そくするこ
とが可能となる。
The geostationary satellite for communication is distant from the ground by about 30,000 km, and it can be seen in a substantially constant azimuth in the range of several thousand km in which an ordinary automobile or the like moves. Therefore, if the directivity is placed in a certain direction, it is possible to capture the communication satellite within a range that is practically acceptable.

【0012】[0012]

【発明の効果】以上で説明したように本発明は、地磁気
によって方位を決定し、ジャイロスコープによってアン
テナの指向性を一定の方位に向けるように制御している
ので、衛星の捕そくに受信信号を必要としないから、通
信路の設定が時間遅れ無しに行える。また、通信路の遮
蔽による回線断を最小に出来る効果がある。
As described above, according to the present invention, the azimuth is determined by the geomagnetism and the gyroscope is controlled so that the directivity of the antenna is directed to a fixed azimuth. Since it is not necessary, the communication path can be set without a time delay. Further, there is an effect that the disconnection due to the blocking of the communication path can be minimized.

【0013】また、パケット通信の様に受信信号の発生
がバースト的であっても、受信信号による衛星捕そくの
方法を用いていないために、有効な通信が可能であると
いった効果に加え、使用する装置構造の単純化が図るこ
とができる効果がある。
In addition to the effect that effective communication is possible because the method of satellite acquisition by the received signal is not used even if the generation of the received signal is burst-like as in packet communication, it can be used. The effect is that the device structure can be simplified.

【図面の簡単な説明】[Brief description of drawings]

【図1】本発明の一実施例のブロック図である。FIG. 1 is a block diagram of an embodiment of the present invention.

【符号の説明】[Explanation of symbols]

1 方位センサ 2 ジャイロスコープ 3 演算器 4 指向性アンテナ 5 駆動装置 1 azimuth sensor 2 gyroscope 3 arithmetic unit 4 directional antenna 5 drive device

Claims (2)

【特許請求の範囲】[Claims] 【請求項1】 移動体に搭載された指向性アンテナと、
地磁気により方位を測定する方位センサと、移動体の進
行方向を測定するジャイロスコープと、前記方位センサ
の出力と前記ジャイロスコープの出力とを積算し比較す
る演算器と、前記演算器からの出力によって指向性アン
テナを回転させる駆動装置とを有し、前記ジャイロスコ
ープで移動体自身の進行方向を測定し、前記方位センサ
で測定した地磁気の向きが安定している事を確認した上
で方位の決定をした後、前記ジャイロスコープの出力と
前記方位センサの出力との比較を行い前記方位センサの
出力の変化率と前記ジャイロスコープの出力の変化率と
の差がある値以下の時には前記方位センサの出力を採用
する事で、前記ジャイロスコープの累積誤差を補正する
機能を前記演算器に与える事で、前記方位センサの出力
と前記ジャイロスコープの出力との相互的な補正を行
い、移動体の向きによらず、常に一定の方位に前記指向
性アンテナの方位が向く事を特徴とする移動体衛星通信
用アンテナ。
1. A directional antenna mounted on a mobile body,
An azimuth sensor that measures the azimuth by geomagnetism, a gyroscope that measures the traveling direction of the moving body, an arithmetic unit that integrates and compares the output of the azimuth sensor and the output of the gyroscope, and an output from the arithmetic unit It has a driving device for rotating a directional antenna, measures the traveling direction of the moving body itself with the gyroscope, and determines the azimuth after confirming that the direction of geomagnetism measured by the azimuth sensor is stable. After that, the output of the gyroscope and the output of the azimuth sensor are compared, and when the difference between the change rate of the output of the azimuth sensor and the change rate of the output of the gyroscope is less than or equal to a value, By adopting the output, by giving the arithmetic unit a function of correcting the accumulated error of the gyroscope, the output of the azimuth sensor and the gyroscope Performs mutual correction of the output of-loop, regardless of the orientation of the moving object, always mobile satellite communication antenna, characterized in that the facing is the orientation of the directional antenna in a certain azimuth.
【請求項2】 前記方位センサの出力の変化率と前記ジ
ャイロスコープの変化率が大きく異なるときには、前記
ジャイロスコープの出力を採用する事で、地磁気の乱れ
や機械的振動による誤動作を防ぐことを特徴とする請求
項1記載の移動体衛星通信用アンテナ。
2. When the rate of change of the output of the azimuth sensor and the rate of change of the gyroscope are significantly different, the output of the gyroscope is adopted to prevent malfunction due to disturbance of the geomagnetic field or mechanical vibration. The antenna for mobile satellite communication according to claim 1.
JP4142528A 1992-06-03 1992-06-03 Antenna for satellite communication for mobile body Pending JPH05335828A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP4142528A JPH05335828A (en) 1992-06-03 1992-06-03 Antenna for satellite communication for mobile body

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP4142528A JPH05335828A (en) 1992-06-03 1992-06-03 Antenna for satellite communication for mobile body

Publications (1)

Publication Number Publication Date
JPH05335828A true JPH05335828A (en) 1993-12-17

Family

ID=15317459

Family Applications (1)

Application Number Title Priority Date Filing Date
JP4142528A Pending JPH05335828A (en) 1992-06-03 1992-06-03 Antenna for satellite communication for mobile body

Country Status (1)

Country Link
JP (1) JPH05335828A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7783405B2 (en) 2004-11-05 2010-08-24 The Yokohama Rubber Co., Ltd. Tire ground contact pattern specifying method and apparatus thereof
US7970510B2 (en) 2004-11-05 2011-06-28 The Yokohama Rubber Co., Ltd. Vehicle drive control system and sensor unit and tire
CN103884352A (en) * 2014-03-15 2014-06-25 浙江大学 Method and device for automatically measuring output delay time of fiber-optic gyroscope
CN105157694A (en) * 2015-09-23 2015-12-16 浙江大学 Device and method for accurately evaluating output delay time of fiber-optic gyroscope

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7783405B2 (en) 2004-11-05 2010-08-24 The Yokohama Rubber Co., Ltd. Tire ground contact pattern specifying method and apparatus thereof
US7970510B2 (en) 2004-11-05 2011-06-28 The Yokohama Rubber Co., Ltd. Vehicle drive control system and sensor unit and tire
CN103884352A (en) * 2014-03-15 2014-06-25 浙江大学 Method and device for automatically measuring output delay time of fiber-optic gyroscope
CN105157694A (en) * 2015-09-23 2015-12-16 浙江大学 Device and method for accurately evaluating output delay time of fiber-optic gyroscope

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