JPH0613810A - Antenna controller - Google Patents

Antenna controller

Info

Publication number
JPH0613810A
JPH0613810A JP15719392A JP15719392A JPH0613810A JP H0613810 A JPH0613810 A JP H0613810A JP 15719392 A JP15719392 A JP 15719392A JP 15719392 A JP15719392 A JP 15719392A JP H0613810 A JPH0613810 A JP H0613810A
Authority
JP
Japan
Prior art keywords
satellite
antenna
search
angular velocity
signal
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.)
Granted
Application number
JP15719392A
Other languages
Japanese (ja)
Other versions
JP3087453B2 (en
Inventor
Yasunori Yoshino
康則 吉野
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 JP04157193A priority Critical patent/JP3087453B2/en
Publication of JPH0613810A publication Critical patent/JPH0613810A/en
Application granted granted Critical
Publication of JP3087453B2 publication Critical patent/JP3087453B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Landscapes

  • Control Of Position Or Direction (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)

Abstract

PURPOSE:To shorten the searching time of a satellite and also to ensure the stable reception with an antenna by compensating the rotational angular speed of an angular speed sensor in the compass direction of a mobile object. CONSTITUTION:In an initial state, a switch 32 of an antenna controller main body 3 is connected to an angular speed sensor 4 together with a switch 33 connected to the search signal side respectively. The signal obtained with inversion of polarity of the angular speed of a mobile object is added to a search signal for compensation and elimination of the angular speed of the mobile object. Thus a satellite is searched at a fixed speed that can search a real satellite, and the satellite is automatically tracked by the signal of a switching transmitter/receiver 2. At the same time, the timer used for tracking of an open loop is initialized. The timer counts the time when the open loop is tracked based on the rotational information on the azimuth direction given from the sensor 4 in a non-catching state of satellite. Therefore the satellite is searched at a fixed speed after the rotational angle of the mobile object is compensated. Thus it is possible to ensure the stable reception and to shorten the searching time of the satellite.

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、アンテナ制御装置に関
し、特に移動体に搭載される衛星通信用装置に使用さ
れ、衛星の追尾を行うアンテナ制御装置に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an antenna control device, and more particularly to an antenna control device used in a satellite communication device mounted on a mobile body and for tracking a satellite.

【0002】[0002]

【従来の技術】従来、この種のアンテナ制御装置では、
車両自体の走行にともなう回転角速度にかかわらず、ア
ンテナを移動体に対して一定速度で回転させ、衛星を探
していた。
2. Description of the Related Art Conventionally, in this type of antenna control device,
The antenna was rotated at a constant speed with respect to the moving body to search for a satellite regardless of the angular velocity of rotation of the vehicle itself.

【0003】[0003]

【発明が解決しようとする課題】この従来のアンテナ制
御装置では、移動体が方位方向に回転してある角速度を
持っていた場合に、アンテナが一定速度で回転すると、
絶対角度で見ると、アンテナは、移動体の回転角速度が
重畳されるので、衛星を一定速度でサーチできず、安定
した受信ができなくなるのみならず、衛星捕そくに要す
る時間が長くなるという欠点があった。
In this conventional antenna control device, when the moving body has an angular velocity rotating in the azimuth direction and the antenna rotates at a constant velocity,
When viewed from an absolute angle, the rotational angular velocity of the moving body is superimposed on the antenna, so that the satellite cannot be searched at a constant velocity, stable reception cannot be achieved, and the time required for satellite acquisition becomes long. was there.

【0004】[0004]

【課題を解決するための手段】本発明のアンテナ制御装
置は、移動体に搭載され衛星電波を送受信する送受信機
およびアンテナと、前記アンテナを駆動するアンテナ駆
動装置と、移動体自体の方位方向の角速度を検出する角
速度センサとを備えたアンテナ制御装置において、衛星
の初期捕そくまたは再捕そくのために、方位方向に一定
速度で衛星をサーチするサーチ信号発生手段と、このサ
ーチ信号から前記角速度センサーの移動体の方位方向の
回転角速度を補償する演算を含む制御手段とを有し、前
記アンテナ駆動装置に衛星追尾のために一定速度のサー
チ動作を行わせる。
SUMMARY OF THE INVENTION An antenna control device of the present invention comprises a transceiver and an antenna mounted on a moving body for transmitting and receiving satellite radio waves, an antenna driving device for driving the antenna, and an azimuth direction of the moving body itself. In an antenna control device provided with an angular velocity sensor for detecting an angular velocity, search signal generating means for searching a satellite at a constant velocity in the azimuth direction for initial capture or recapture of the satellite, and the angular velocity from the search signal. And a control unit including a calculation for compensating the rotational angular velocity of the moving body of the sensor in the azimuth direction, and causing the antenna driving device to perform a constant velocity search operation for satellite tracking.

【0005】[0005]

【実施例】次に本発明について図面を参照して説明す
る。図1は本発明の一実施例の構成図、図2は本実施例
を説明する動作フローである。図1において、1は、衛
星追尾のためのアンテナ、2は送受信機であり、アンテ
ナ1からのRF信号を受信し、また、アンテナ1へRF
信号を送信する。送受信機2が衛星を捕そくして、衛星
電波を受信すると、その捕そく状態を最適に保つための
自動追尾信号を出力する。さらに、送受信機2は衛星を
捕そく中であるかどうかの衛星捕そく信号を出力する機
能を有する。4は角速度センサであり、移動体自体の方
位方向の回転を検出する。3は、アンテナ制御装置本体
であり送受信機2からの衛星捕そく信号、自動追尾信
号、及び、角速度センサ4から検出される信号に基づき
アンテナ駆動装置5に駆動指令を生成する。このアンテ
ナ制御装置本体3は次の部分から構成される。角速度セ
ンサ4からの角速度信号の極性を反転させるためのアン
プ30、初期捕そくに必要な一定速度でアンテナを駆動
するためのサーチ信号発生回路31、切り替えスイッチ
32は角速度センサ4の信号と自動追尾信号との切り替
えを行い、切り替えスイッチ33はサーチ信号発生回路
31の出力信号のオンオフを行う。演算装置34は送受
信機2からの衛星捕そく信号に基づき切り替えスイッチ
32,33を切り替える。ほかに、アンテナ駆動装置5
があり、アンテナ制御装置3からの信号によりアンテナ
を駆動する。さらにモータ6、減速機7を備えておりア
ンテナ1を駆動する。
The present invention will be described below with reference to the drawings. FIG. 1 is a block diagram of an embodiment of the present invention, and FIG. 2 is an operation flow for explaining the present embodiment. In FIG. 1, reference numeral 1 is an antenna for satellite tracking, 2 is a transceiver, which receives an RF signal from the antenna 1 and transmits an RF signal to the antenna 1.
Send a signal. When the transceiver 2 captures a satellite and receives a satellite radio wave, it outputs an automatic tracking signal for keeping the captured state optimum. Further, the transceiver 2 has a function of outputting a satellite capture signal indicating whether the satellite is being captured. An angular velocity sensor 4 detects the rotation of the moving body in the azimuth direction. Reference numeral 3 denotes an antenna control device main body, which generates a drive command to the antenna drive device 5 based on a satellite capture signal from the transceiver 2, an automatic tracking signal, and a signal detected by the angular velocity sensor 4. The antenna control device body 3 is composed of the following parts. An amplifier 30 for reversing the polarity of the angular velocity signal from the angular velocity sensor 4, a search signal generating circuit 31 for driving the antenna at a constant speed necessary for initial capture, and a changeover switch 32 are the signals of the angular velocity sensor 4 and automatic tracking. Switching with a signal, the changeover switch 33 turns on / off the output signal of the search signal generating circuit 31. The arithmetic unit 34 switches the changeover switches 32 and 33 based on the satellite acquisition signal from the transceiver 2. Besides, the antenna driving device 5
Then, the antenna is driven by the signal from the antenna control device 3. Further, a motor 6 and a speed reducer 7 are provided to drive the antenna 1.

【0006】次に、図2のフローチャートにより動作を
説明する。まず、ステップ101は衛星の初期捕そくを
行う。すなわち、初期時に、アンテナ制御装置本体3の
スイッチ32は、角速度センサ側に、スイッチ33は、
サーチ信号側に接続させる事により、移動体の角速度の
極性が反転した信号とサーチ信号とを加算することによ
り移動体の回転角速度を補償除去する。すなわち、真の
衛星をサーチする一定速度の角度で衛星をサーチする。
ステップ102は衛星捕そくの状態を送受信機2からの
衛星捕そく信号に基づき判断し、衛星電波を受信し捕そ
く中であるときには、ステップ103に移行し、スイッ
チ32,33を切り替え送受信機2の自動追尾信号によ
り自動追尾を行う。ステップ104では、この自動追尾
に入いった時点で、オープンループ追尾(すなわち初期
捕そく)に用いられるタイマの初期化を行う。ステップ
102においてNOの場合、すなわち衛星捕そく状態で
ない時には、ステップ105に移り角速度センサ4から
の方位方向の回転情報に基づき、オープンループ追尾を
行う。ステップ106はオープンループ追尾を行ってい
る時間をタイマによりカウントさせる。ステップ107
によりNOの場合、すなわち、タイムアウトしていない
ときは、オープンループによる追尾を継続する。また、
タイムアウトしたときは、YESとしてオープンループ
追尾をあきらめ、ステップ101のサーチモードに戻り
再度衛星を捕そくする。
Next, the operation will be described with reference to the flowchart of FIG. First, step 101 performs initial satellite acquisition. That is, at the initial stage, the switch 32 of the antenna control device body 3 is on the angular velocity sensor side, and the switch 33 is
By connecting to the search signal side, the rotational angular velocity of the moving body is compensated and removed by adding the signal in which the polarity of the angular velocity of the moving body is inverted and the search signal. That is, a satellite is searched at an angle of a constant speed for searching a true satellite.
In step 102, the state of satellite acquisition is judged based on the satellite acquisition signal from the transceiver 2, and if satellite radio waves are being received and acquisition is in progress, the process proceeds to step 103, and switches 32 and 33 are switched to the transceiver 2 Automatic tracking is performed by the automatic tracking signal of. In step 104, when the automatic tracking is started, the timer used for the open loop tracking (that is, the initial acquisition) is initialized. If NO in step 102, that is, if the satellite is not in the satellite acquisition state, the process proceeds to step 105 and open loop tracking is performed based on the rotation information in the azimuth direction from the angular velocity sensor 4. In step 106, the time during which open loop tracking is performed is counted by a timer. Step 107
If NO, that is, if the time-out has not occurred, the open-loop tracking is continued. Also,
When the time-out has occurred, the answer is YES and the open loop tracking is abandoned, and the process returns to the search mode of step 101 to capture the satellite again.

【0007】[0007]

【発明の効果】上述したように本発明のアンテナ制御装
置では、移動体自体の回転角速度を検出する角速度セン
サと、切り替えスイッチ32,33と加算器とを備えて
いるので、衛星の初期捕そくのために、全方位をサーチ
する際に、移動体自体の回転角速度を補償した上で一定
速度で衛星をサーチすることができる。したがって安定
した受信ができ衛星サーチに要する時間を短縮できると
いう効果がある。
As described above, the antenna control device of the present invention is provided with the angular velocity sensor for detecting the rotational angular velocity of the moving body itself, the changeover switches 32 and 33, and the adder. Therefore, when searching in all directions, the satellite can be searched at a constant speed after compensating for the rotational angular speed of the moving body itself. Therefore, there is an effect that stable reception is possible and the time required for satellite search can be shortened.

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

【図1】本発明の一実施例を示す構成図である。FIG. 1 is a configuration diagram showing an embodiment of the present invention.

【図2】本実施例を説明するための動作フローである。FIG. 2 is an operation flow for explaining the present embodiment.

【符号の説明】[Explanation of symbols]

1 アンテナ 2 送受信機 3 アンテナ制御装置本体 4 角速度センサ 5 アンテナ駆動装置 6 モータ 7 減速機 30 アンプ 31 サーチ信号発生回路 32,33 スイッチ 34 演算装置 1 Antenna 2 Transceiver 3 Antenna Control Device Main Body 4 Angular Velocity Sensor 5 Antenna Drive Device 6 Motor 7 Reducer 30 Amplifier 31 Search Signal Generation Circuit 32, 33 Switch 34 Computing Device

Claims (3)

【特許請求の範囲】[Claims] 【請求項1】 移動体に搭載され衛星電波を送受信する
送受信機およびアンテナと、前記アンテナを駆動するア
ンテナ駆動装置と、移動体自体の方位方向の角速度を検
出する角速度センサとを備えたアンテナ制御装置におい
て、衛星の初期捕そくまたは再捕そくのために、方位方
向に一定速度で衛星をサーチするサーチ信号発生手段
と、このサーチ信号から前記角速度センサーの移動体の
方位方向の回転角速度を補償する演算を含む制御手段と
を有し、前記アンテナ駆動装置に衛星追尾のために一定
速度のサーチ動作を行わせる事を特徴とするアンテナ制
御装置。
1. An antenna control equipped with a transceiver and an antenna mounted on a mobile body for transmitting and receiving satellite radio waves, an antenna driving device for driving the antenna, and an angular velocity sensor for detecting an angular velocity in the azimuth direction of the mobile body itself. In the device, search signal generating means for searching the satellite at a constant velocity in the azimuth direction for initial capture or recapture of the satellite, and compensation of the rotational angular velocity in the azimuth direction of the moving body of the angular velocity sensor from the search signal. And a control unit including a calculation for performing the search operation at a constant speed for tracking the satellite by the antenna drive device.
【請求項2】 前記制御手段が前記送受信機からの情報
により生成される制御信号により前記サーチ信号発生手
段からのサーチ信号をオン・オフする第1のスイッチ
と、前記角速度センサーからの信号又は前記送受信機か
らの自動追尾信号のいずれかを選択する第2のスイッチ
とを有することを特徴とする請求項1記載のアンテナ制
御装置。
2. A first switch for turning on / off a search signal from said search signal generating means by said control means according to a control signal generated from information from said transceiver, and a signal from said angular velocity sensor or said The antenna control device according to claim 1, further comprising a second switch that selects one of the automatic tracking signals from the transceiver.
【請求項3】 前記制御手段が衛星のサーチを開始した
時点からの時間を計数するタイムカウンタと、このタイ
ムカウンタが所定時間を計数すると初期捕そく動作にも
どり衛星のサーチを開始させることを特徴とする請求項
1記載のアンテナ制御装置。
3. A time counter for counting the time from the time when the control means starts the satellite search, and when the time counter counts a predetermined time, it returns to the initial trapping operation and starts the satellite search. The antenna control device according to claim 1.
JP04157193A 1992-06-17 1992-06-17 Antenna control device Expired - Fee Related JP3087453B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP04157193A JP3087453B2 (en) 1992-06-17 1992-06-17 Antenna control device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP04157193A JP3087453B2 (en) 1992-06-17 1992-06-17 Antenna control device

Publications (2)

Publication Number Publication Date
JPH0613810A true JPH0613810A (en) 1994-01-21
JP3087453B2 JP3087453B2 (en) 2000-09-11

Family

ID=15644237

Family Applications (1)

Application Number Title Priority Date Filing Date
JP04157193A Expired - Fee Related JP3087453B2 (en) 1992-06-17 1992-06-17 Antenna control device

Country Status (1)

Country Link
JP (1) JP3087453B2 (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5537122A (en) * 1994-07-22 1996-07-16 Japan Radio Co., Ltd. Tracking array antenna system
WO1996038876A1 (en) * 1995-05-29 1996-12-05 Nippon Steel Corporation Satellite communication device mounted on mobile body
US5594460A (en) * 1994-11-16 1997-01-14 Japan Radio Co., Ltd. Tracking array antenna system
KR100309682B1 (en) * 1999-03-18 2001-09-26 오길록 Satellite Tracking Control Method and Tracking apparatus for Vehicle-mounted Receive Antenna Systems
KR100682984B1 (en) * 2004-12-07 2007-02-15 한국전자통신연구원 Hybrid Antenna System
US7564420B2 (en) 2004-12-07 2009-07-21 Electronics And Telecommunications Research Institute Hybrid antenna system

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5537122A (en) * 1994-07-22 1996-07-16 Japan Radio Co., Ltd. Tracking array antenna system
US5594460A (en) * 1994-11-16 1997-01-14 Japan Radio Co., Ltd. Tracking array antenna system
WO1996038876A1 (en) * 1995-05-29 1996-12-05 Nippon Steel Corporation Satellite communication device mounted on mobile body
EP0829919A1 (en) * 1995-05-29 1998-03-18 Nippon Steel Corporation Satellite communication device mounted on mobile body
EP0829919A4 (en) * 1995-05-29 1998-06-10 Nippon Steel Corp Satellite communication device mounted on mobile body
KR100309682B1 (en) * 1999-03-18 2001-09-26 오길록 Satellite Tracking Control Method and Tracking apparatus for Vehicle-mounted Receive Antenna Systems
KR100682984B1 (en) * 2004-12-07 2007-02-15 한국전자통신연구원 Hybrid Antenna System
US7564420B2 (en) 2004-12-07 2009-07-21 Electronics And Telecommunications Research Institute Hybrid antenna system

Also Published As

Publication number Publication date
JP3087453B2 (en) 2000-09-11

Similar Documents

Publication Publication Date Title
US8314735B2 (en) Satellite tracking antenna system with improved tracking characteristics and operating method thereof
JPH0888510A (en) Tracking array antenna system
JPH0613810A (en) Antenna controller
WO1996038876A1 (en) Satellite communication device mounted on mobile body
JP2000059282A (en) Satellite tracking antenna device for mobile object
JPH05142321A (en) Satellite tracking receiver of antenna fore moving body
JP3290322B2 (en) Tracking control system for mobile antenna
JP3181818B2 (en) Antenna pointing direction control method and device
JPH05232206A (en) Antenna control apparatus
JPH11154816A (en) On-vehicle antenna system
JPH0448282A (en) Antenna controller
JP2725443B2 (en) Antenna control device
JP3227060B2 (en) Tracking control method for mobile antenna
JP2722843B2 (en) Antenna control device
JP3358921B2 (en) Antenna automatic tracking method
JP3159873B2 (en) Tracking control method and tracking control device for mobile body mounted antenna
JP3186533B2 (en) Tracking antenna device
JP3110829B2 (en) Satellite broadcast receiving antenna device
JP2002296340A (en) Satellite signal receiver for positioning
JP2814844B2 (en) Flying object tracking device
JP3501214B2 (en) Satellite tracking device
JP3097797B2 (en) Mobile antenna satellite tracking method and apparatus
JP3249901B2 (en) Mobile antenna device and directivity control method thereof
JP2985860B2 (en) Antenna control device
JPH11153658A (en) Device and method for controlling tracking of antenna mounted on traveling object

Legal Events

Date Code Title Description
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20000613

LAPS Cancellation because of no payment of annual fees