JPH03266508A - Antenna controller - Google Patents

Antenna controller

Info

Publication number
JPH03266508A
JPH03266508A JP6642690A JP6642690A JPH03266508A JP H03266508 A JPH03266508 A JP H03266508A JP 6642690 A JP6642690 A JP 6642690A JP 6642690 A JP6642690 A JP 6642690A JP H03266508 A JPH03266508 A JP H03266508A
Authority
JP
Japan
Prior art keywords
antenna
phase
scanning
phib
phia
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
JP6642690A
Other languages
Japanese (ja)
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 JP6642690A priority Critical patent/JPH03266508A/en
Publication of JPH03266508A publication Critical patent/JPH03266508A/en
Pending legal-status Critical Current

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  • Variable-Direction Aerials And Aerial Arrays (AREA)

Abstract

PURPOSE:To simplify the mechanical constitution of the controller and to attain miniaturization and light weight by correcting an antenna beam electrically so that an error signal detected by the electric beam scanning is made zero with respect to an elevating angle in the tracking system of the antenna controller. CONSTITUTION:Let scanning phase shifts of antenna elements 1A-1D be respectively phiA, phiB, phiC, phiD, then they are selected so as to be phiA=phiC=theta1, phiB=phiD=0 in the azimuth direction (1) and phiB=phiD=theta1, phiA=phiC=0 in the azimuth direction (2). Moreover, they are selected so as to be phiA=phiB=theta2, phiC=phiD=0 and phiA=phiB=0, phiC=phiD=theta2 in the elevating angle directions (1), (2) of the electric scanning phase shift respectively. A phase shift eta to correct the antenna beam in the elevating angle is added to scanning phase shifts phiA, phiB of antenna elements 1A, 1B for the beam scanning to obtain a tracking error signal from the phase of each antenna and the beam is offset in the accurate elevating angle direction by varying the phase shift eta. Thus, the controller is simplified and miniaturization and light weight are attained.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 この発明はアンテナ制御装置に関し、特に衛星に対する
移動体通信等に利用される小型化・軽量化をはかったア
ンテナ制御装置に関する。
DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to an antenna control device, and more particularly to a miniaturized and lightweight antenna control device used for mobile communications with satellites.

〔従来の技術〕[Conventional technology]

従来の衛星電波を追尾するビームスキャン追尾のアンテ
ナ制御装置ではビーム走査により得られる追尾信号をも
とにして仰角および方位方向ともに、モータを駆動させ
ることにより機械的に追尾を行なっていた。
Conventional antenna control devices for beam scan tracking that track satellite radio waves mechanically perform tracking by driving motors in both elevation and azimuth directions based on tracking signals obtained by beam scanning.

〔発明が解決しようとする課題〕[Problem to be solved by the invention]

上述した従来のアンテナ制御装置は、アンテナの仰角お
よび方位角方向の駆動を機械的に行うための機構が必要
であるので、その構造が複雑となり、小型化、軽量化と
いう面で大きな障害となる欠点がある。
The above-mentioned conventional antenna control device requires a mechanism to mechanically drive the antenna in the elevation and azimuth directions, which makes its structure complicated and poses a major obstacle in terms of miniaturization and weight reduction. There are drawbacks.

〔課題を解決するための手段〕[Means to solve the problem]

本発明のアンテナ制御装置はビーム走査により衛星電波
の追尾を行なう少なくとも4個のアンテナ素子を有する
アンテナ制御装置において、追尾方向の方位方向追尾を
行う機械駆動機構と、追尾を行う前記4個のアンテナ素
子のそれぞれから受信される高周波信号の移相走査を行
う4個の移相器と、追尾誤差信号に対応して位相補正を
行う補正用移相器と前記4個の移相器および前記補正用
移相器を制御する位相制御部と、前記機械的駆動機構と
前記位相制御部とを所定の手順により制御する演算処理
部とを有する。
An antenna control device of the present invention is an antenna control device having at least four antenna elements that performs tracking of satellite radio waves by beam scanning, and includes a mechanical drive mechanism that performs azimuth direction tracking in a tracking direction, and a mechanical drive mechanism that performs azimuth direction tracking in a tracking direction, and a mechanical drive mechanism that performs azimuth direction tracking in a tracking direction, and four phase shifters that perform phase shift scanning of high frequency signals received from each of the elements; a correction phase shifter that performs phase correction in response to a tracking error signal; the four phase shifters and the correction. and a calculation processing section that controls the mechanical drive mechanism and the phase control section according to a predetermined procedure.

〔実施例〕〔Example〕

次に本発明について図面を参照して説明する。 Next, the present invention will be explained with reference to the drawings.

第1図は本発明の一実施例の構成図、第2図(a>、(
b)は本実施例のアンテナビームの切換え条件とアンテ
ナ位相の関係を説明する説明図である。第1図の実施例
は4つのアンテナ素子LA、IB、IC,LDから構成
されるアレーアンテナ1、各アンテナ素子IA、IB、
IC。
FIG. 1 is a configuration diagram of an embodiment of the present invention, and FIG. 2 (a>, (
b) is an explanatory diagram illustrating the relationship between the antenna beam switching conditions and the antenna phase in this embodiment. The embodiment shown in FIG. 1 includes an array antenna 1 consisting of four antenna elements LA, IB, IC, and LD, each antenna element IA, IB,
I.C.

IDのビームをそれぞれある移相量で電気的に走査する
ための移相器2A、2B、2C,2D、アレーアンテナ
1を仰角方向に電気的にビーム走査するための移相器3
、各移相器2A〜2D、および移相器3の移相量を制御
する位相制御部4、さらに従来と同じアレーアンテナ]
を方位方向に機械的に駆動するためのモータ駆動部6、
駆動されるモータ7、モータ7の減速機構がある。また
、衛星電波を受ける受信装置(図示せず)から検出され
る誤差信号人力9にもとづき、機械的ビーム走査の方位
方向と電気的ビーム走査の仰角方向とを所定の手順にし
たがい制御信号を出力する演算処理部5が構成されてい
る。なお、高周波出力10が移相器3、移相器2A〜2
Dを経由してアレーアンテナ1から出力される。
Phase shifters 2A, 2B, 2C, 2D for electrically scanning the ID beams by a certain phase shift amount, and a phase shifter 3 for electrically scanning the beams of the array antenna 1 in the elevation direction.
, each of the phase shifters 2A to 2D, and a phase control unit 4 that controls the amount of phase shift of the phase shifter 3, and the same array antenna as the conventional one]
a motor drive unit 6 for mechanically driving the azimuth direction;
There is a motor 7 to be driven and a speed reduction mechanism for the motor 7. Also, based on the error signal 9 detected from a receiving device (not shown) that receives satellite radio waves, a control signal is output in accordance with a predetermined procedure for the azimuth direction of mechanical beam scanning and the elevation direction of electrical beam scanning. An arithmetic processing unit 5 is configured. Note that the high frequency output 10 is the phase shifter 3, the phase shifters 2A to 2
It is output from the array antenna 1 via D.

次に本実施例の動作を第2図(a)、(b)により説明
する。第1図(a)のビームスイツチング条件はアンテ
ナビームの方位方向(1) 、 (2)の条件と仰角方
向(1) 、 (2)の条件に分けられる。
Next, the operation of this embodiment will be explained with reference to FIGS. 2(a) and 2(b). The beam switching conditions in FIG. 1(a) are divided into conditions for the azimuth directions (1) and (2) of the antenna beam and conditions for the elevation directions (1) and (2).

方位方向(1) 、 (2)に対してはそれぞれアンテ
ナ素子IA〜IDの走査移相量をφA、φB。
For azimuth directions (1) and (2), the scanning phase shift amount of antenna elements IA to ID is φA and φB, respectively.

φC2φDとすると、第1図(a)のように走査移相量
が設定される。すなわち、方位方向(1)はφA=φC
:θ1、φB=φ0=0であり、方位方向(2)はφB
=φD=θ0、φA=φc=Qのように設定する。次に
電気的走査移相量の仰角方向(1) 、 (2)に対し
てはそれぞれφA=φB=θ2、φC=φD=0、およ
びφA=φ8=0、φC=φD=θ2のように設定する
。この走査移相量φA〜φDは対応する移相器2A〜2
Dを制御することにより行われる。このように方位方向
にθ1の移相量で走査し、仰角方向にθ2の移相量で走
査することにより、各方向の追尾誤差信号を得ることが
できる。
When φC2φD, the scanning phase shift amount is set as shown in FIG. 1(a). That is, the azimuth direction (1) is φA=φC
: θ1, φB=φ0=0, and the azimuth direction (2) is φB
=φD=θ0, φA=φc=Q. Next, for the elevation direction (1) and (2) of the electrical scanning phase shift amount, φA=φB=θ2, φC=φD=0, and φA=φ8=0, φC=φD=θ2, respectively. Set. These scanning phase shift amounts φA to φD correspond to the corresponding phase shifters 2A to 2.
This is done by controlling D. By scanning in the azimuth direction with a phase shift amount of θ1 and scanning in the elevation direction with a phase shift amount of θ2 in this manner, tracking error signals in each direction can be obtained.

移相器3は仰角方向に対して得られた追尾誤差信号に基
づき誤差角度分だけビーム方向を移動させて補正するた
めの移相器である。つまり、各アンテナの位相は、第2
図(b)のように、追尾誤差信号を得るためのビームス
キャンのためにアンテナ素子IA、IBの走査移相量φ
A、φBをさらに仰角方向にアンテナビームを補正する
移相量ηを相加して、この移相量ηを変化させることで
ビームを正確な仰角方向にオフセットさせる。この場合
に方位方向(1) 、 (2)に対しても仰角で移動さ
せた分移相量ηの補正を行う。
The phase shifter 3 is a phase shifter for correcting by moving the beam direction by the error angle based on the tracking error signal obtained in the elevation direction. In other words, the phase of each antenna is
As shown in Figure (b), the scanning phase shift amount φ of antenna elements IA and IB is used for beam scanning to obtain a tracking error signal.
A and φB are further added with a phase shift amount η for correcting the antenna beam in the elevation direction, and by changing this phase shift amount η, the beam is offset in the accurate elevation direction. In this case, the phase shift amount η is corrected by the movement in the elevation angle in the azimuth directions (1) and (2) as well.

〔発明の効果〕〔Effect of the invention〕

以上説明したように本発明はアンテナ用制御装置の追尾
方式を仰角方向に対しては電気的ビーム走査により誤差
信号を検出し、この誤差信号が0となるように電気的に
アンテナビームを補正することにより、装置の機械的構
成を簡略化でき、小型化・軽量化をはかることができる
効果がある。
As explained above, the present invention uses the tracking method of the antenna control device to detect an error signal by electrical beam scanning in the elevation direction, and electrically correct the antenna beam so that this error signal becomes 0. This has the effect of simplifying the mechanical configuration of the device and making it smaller and lighter.

またビームは高速走査が可能なため仰角方向の急激な変
化に対応できるという効果もある。
Furthermore, since the beam can be scanned at high speed, it has the advantage of being able to respond to rapid changes in the direction of elevation angle.

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

第1図はこの発明の一実施例の構成図、第2図(a)、
(b)は本実施例を説明する説明図である。 1・・・アレーアンテナ、IA〜ID・・・アンテナ素
子、2A〜2,3・・・移相器、4・・・位相制御部、
5・・・演算処理部、6・・・モータ駆動部、7・・・
モータ、8・・・減速機構、9・・・誤差信号入力、1
0・・・高周波信号出力。
Fig. 1 is a configuration diagram of an embodiment of the present invention, Fig. 2(a),
(b) is an explanatory diagram illustrating this embodiment. DESCRIPTION OF SYMBOLS 1... Array antenna, IA-ID... Antenna element, 2A-2, 3... Phase shifter, 4... Phase control unit,
5... Arithmetic processing unit, 6... Motor drive unit, 7...
Motor, 8... Reduction mechanism, 9... Error signal input, 1
0...High frequency signal output.

Claims (1)

【特許請求の範囲】[Claims] ビーム走査により衛星電波の追尾を行なう少なくとも4
個のアンテナ素子を有するアンテナ制御装置において、
追尾方向の方位方向追尾を行う機械駆動機構と、追尾を
行う前記4個のアンテナ素子のそれぞれから受信される
高周波信号の移相走査を行う4個の移相器と、追尾誤差
信号に対応して位相補正を行う補正用移相器と前記4個
の移相器および前記補正用移相器を制御する位相制御部
と、前記機械的駆動機構と前記位相制御部とを所定の手
順により制御する演算処理部とを有することを特徴とす
るアンテナ制御装置。
At least 4 satellites that track satellite radio waves by beam scanning
In an antenna control device having antenna elements,
A mechanical drive mechanism that performs azimuth direction tracking in the tracking direction, four phase shifters that perform phase shift scanning of high frequency signals received from each of the four antenna elements that perform tracking, and a tracking error signal corresponding to the tracking error signal. a correction phase shifter that performs phase correction, a phase control section that controls the four phase shifters and the correction phase shifter, and the mechanical drive mechanism and the phase control section that are controlled according to a predetermined procedure. What is claimed is: 1. An antenna control device comprising: an arithmetic processing section;
JP6642690A 1990-03-15 1990-03-15 Antenna controller Pending JPH03266508A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP6642690A JPH03266508A (en) 1990-03-15 1990-03-15 Antenna controller

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP6642690A JPH03266508A (en) 1990-03-15 1990-03-15 Antenna controller

Publications (1)

Publication Number Publication Date
JPH03266508A true JPH03266508A (en) 1991-11-27

Family

ID=13315449

Family Applications (1)

Application Number Title Priority Date Filing Date
JP6642690A Pending JPH03266508A (en) 1990-03-15 1990-03-15 Antenna controller

Country Status (1)

Country Link
JP (1) JPH03266508A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH06188618A (en) * 1992-12-22 1994-07-08 Miriueibu:Kk Mobile radio terminal equipment
JP2012044596A (en) * 2010-08-23 2012-03-01 Nippon Telegr & Teleph Corp <Ntt> Tracking antenna device

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH06188618A (en) * 1992-12-22 1994-07-08 Miriueibu:Kk Mobile radio terminal equipment
JP2012044596A (en) * 2010-08-23 2012-03-01 Nippon Telegr & Teleph Corp <Ntt> Tracking antenna device

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