JPH0563433A - Antenna supporting device - Google Patents

Antenna supporting device

Info

Publication number
JPH0563433A
JPH0563433A JP24695791A JP24695791A JPH0563433A JP H0563433 A JPH0563433 A JP H0563433A JP 24695791 A JP24695791 A JP 24695791A JP 24695791 A JP24695791 A JP 24695791A JP H0563433 A JPH0563433 A JP H0563433A
Authority
JP
Japan
Prior art keywords
shaft
adjusting member
elevation angle
antenna
support
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
JP24695791A
Other languages
Japanese (ja)
Inventor
Junji Koide
淳史 小出
Yosuke Watanabe
洋輔 渡辺
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.)
Victor Company of Japan Ltd
Original Assignee
Victor Company of Japan 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 Victor Company of Japan Ltd filed Critical Victor Company of Japan Ltd
Priority to JP24695791A priority Critical patent/JPH0563433A/en
Publication of JPH0563433A publication Critical patent/JPH0563433A/en
Pending legal-status Critical Current

Links

Abstract

PURPOSE:To perform the elevation angle and bearing of a parabola antenna with a simple mechanism by enabling the scan of a plurarity of communication satellites. CONSTITUTION:In the case the distance between a horizontal axis 5 of a first indication part 2 and an axis 8 of a second indication part 3 shall be L1 and the distance between the rotation center (rotary shaft of a motor 10) of a bearing adjustment member 11 and the connection part for a supporting axis 6, that is, a foot part 12 shall be L2, the L1:L2 1:6.6 is satisfied. Thus, even when a supporting shaft 6 is rotated in the vertical surface around a shaft 5 to adjust the elevation angle and the azimuth is adjusted by rotating the azimuth adjustment member 11 around the rotary shaft of the motor 10, the L1 and L2 maintain the relationship, resulting in accurate scanning after temporarily taking a satellite position P.

Description

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

【0001】[0001]

【産業上の利用分野】本発明はパラボラアンテナの支持
に適したアンテナ支持装置、特に、通信衛星の追尾が容
易なアンテナ支持装置に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an antenna supporting device suitable for supporting a parabolic antenna, and more particularly to an antenna supporting device for easily tracking a communication satellite.

【0002】[0002]

【従来の技術】当初のパラボラアンテナ支持装置は仰
角、方位角いずれも固定されたもの、或いは方位角につ
いてのみ調整可能な構造であったので、複数の衛星を1
つのパラボラアンテナで受信できなかったり、赤道上空
の衛星に対して正確にアンテナを向けることができない
という不利があった。
2. Description of the Related Art The original parabolic antenna support device had a fixed elevation angle and azimuth angle, or a structure in which only the azimuth angle could be adjusted.
There was a disadvantage that the two parabolic antennas could not be received, or the antennas could not be accurately aimed at the satellites above the equator.

【0003】そこで、図5に示すような仰角及び方位角
のいずれについても調整可能な支持装置が最近では用い
られている。このアンテナ支持装置は、地面あるいは建
物上に鉛直に立設したポスト100上端にポスト100
と平行な固定軸101を回動可能に取り付け、この固定
軸101に外嵌した歯車102とモータにて回転せしめ
られる歯車103とを噛合し、また固定軸101の上端
にパラボラアンテナ104をブラケットを介して上下回
動自在に取り付けるとともに固定軸101に取付けたシ
リンダユニット105のロッド105aの先端をパラボ
ラアンテナ104の下部に結合している。
Therefore, a supporting device capable of adjusting both the elevation angle and the azimuth angle as shown in FIG. 5 has recently been used. This antenna support device is provided with a post 100 at the upper end of the post 100 that stands vertically on the ground or a building.
A fixed shaft 101 parallel to the fixed shaft 101 is rotatably mounted, a gear 102 externally fitted to the fixed shaft 101 and a gear 103 rotated by a motor are meshed with each other, and a parabolic antenna 104 is provided with a bracket at the upper end of the fixed shaft 101. The tip of the rod 105a of the cylinder unit 105 attached to the fixed shaft 101 is attached to the lower portion of the parabolic antenna 104 while being attached so as to be rotatable up and down.

【0004】而して、固定軸101をモータの駆動で回
動させてパラボラアンテナ104の方位角を、またシリ
ンダユニット105を伸縮作動させて仰角を調整し、通
信衛星を追尾、すなわちパラボラアンテナ104を通信
衛星に向け、通信衛星が出力する電波を受信する。
Then, the fixed shaft 101 is rotated by driving a motor to adjust the azimuth angle of the parabolic antenna 104, and the cylinder unit 105 is extended / contracted to adjust the elevation angle to track the communication satellite, that is, the parabolic antenna 104. To the communication satellite and receive the radio waves output by the communication satellite.

【0005】[0005]

【発明が解決しようとする課題】しかしながら、上述し
た従来のアンテナ支持装置にあっては、パラボラアンテ
ナ104を通信衛星に向けるために、固定軸101(モ
ータ)とシリンダユニット105とを独立して作動させ
て方位角と仰角とを調整しなければならず、その作業が
煩雑でパラボラアンテナを通信衛星に向けることが困難
であった。
However, in the above-mentioned conventional antenna support device, the fixed shaft 101 (motor) and the cylinder unit 105 are operated independently to direct the parabolic antenna 104 to the communication satellite. Therefore, the azimuth angle and the elevation angle must be adjusted, and the work is complicated and it is difficult to direct the parabolic antenna to the communication satellite.

【0006】[0006]

【課題を解決するための手段】上記課題を解決すべく本
発明に係るアンテナ支持装置は、鉛直に起立する基体に
第1及び第2の支持部を設け、第1の支持部には先端に
パラボラアンテナを取付けた支持軸の中間部を垂直面内
で回動自在に支承し、第2の支持部には仰角調整部材を
垂直面内で回動自在に支承し、この仰角調整部材に方位
調整部材の先端を回動自在に取付け、この方位調整部材
の基端と前記支持軸の基端とを回転且つ摺動自在に連結
し、更に前記基体の第1の指示部と第2の指示部との間
の距離L1に対し、前記方位調整部材の回動中心と支持
軸に対する連結部との間の距離L2を約6.6倍の長さ
に設定した。
In order to solve the above problems, an antenna supporting apparatus according to the present invention is provided with a first and a second supporting portions on a vertically standing base body, and the first supporting portion has a tip end. An intermediate portion of the support shaft having the parabolic antenna mounted thereon is rotatably supported in a vertical plane, and an elevation angle adjusting member is rotatably supported in a vertical plane on the second supporting portion, and the azimuth is adjusted to the elevation angle adjusting member. The tip end of the adjusting member is rotatably attached, and the base end of the azimuth adjusting member and the base end of the support shaft are rotatably and slidably connected to each other, and further, the first indicating portion and the second indicating portion of the base body. The distance L2 between the rotation center of the azimuth adjusting member and the connecting portion with respect to the support shaft is set to be about 6.6 times the distance L1 between the portion and the portion.

【0007】[0007]

【作用】図3および図4において、Eは地球、Oは地球
の中心、Aは観測点、Mは衛星軌道、Pは衛星軌道上の
点、O’はA点において鉛直方向に延長した任意の点、
M’は点O’を通る軌道Mと平行な軌道、P’は線分P
Aの延長線と軌道M’との交点とすると、三角形OAP
と三角形O’AP’は点Aの位置(緯度)に関係なく常
に相似形である。
In FIGS. 3 and 4, E is the earth, O is the center of the earth, A is the observation point, M is the satellite orbit, P is the point on the satellite orbit, and O'is an arbitrary point extending vertically at point A. Point of
M'is an orbit parallel to the orbit M passing through the point O ', P'is a line segment P
The intersection of the extension line of A and the orbit M'is the triangle OAP
And the triangle O'AP 'are always similar regardless of the position (latitude) of the point A.

【0008】一方、衛星軌道Mは赤道(地球表面)の上
空約35,800kmの円であり、三角形OAPは円M
を導線、Aを頂点とした円錐(正確には円錐台)、三角
形O’AP’は円M’を導線、Aを頂点とした円錐(正
確には円錐台)を形成し、これら円錐は相似関係にあ
る。そして、この相似関係において、点Pと点P’とが
導線としての円M、円M’の相対する位置にあればP-
A-P’は一直線となる。このことは、円M’上の点
P’を決めれば線分P’Aの延長線上に必ず点Pつまり
衛星があることになる。
On the other hand, the satellite orbit M is a circle about 35,800 km above the equator (earth surface), and the triangle OAP is the circle M.
, A cone with A as a vertex (correctly a truncated cone), a triangle O'AP 'forms a circle with M'as a lead, and A as a vertex (correctly a truncated cone), and these cones are similar. Have a relationship. Then, in this similarity relationship, if the point P and the point P'are located at the positions where the circle M and the circle M'as conductors face each other, P-
AP 'becomes a straight line. This means that if the point P'on the circle M'is determined, the point P, that is, the satellite is always on the extension of the line segment P'A.

【0009】ここで、線分OPは35,800kmに地
球の半径約6,380kmを加えた約42,180km
であり、線分OAは地球の半径約6,380kmである
ので、OA:OP=O’A:O’P≒1:6.6の関係
が成立する。即ち、点A及び点Pの位置がどこにあって
も、三角形OAPにおける線分OAと線分OPとの比は
常に1:6.6であるので、三角形の2つの片の長さの
比が常に1:6.6の関係を維持し得る骨格の支持装置
を制作することにより、任意の通信衛星の追尾が正確に
行える。
Here, the line segment OP is about 42,180 km, which is 35,800 km plus the radius of the earth about 6,380 km.
Since the line segment OA has a radius of the earth of about 6,380 km, the relationship of OA: OP = O′A: O′P≈1: 6.6 holds. That is, no matter where the points A and P are located, the ratio between the line segment OA and the line segment OP in the triangle OAP is always 1: 6.6. By manufacturing a skeletal support device that can always maintain the relationship of 1: 6.6, it is possible to accurately track an arbitrary communication satellite.

【0010】[0010]

【実施例】以下に本発明の実施例を添付図面に基づいて
説明する。ここで図1は本発明に係るアンテナ支持装置
の側面図、図2は同アンテナ支持装置の要部の斜視図で
あり、アンテナ支持装置は鉛直に起立する基体1に第1
及び第2の支持部2,3を設けている。
Embodiments of the present invention will be described below with reference to the accompanying drawings. Here, FIG. 1 is a side view of an antenna supporting device according to the present invention, and FIG. 2 is a perspective view of a main part of the antenna supporting device. The antenna supporting device is firstly mounted on a vertically standing base body 1.
And the second supporting portions 2 and 3 are provided.

【0011】第1の支持部2には図2にも示すように枠
体4内に水平軸5を回転可能に架設し、この水平軸5に
支持軸6の中間部を固着し、この支持軸6の先端部にパ
ラボラアンテナ7を取付け、支持軸6を垂直面内で回動
せしめることでパラボラアンテナ7の仰角を変化せしめ
るようにしている。
As shown in FIG. 2, a horizontal shaft 5 is rotatably installed on the first support portion 2 in a frame body 4, and an intermediate portion of the support shaft 6 is fixed to the horizontal shaft 5 to support the same. The parabolic antenna 7 is attached to the tip of the shaft 6, and the elevation angle of the parabolic antenna 7 is changed by rotating the support shaft 6 in a vertical plane.

【0012】第2の支持部3には軸8を介して仰角調整
部材9を垂直面内で回動自在に支承し、この仰角調整部
材9にモータ10を固設し、このモータ10の回転軸を
板状をなす方位調整部材11の先端に結合している。
An elevation angle adjusting member 9 is rotatably supported on the second supporting portion 3 via a shaft 8 in a vertical plane, and a motor 10 is fixedly mounted on the elevation angle adjusting member 9 to rotate the motor 10. The shaft is connected to the tip of the plate-shaped azimuth adjusting member 11.

【0013】また、方位調整部材11の基端部には脚部
12を設け、この脚部12の下端に枠体13を取付け、
この枠体13内に水平軸14を回転可能に架設し、この
水平軸14に固着した軸受け15に前記支持軸6の基端
部を摺動自在に挿通している。軸受けの構造は上記に限
らず球面軸受け等を採用してもよい。
A leg portion 12 is provided at the base end portion of the azimuth adjusting member 11, and a frame 13 is attached to the lower end of the leg portion 12,
A horizontal shaft 14 is rotatably installed in the frame body 13, and a base end portion of the support shaft 6 is slidably inserted into a bearing 15 fixed to the horizontal shaft 14. The structure of the bearing is not limited to the above, and a spherical bearing or the like may be adopted.

【0014】そして、上記の構造において、第1の指示
部2の水平軸5と第2の指示部3の軸8との間の距離を
L1とし、前記方位調整部材11の回動中心(モータ1
0の回転軸)と支持軸6に対する連結部つまり脚部12
との間の距離をL2とした場合、L1:L2≒1:6.
6となるように設定している。
In the above structure, the distance between the horizontal shaft 5 of the first indicator 2 and the shaft 8 of the second indicator 3 is L1, and the center of rotation of the azimuth adjusting member 11 (motor 1
0 rotation axis) and the support shaft 6 are connected to each other, that is, the legs 12
When the distance between L1 and L2 is L2, L1: L2≈1: 6.
It is set to be 6.

【0015】ここで、L1:L2≒1:6.6となるよ
うに設定することで、指示部2,3及び方位調整部材1
1にて形成される三角形は図3に示した三角形O’A
P’と相似関係になる。即ち、軸8の中心が点O’に、
軸5の中心が点Aに、軸14の中心が点P’にそれぞれ
相当し、支持軸6を軸5を中心として垂直面内で回動さ
せて仰角を調整しても、また方位角調整部材11をモー
タ10の回転軸を中心に回動させて方位角を調整して
も、L1とL2は上記の関係を維持するので、一旦衛星
の位置Pを捉えた後は正確に追尾することができる。
Here, by setting so that L1: L2≈1: 6.6, the indicating sections 2 and 3 and the azimuth adjusting member 1 are set.
The triangle formed by 1 is the triangle O'A shown in FIG.
It becomes similar to P '. That is, the center of the axis 8 is at the point O ',
The center of the shaft 5 corresponds to the point A and the center of the shaft 14 corresponds to the point P ', and the azimuth angle is adjusted even if the support shaft 6 is rotated in the vertical plane about the shaft 5 to adjust the elevation angle. Even if the member 11 is rotated about the rotation axis of the motor 10 to adjust the azimuth angle, L1 and L2 maintain the above relationship, so that the position P of the satellite should be accurately tracked. You can

【0016】[0016]

【発明の効果】以上に説明したように本発明に係るアン
テナ支持装置によれば、簡単な構造で複数の衛星のうち
任意の衛星に対して正確にアンテナを向けることがで
き、しかも1つの部材にアンテナの仰角と方位を調整す
る機能を兼持せしめたので、部品点数も少なくなる。
As described above, according to the antenna supporting apparatus of the present invention, the antenna can be accurately directed to any satellite among a plurality of satellites with a simple structure, and one member is provided. Since it also has the function of adjusting the elevation angle and azimuth of the antenna, the number of parts is also reduced.

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

【図1】本発明に係るアンテナ支持装置の側面図FIG. 1 is a side view of an antenna support device according to the present invention.

【図2】同アンテナ支持装置の要部の斜視図FIG. 2 is a perspective view of a main part of the antenna support device.

【図3】本発明の原理を平面的に説明した図FIG. 3 is a diagram for explaining the principle of the present invention two-dimensionally.

【図4】本発明の原理を立体的に説明した図FIG. 4 is a diagram for three-dimensionally explaining the principle of the present invention.

【図5】従来のアンテナ支持装置の構造を示す図FIG. 5 is a diagram showing a structure of a conventional antenna support device.

【符号の説明】[Explanation of symbols]

1…基体、2…第1の支持部、3…第2の支持部、5、
8、14…水平軸、6…支持軸、7…パラボラアンテ
ナ、9…仰角調整部材、10…モータ、11…方位調整
部材、L1…第1の指示部と第2の指示部との間の距
離、L2…方位調整部材の回動中心と支持軸に対する連
結部との間の距離。
1 ... Base, 2 ... 1st support part, 3 ... 2nd support part, 5,
8, 14 ... Horizontal axis, 6 ... Support axis, 7 ... Parabolic antenna, 9 ... Elevation angle adjusting member, 10 ... Motor, 11 ... Direction adjusting member, L1 ... Between first indicator and second indicator Distance, L2 ... Distance between the rotation center of the azimuth adjusting member and the connecting portion with respect to the support shaft.

Claims (2)

【特許請求の範囲】[Claims] 【請求項1】 鉛直に起立する基体に第1及び第2の支
持部を設け、第1の支持部には先端にパラボラアンテナ
を取付けた支持軸の中間部を垂直面内で回動自在に支承
し、第2の支持部には仰角調整部材を垂直面内で回動自
在に支承し、この仰角調整部材に方位調整部材の先端を
回動自在に取付け、この方位調整部材の基端と前記支持
軸の基端とを回転且つ摺動自在に連結し、更に前記基体
の第1の指示部と第2の指示部との間の距離をL1、前
記方位調整部材の回動中心と支持軸に対する連結部との
間の距離をL2とした場合、これらを下記の比に設定し
たことを特徴とするアンテナ支持装置。 L1:L2≒1:6.6
1. A vertically erected base body is provided with first and second support portions, and the first support portion has an intermediate portion of a support shaft having a parabola antenna attached to a tip end thereof to be rotatable in a vertical plane. In the vertical direction, the elevation angle adjusting member is rotatably supported on the second support portion, and the tip of the azimuth adjusting member is rotatably attached to the elevation angle adjusting member. The base end of the support shaft is rotatably and slidably connected, and further, the distance between the first indicating portion and the second indicating portion of the base is L1, and the rotation center of the azimuth adjusting member is supported. The antenna supporting device is characterized in that when the distance between the shaft and the connecting portion is L2, these are set to the following ratios. L1: L2≈1: 6.6
【請求項2】 前記仰角調整部材には仰角調整部材と前
記支持軸とを一体的に回動させる駆動手段を設けたこと
を特徴とする請求項1に記載のアンテナ支持装置。
2. The antenna support device according to claim 1, wherein the elevation angle adjusting member is provided with a drive means for integrally rotating the elevation angle adjusting member and the support shaft.
JP24695791A 1991-08-30 1991-08-30 Antenna supporting device Pending JPH0563433A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP24695791A JPH0563433A (en) 1991-08-30 1991-08-30 Antenna supporting device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP24695791A JPH0563433A (en) 1991-08-30 1991-08-30 Antenna supporting device

Publications (1)

Publication Number Publication Date
JPH0563433A true JPH0563433A (en) 1993-03-12

Family

ID=17156247

Family Applications (1)

Application Number Title Priority Date Filing Date
JP24695791A Pending JPH0563433A (en) 1991-08-30 1991-08-30 Antenna supporting device

Country Status (1)

Country Link
JP (1) JPH0563433A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2011102766A (en) * 2009-11-11 2011-05-26 Japan Radio Co Ltd Satellite capturing device
KR20150097354A (en) * 2014-02-17 2015-08-26 주식회사 아이두잇 Antenna supporting apparatus

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2011102766A (en) * 2009-11-11 2011-05-26 Japan Radio Co Ltd Satellite capturing device
KR20150097354A (en) * 2014-02-17 2015-08-26 주식회사 아이두잇 Antenna supporting apparatus

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