JPH1090389A - Controller for satellite communication antenna - Google Patents

Controller for satellite communication antenna

Info

Publication number
JPH1090389A
JPH1090389A JP26385396A JP26385396A JPH1090389A JP H1090389 A JPH1090389 A JP H1090389A JP 26385396 A JP26385396 A JP 26385396A JP 26385396 A JP26385396 A JP 26385396A JP H1090389 A JPH1090389 A JP H1090389A
Authority
JP
Japan
Prior art keywords
antenna
satellite
control
communication
azimuth
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
JP26385396A
Other languages
Japanese (ja)
Inventor
Motoo Sato
基夫 佐藤
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.)
Japan Radio Co Ltd
Original Assignee
Japan Radio Co Ltd
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 Japan Radio Co Ltd filed Critical Japan Radio Co Ltd
Priority to JP26385396A priority Critical patent/JPH1090389A/en
Publication of JPH1090389A publication Critical patent/JPH1090389A/en
Pending legal-status Critical Current

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  • Position Fixing By Use Of Radio Waves (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)

Abstract

PROBLEM TO BE SOLVED: To make a controller for satellite communication antenna possible to automatically perform operations from the control of the attitude of an antenna to the tracking of a communication satellite by inputting the positional information, etc., of the satellite and antenna to an arithmetic and control unit and driving the azimuth, elevation, an polarization axes of the antenna with a control voltage. SOLUTION: An arithmetic and control unit 14 calculates the turning ranges of the azimuth, elevation, and polarization axes or an antenna until the antenna comes to oppositely face a target communication satellite from the positional information on the satellite from a target satellite data storing section 10 and the information on the latitude, longitude, azimuth, inclined angle of the antenna respectively sent from sensors 11-13. Then the unit 14 controls the attitude of the antenna by driving the shafts by outputting a control voltage to each shaft driving device 15-17. When the attitude control is terminated and the antenna is set to a state where the antenna can receive radio waves from the target communication satellite, satellite tracking operations are automatically started by utilizing the receiving field intensity of the radio waves. The satellite tracking operations are performed by performing feedback control which stops the antenna at the position where the receiving field intensity inputted from a receiving level input terminal 20 becomes the strongest by finely driving each axis by means of the devices 15-17.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】本発明は衛星通信アンテナ制
御装置、特に災害パトロール車両等に車載される衛星通
信用アンテナの位置制御(姿勢制御および衛星追尾)を
行う衛星通信アンテナ制御装置に関するものである。
The present invention relates to a satellite communication antenna control device, and more particularly to a satellite communication antenna control device for controlling the position (attitude control and satellite tracking) of a satellite communication antenna mounted on a disaster patrol vehicle or the like. .

【0002】[0002]

【従来の技術】災害パトロール車両には衛星通信装置を
搭載したものがあり、災害時や緊急事態が発生した場合
に直ちに現場へ直行し、現場の情況を衛星通信で本部等
へ通報する。このような災害パトロール車両でその通信
手段に衛星通信が利用されるのは、どのような現場でも
比較的確実に通信が行えるからであるが、衛星通信は静
止衛星(INTELSATや SCC)を利用していても電波の指向
性が比較的鋭いため、移動地球局となる車両側ではアン
テナの位置制御(姿勢制御および衛星追尾)を行って衛
星に正対させる必要がある。
2. Description of the Related Art Some disaster patrol vehicles are equipped with a satellite communication device. In the event of a disaster or emergency, the vehicle goes straight to the site immediately and reports the status of the site to the headquarters or the like by satellite communication. Such disaster patrol vehicles use satellite communication as their communication means because communication can be performed relatively reliably at any site, but satellite communication uses geostationary satellites (INTELSAT or SCC). However, since the directivity of the radio wave is relatively sharp, it is necessary for the vehicle serving as the mobile earth station to perform position control (attitude control and satellite tracking) of the antenna to face the satellite.

【0003】従来、衛星地球局でアンテナを衛星に正対
させるための装置としては、例えばロービング方式やモ
ノパルス方式を利用する自己追尾型の衛星追尾装置があ
るが、災害パトロール車両等では、災害現場に直行した
車両の屋上に取り付けられたアンテナの現在位置(緯
度,経度)や方位,傾斜角度等を事前に正確に知ること
が難しいため、自己追尾型の衛星追尾装置を使用する前
に、衛星からの電波が入る位置にアンテナを向けてやる
姿勢制御が必要になる。従来このアンテナの姿勢制御
は、専ら外部のセンサー情報を用いて車両の位置や方
位,停止角度の情報を得、この情報を用いて手動で衛星
からの電波が入る位置にアンテナを動かしている。
Conventionally, a self-tracking type satellite tracking device using a roving method or a monopulse method has been used as a device for directly pointing an antenna to a satellite at a satellite earth station. Before using a self-tracking type satellite tracking device, it is difficult to know the current position (latitude, longitude), azimuth, inclination angle, etc. of an antenna mounted on the roof of a vehicle that goes straight to It is necessary to control the attitude of pointing the antenna to the position where radio waves from the antenna enter. Conventionally, in attitude control of this antenna, information on the position, direction, and stop angle of the vehicle is obtained exclusively using external sensor information, and the antenna is manually moved to a position where radio waves from a satellite can be input using this information.

【0004】[0004]

【発明が解決しようとする課題】上記のように従来で
は、災害パトロール車両等に車載される衛星通信のアン
テナの姿勢制御は、専ら外部のセンサー情報を用いて行
っているが、外部のセンサー情報でアンテナを一軸ずつ
試行錯誤しながら行わなければならず、この作業は容易
でない。特に外部センサーで計測した情報を用いる場
合、センサーの本来の誤差の他に、アンテナと外部セン
サーとの位置の相違からくる誤差も含まれるため、特に
この作業が困難なものになり、利用者に無駄な作業を強
いると共に、緊急通報の遅れにつながる等の問題点があ
った。
As described above, in the prior art, the attitude control of a satellite communication antenna mounted on a disaster patrol vehicle or the like is performed exclusively using external sensor information. This operation is not easy because the antenna must be performed by trial and error for each axis. In particular, when using information measured by an external sensor, in addition to the original error of the sensor, errors due to differences in the positions of the antenna and the external sensor are also included, making this task particularly difficult, and making it difficult for users. There was a problem in that unnecessary work was forced and an emergency call was delayed.

【0005】本発明はかかる問題点を解決するためにな
されたものであり、例えば災害パトロール車両等に車載
され、その車両がどのような場所でどのような状態にあ
っても自動的にアンテナの位置制御(姿勢制御および衛
星追尾)を行い、アンテナを通信衛星に正対させること
ができる衛星通信アンテナ制御装置を提供することを目
的としている。
The present invention has been made in order to solve such a problem. For example, the present invention is mounted on a disaster patrol vehicle or the like, and the antenna is automatically installed regardless of the vehicle position and state. It is an object of the present invention to provide a satellite communication antenna control device capable of performing position control (attitude control and satellite tracking) and pointing an antenna directly to a communication satellite.

【0006】[0006]

【課題を解決するための手段】本発明に係わる衛星通信
アンテナ制御装置は、移動して任意の状態におかれた衛
星通信用アンテナを目標とする通信衛星に正対させる場
合に、始めにアンテナの姿勢制御を行い、当該アンテナ
で目標とする通信衛星からの電波を受信できるようにな
ると、次に受信した電波の受信電界強度を利用して衛星
追尾動作を行う衛星通信アンテナ制御装置において、装
置を構成する演算制御装置に少なくとも、目標とする通
信衛星の位置情報と、任意の状態におかれたアンテナの
位置(緯度,経度)情報,方位情報,傾斜角情報と、目
標とする通信衛星からの電波の受信電界強度の情報とを
入力する手段と、上記演算制御装置からの制御電圧によ
り、当該アンテナの方位軸,仰角軸,偏波軸をそれぞれ
駆動する手段とを備え、上記アンテナの姿勢制御から衛
星追尾動作までを自動で行う構成としたものである。
SUMMARY OF THE INVENTION A satellite communication antenna control apparatus according to the present invention, when a mobile communication antenna is placed in an arbitrary state and directly faces a target communication satellite, an antenna for controlling the antenna is first used. When the antenna can receive the radio wave from the target communication satellite with the antenna, the satellite communication antenna control device that performs the satellite tracking operation by using the received electric field strength of the next received radio wave includes the device. At least the target communication satellite position information, the antenna position (latitude and longitude) information, the azimuth information, the tilt angle information in an arbitrary state, and the target communication satellite Means for inputting information on the received electric field strength of the radio wave of the antenna and means for driving the azimuth axis, the elevation angle axis, and the polarization axis of the antenna by the control voltage from the arithmetic and control unit. For example, it is obtained by the arrangement performed automatically until the satellite tracking operation from the attitude control of the antenna.

【0007】また、上記アンテナのアンテナベースが固
定される車両に車載されることを特徴とする。さらに、
キーボードやタッチパネルで構成される対話型入力装置
を備えたことを特徴とする。
The antenna is mounted on a vehicle to which the antenna base of the antenna is fixed. further,
An interactive input device including a keyboard and a touch panel is provided.

【0008】[0008]

【発明の実施の形態】以下、本発明の実施形態を図面を
用いて説明する。図1は本発明の衛星通信アンテナ制御
装置の構成の一実施形態を示すブロック図であり、図に
おいて、10は通信に使用する衛星の位置情報を格納し
ている目標衛星データ格納部、11はアンテナの現在の
設置方位(車両にアンテナベースが固定されている場合
には車両の方位、以下同様)を計測する磁気方位センサ
ー、12は同じく設置傾斜角を計測する傾斜角センサ
ー、13は同じく設置位置(緯度,経度)を計測するG
PS測位センサーである。なお、磁気方位センサー11
および傾斜角センサー12には、ジャイロセンサーを用
いることができる。
Embodiments of the present invention will be described below with reference to the drawings. FIG. 1 is a block diagram showing an embodiment of the configuration of a satellite communication antenna control apparatus according to the present invention. In FIG. 1, reference numeral 10 denotes a target satellite data storage unit that stores position information of satellites used for communication, and 11 denotes a satellite data storage unit. Magnetic orientation sensor that measures the current installation orientation of the antenna (orientation of the vehicle if the antenna base is fixed to the vehicle, the same applies hereinafter), 12 is an inclination angle sensor that measures the installation inclination angle, and 13 is the same. G to measure position (latitude, longitude)
It is a PS positioning sensor. The magnetic direction sensor 11
A gyro sensor can be used for the tilt angle sensor 12.

【0009】また14は演算制御装置、15はアンテナ
の方位軸駆動装置、16はアンテナの仰角軸駆動装置、
17はアンテナの偏波軸駆動装置、18はキーボードや
タッチパネル等で構成された対話型入力装置、19はモ
ニタ、20はアンテナ受信レベルが入力される受信レベ
ル入力端である。方位軸駆動装置15,仰角軸駆動装置
16,偏波軸駆動装置17は、例えばサーボアンプ15
1,駆動モータ152,エンコーダ153等で構成さ
れ、それぞれの軸を演算制御装置14からの駆動電圧に
よりフィードバック制御で駆動するように構成されてい
る。
Further, 14 is an arithmetic and control unit, 15 is an azimuth axis driving device of the antenna, 16 is an elevation axis driving device of the antenna,
Reference numeral 17 denotes a polarization axis driving device for the antenna, reference numeral 18 denotes an interactive input device including a keyboard, a touch panel, and the like, reference numeral 19 denotes a monitor, and reference numeral 20 denotes a reception level input terminal to which an antenna reception level is input. The azimuth axis drive device 15, the elevation angle drive device 16, and the polarization axis drive device 17 are, for example, servo amplifiers 15
1, a drive motor 152, an encoder 153, etc., and each axis is driven by a drive voltage from the arithmetic and control unit 14 by feedback control.

【0010】次に動作について説明する。この種のアン
テナには一般的にオフセットパラボラアンテナが用いら
れ、アンテナの姿勢制御には方位軸を駆動してアンテナ
ベースを回転させてアンテナの方位角を決定し、仰角軸
を駆動して主反射鏡(アンテナディッシュとも言う)を
回転させてアンテナの仰角を決定し、一次放射器の偏波
軸を回転させて偏波角を決定する。従ってこの種のアン
テナの姿勢制御および衛星追尾は、この方位軸,仰角軸
および偏波軸を駆動して行われるが、本発明の衛星通信
アンテナ制御装置は、目標衛星データ入力部10から入
力される衛星の位置情報と、現在おかれているアンテナ
の緯度,経度、方位角、傾斜角の情報とから、演算制御
装置14でアンテナが通信衛星と正対するまでの方位
軸,仰角軸,偏波軸の回動範囲を算出し、それぞれの軸
駆動装置15〜17に制御電圧を出力し、各軸駆動装置
15〜17を駆動してアンテナの姿勢制御を行う。
Next, the operation will be described. Generally, an offset parabolic antenna is used for this type of antenna, and the azimuth axis is driven to rotate the antenna base to determine the azimuth angle of the antenna, and the main reflection is performed by driving the elevation axis for the attitude control of the antenna. A mirror (also called an antenna dish) is rotated to determine the elevation angle of the antenna, and the polarization axis of the primary radiator is rotated to determine the polarization angle. Therefore, this kind of antenna attitude control and satellite tracking are performed by driving the azimuth axis, elevation axis and polarization axis. The satellite communication antenna control device of the present invention is input from the target satellite data input unit 10. Azimuth axis, elevation axis, and polarization until the antenna is directly opposed to the communication satellite by the arithmetic and control unit 14 from the position information of the current satellite and the information of the latitude, longitude, azimuth angle, and inclination angle of the currently placed antenna. The rotation range of the shaft is calculated, a control voltage is output to each of the shaft driving devices 15 to 17, and each of the shaft driving devices 15 to 17 is driven to control the attitude of the antenna.

【0011】図2は、タッチパネルで構成された対話型
入力装置18のメインメニューの表示例を示す図であ
り、例えば電源投入後の動作開始時には、「自動運
転」,「手動運転」,「キー入力運転」,「衛星選択」
等のメニューが表示される。ここで使用者が自動運転3
0を選択した場合には、既に選択されている、あるいは
装置自身が最適と判断した通信衛星の位置情報が目標衛
星データ格納部10から演算制御装置14へ入力され、
上述のようにアンテナの姿勢制御が自動で行われる。
FIG. 2 is a diagram showing a display example of a main menu of the interactive input device 18 constituted by a touch panel. For example, at the start of operation after turning on the power, "automatic operation", "manual operation", "key" Input operation ”,“ Satellite selection ”
Is displayed. Here, the user automatically drives 3
When 0 is selected, the position information of the communication satellite that has already been selected or that the device itself has determined to be optimal is input from the target satellite data storage unit 10 to the arithmetic and control unit 14,
As described above, the attitude control of the antenna is automatically performed.

【0012】また、使用者がアンテナの姿勢制御を従来
と同様に手動で行いたい場合には、手動運転メニュー3
1を選択する。また、例えば方位センサー11,傾斜角
センサー12,GPS測位センサー13の何れかから情
報が入力できない場合には、キー入力運転メニュー32
を選択して、他の手段から得たこれらの情報を入力す
る。
If the user wants to manually control the attitude of the antenna in the same manner as in the prior art, the manual operation menu 3
Select 1. For example, when information cannot be input from any of the azimuth sensor 11, the inclination angle sensor 12, and the GPS positioning sensor 13, the key input operation menu 32
And enter these information obtained from other means.

【0013】このようにアンテナの姿勢制御を終了し、
目標とする通信衛星からの電波が入力できる状態になる
と、この電波の受信電界強度を利用して自動的に衛星追
尾動作に移行する。この衛星追尾動作は、演算制御装置
14が各軸駆動装置15〜17で各軸を微少駆動させ
て、受信レベル入力端20から入力される受信電界強度
が1番強い位置で停止させるフィードバック制御により
行う。
Thus, the attitude control of the antenna is completed,
When a radio wave from the target communication satellite can be input, the operation automatically shifts to the satellite tracking operation using the received electric field strength of the radio wave. The satellite tracking operation is performed by feedback control in which the arithmetic and control unit 14 minutely drives each axis by each of the axis driving devices 15 to 17 and stops at a position where the reception electric field intensity input from the reception level input terminal 20 is the strongest. Do.

【0014】[0014]

【発明の効果】以上説明したように本発明の衛星通信ア
ンテナ制御装置は、少なくとも現在のアンテナの位置
(緯度・経度),方位,傾斜角の情報と、目標とする衛
星の位置情報とを入力してアンテナの方位軸と仰角軸と
偏波軸とを駆動させてアンテナの姿勢制御を自動で行
い、目標とする衛星からの電波を受信できるようになる
と、この電波の受信電界強度の情報を用いてアンテナの
方位軸と仰角軸と偏波軸とを微小駆動させて、目標の衛
星に正対させる衛星追尾を自動的に行わせることとした
ので、災害パトロール車両等に車載して災害現場で行う
衛星通信においても、アンテナの姿勢制御から衛星追尾
までの動作を自動で行わせることができ、使用者の負担
を大幅に軽減できると共に、緊急通報の遅れを回避でき
る等の効果がある。また、常にアンテナの姿勢制御と衛
星追尾とを行わせることができるので、車載した車両の
走行中にも通信衛星を用いた通信が可能となる等の効果
がある。
As described above, the satellite communication antenna control apparatus of the present invention receives at least information on the current antenna position (latitude / longitude), azimuth, inclination angle, and target satellite position information. When the azimuth axis, elevation axis, and polarization axis of the antenna are driven to automatically control the attitude of the antenna, and it becomes possible to receive radio waves from the target satellite, information on the received electric field strength of this radio wave is obtained. The azimuth axis, elevation axis, and polarization axis of the antenna are finely driven to automatically perform satellite tracking to face the target satellite, so it is mounted on a disaster patrol vehicle etc. Also in the satellite communication performed by, the operations from the attitude control of the antenna to the tracking of the satellite can be automatically performed, so that the burden on the user can be greatly reduced and the delay of the emergency call can be avoided. In addition, since the attitude control of the antenna and the satellite tracking can be always performed, there is an effect that the communication using the communication satellite can be performed even while the vehicle mounted on the vehicle is running.

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

【図1】本発明の装置構成の一実施形態を示すブロック
図である。
FIG. 1 is a block diagram showing an embodiment of the device configuration of the present invention.

【図2】対話型入力装置のメインメニューの表示例を示
す図である。
FIG. 2 is a diagram illustrating a display example of a main menu of the interactive input device.

【符号の説明】[Explanation of symbols]

10 目標衛星データ格納部 11 方位センサー 12 傾斜角センサー 13 測位センサー 14 演算制御装置 15 方位軸駆動装置 16 仰角軸駆動装置 17 偏波軸駆動装置 18 対話型入力装置 19 モニタ 20 受信レベル入力端 DESCRIPTION OF SYMBOLS 10 Target satellite data storage part 11 Azimuth sensor 12 Tilt angle sensor 13 Positioning sensor 14 Arithmetic control device 15 Azimuth axis drive device 16 Elevation axis drive device 17 Polarization axis drive device 18 Interactive input device 19 Monitor 20 Reception level input terminal

Claims (3)

【特許請求の範囲】[Claims] 【請求項1】 移動して任意の状態におかれた衛星通信
用アンテナを目標とする通信衛星に正対させる場合に、
始めにアンテナの姿勢制御を行い、当該アンテナで目標
とする通信衛星からの電波を受信できるようになると、
次に受信した電波の受信電界強度を利用して衛星追尾動
作を行う衛星通信アンテナ制御装置において、 装置を構成する演算制御装置に少なくとも、目標とする
通信衛星の位置情報と、任意の状態におかれたアンテナ
の位置(緯度,経度)情報,方位情報,傾斜角情報と、
目標とする通信衛星からの電波の受信電界強度の情報と
を入力する手段と、 上記演算制御装置からの制御電圧により、当該アンテナ
の方位軸,仰角軸,偏波軸をそれぞれ駆動する手段とを
備え、 上記アンテナの姿勢制御から衛星追尾動作までを自動で
行う衛星通信アンテナ制御装置。
When a mobile communication antenna that is moved and placed in an arbitrary state is directly opposed to a target communication satellite,
First, control the attitude of the antenna, and when the antenna can receive radio waves from the target communication satellite,
Next, in a satellite communication antenna control device that performs a satellite tracking operation using the received electric field strength of a received radio wave, at least a position information of a target communication satellite and an arbitrary state are provided to an arithmetic and control unit constituting the device. Position (latitude, longitude) information, azimuth information, tilt angle information of the placed antenna,
Means for inputting information on the received electric field strength of a radio wave from a target communication satellite; and means for driving the azimuth axis, elevation angle axis, and polarization axis of the antenna with a control voltage from the arithmetic and control unit. A satellite communication antenna control device for automatically performing from the attitude control of the antenna to the satellite tracking operation.
【請求項2】 上記アンテナのアンテナベースが固定さ
れる車両に車載されることを特徴とする請求項第1項記
載の衛星通信アンテナ制御装置。
2. The satellite communication antenna control device according to claim 1, wherein the antenna communication device is mounted on a vehicle to which an antenna base of the antenna is fixed.
【請求項3】キーボードやタッチパネルで構成される対
話型入力装置を備えたことを特徴とする請求項第1項,
第2項記載の衛星通信アンテナ制御装置。
3. An apparatus according to claim 1, further comprising an interactive input device comprising a keyboard and a touch panel.
3. The satellite communication antenna control device according to claim 2.
JP26385396A 1996-09-13 1996-09-13 Controller for satellite communication antenna Pending JPH1090389A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP26385396A JPH1090389A (en) 1996-09-13 1996-09-13 Controller for satellite communication antenna

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP26385396A JPH1090389A (en) 1996-09-13 1996-09-13 Controller for satellite communication antenna

Publications (1)

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JPH1090389A true JPH1090389A (en) 1998-04-10

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JP2009284458A (en) * 2008-04-25 2009-12-03 Mitsubishi Electric Corp Antenna attitude control device
JP4535187B2 (en) * 2008-04-25 2010-09-01 三菱電機株式会社 Antenna attitude control device
JP2013005277A (en) * 2011-06-17 2013-01-07 Mitsubishi Electric Corp Antenna polarization angle error calculation method and antenna polarization angle control device
WO2015001848A1 (en) * 2013-07-03 2015-01-08 三菱電機株式会社 Tracking system, tracking method, and program
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