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JP2001119227A - Radio transmission method - Google Patents

Radio transmission method

Info

Publication number
JP2001119227A
JP2001119227A JP29890399A JP29890399A JP2001119227A JP 2001119227 A JP2001119227 A JP 2001119227A JP 29890399 A JP29890399 A JP 29890399A JP 29890399 A JP29890399 A JP 29890399A JP 2001119227 A JP2001119227 A JP 2001119227A
Authority
JP
Japan
Prior art keywords
radio
directional antenna
radio wave
rotation
drop
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
JP29890399A
Other languages
Japanese (ja)
Inventor
Tomoaki Yuasa
智明 湯浅
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.)
Mitsubishi Electric Corp
Original Assignee
Mitsubishi Electric 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 Mitsubishi Electric Corp filed Critical Mitsubishi Electric Corp
Priority to JP29890399A priority Critical patent/JP2001119227A/en
Publication of JP2001119227A publication Critical patent/JP2001119227A/en
Pending legal-status Critical Current

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Abstract

(57)【要約】 【課題】 空中投下型電波機器は、従来、無指向性アン
テナで電波送信されており、指向性アンテナ使用に比べ
送信機の出力が十分に生かせない欠点があった。 【解決手段】 指向性アンテナ3を備えた空中投下型電
波機器1を打ち上げロケットや航空機等から投下し、そ
の落下中に上記電波機器1から電波を送信し、移動体や
地上の受信局2で電波受信を行う電波送信方法におい
て、空中投下型電波機器1には空中での自己方位の取得
のために地磁気センサ7を搭載し、その方位を自己基準
として受信局方向へ指向性アンテナ3を向けるに際し、
指向性アンテナ3の正回転または逆回転のいずれかの
内、受信局方向への最小動作角を算出し、その最小動作
角に従って指向性アンテナ3の軸回転制御を行うように
した。
(57) [Summary] [PROBLEMS] An air-drop radio device has conventionally been radio-transmitted by a non-directional antenna, and has a drawback that the output of the transmitter cannot be sufficiently utilized compared to the use of a directional antenna. SOLUTION: An air-drop radio device 1 provided with a directional antenna 3 is dropped from a launch vehicle, an aircraft, or the like, and a radio wave is transmitted from the radio device 1 during the drop. In the radio wave transmission method for receiving radio waves, the air-drop radio device 1 is equipped with a geomagnetic sensor 7 for acquiring its own azimuth in the air, and the directional antenna 3 is directed toward the receiving station with the azimuth as its reference. On the occasion,
The minimum operation angle toward the receiving station is calculated from either the forward rotation or the reverse rotation of the directional antenna 3, and the rotation of the directional antenna 3 is controlled in accordance with the minimum operation angle.

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】この発明は、打ち上げロケッ
トや航空機等からの投下で、落下中に電波を送信し、移
動体(車、航空機、飛翔体、船舶など)や地上の受信局
で電波受信を行うことを目的とした電波送信方法に係る
ものである。ここでいう受信局は、この発明の装置から
の受信を本来の目的としない妨害電波の受信局である場
合も含む。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to transmitting radio waves during a fall by dropping from a launch vehicle, an aircraft, or the like, and receiving the radio waves at a mobile unit (car, aircraft, flying object, ship, etc.) or a receiving station on the ground. The present invention relates to a radio wave transmission method intended to perform The term "receiving station" used herein includes a case where a receiving station for jamming radio waves not intended for receiving from the apparatus of the present invention is intended.

【0002】[0002]

【従来の技術】従来の打ち上げロケットや航空機等から
の投下で、落下中に電波を送信し、移動体(車、航空
機、飛翔体、船舶など)や地上の受信局で電波受信を行
うことを目的とした電波送信方法として、自己の方位基
準が不明のまま無指向性のアンテナを用い全方位送信す
る電波送信方法があった。その構成を図7に示してい
る。図7において、1は空中投下型電波機器、4はその
中に搭載されている送信機、14は無指向性のアンテ
ナ、8は落下傘、9は送信電波、2は受信局である。
2. Description of the Related Art Radio waves are transmitted while falling from a conventional launch vehicle or aircraft, and received by a mobile unit (car, aircraft, flying object, ship, etc.) or a receiving station on the ground. As a target radio wave transmission method, there has been a radio wave transmission method in which omnidirectional transmission is performed using an omni-directional antenna with its own azimuth reference unknown. The configuration is shown in FIG. In FIG. 7, 1 is an air-drop radio device, 4 is a transmitter mounted therein, 14 is a non-directional antenna, 8 is a parachute, 9 is a transmission radio wave, and 2 is a receiving station.

【0003】上記構成の他に、例えば、装置内部にジャ
イロスコープ回路を有し、基準方位が判明している状態
からの累積の回転角を積分算出して、空中浮遊時の自己
方位角度基準を用いる方法や、さらに、地磁気センサに
よる自己方位基準検出であるが、回転数を求めることを
目的とし、空中線の指向性制御等への応用に際しては、
基準方位として使用するのではなく、ジャイロスコープ
装置の代用として自己回転数の計測記憶累積分だけ指向
性空中線を逆回転させる方法等があった。
[0003] In addition to the above configuration, for example, a gyroscope circuit is provided inside the device, and the cumulative rotation angle from a state in which the reference azimuth is known is integrated and calculated, and the self azimuth angle reference when floating in the air is calculated. The method used, and furthermore, self-azimuth reference detection by a geomagnetic sensor, but for the purpose of finding the number of revolutions, when applied to antenna directivity control, etc.
Instead of using the reference azimuth, there has been a method in which the directional antenna is reversely rotated by an amount equivalent to the measurement and accumulation of the self-rotational speed instead of the gyroscope device.

【0004】[0004]

【発明が解決しようとする課題】従来、航空機や気球と
いった空中移動の乗り物そのものからの電波機器による
電波送信は通信等で多く存在してきたが、近年、電子・
電気機器の小型軽量化技術により航空機や気球等からの
落下傘や安定翼等をもっただけの空中投下物や、観測デ
ータの送信や電波妨害装置などの電波送信の機器を搭載
した小型ロケット弾や砲弾が存在している。
Conventionally, there have been many radio wave transmissions by radio equipment from airborne vehicles such as airplanes and balloons in communication and the like.
Small rockets equipped with airdrops that have parachute and stable wings from aircraft and balloons, and radio wave transmission devices such as transmission of observation data and radio wave jamming devices, using technology to reduce the size and weight of electrical equipment. A shell is present.

【0005】これらの機器では、搭載制限による小型軽
量化、装置のコストダウン等の理由と、空中投下中に自
己の方位基準が容易に得られないことを理由に、従来、
図7のような無指向性アンテナ14が採用され、全方位
に電波送信する方法が採られていた。この方法の場合、
指向性アンテナと比べ送信機4の出力は全方位放射のた
め、特定の受信局に対しては弱い電波とならざるを得な
い問題点があった。
Conventionally, these devices have been conventionally used for reasons such as a reduction in size and weight due to mounting restrictions, a reduction in the cost of the device, and the fact that it is not easy to obtain their own azimuth reference during airdrop.
An omnidirectional antenna 14 as shown in FIG. 7 has been adopted, and a method of transmitting radio waves in all directions has been adopted. In this case,
Since the output of the transmitter 4 is omnidirectional radiation as compared with the directional antenna, there is a problem that a weak radio wave must be transmitted to a specific receiving station.

【0006】また、ジャイロスコープ回路や地磁気セン
サと、半導体メモリ記憶を組み合わせた積分または積算
算出による自己方位基準算出の方法は、積分と積算で誤
差が著しく累積するという問題があった。
Further, the self-azimuth reference calculation method by integration or integration calculation combining a gyroscope circuit or a geomagnetic sensor with semiconductor memory storage has a problem that errors are significantly accumulated in integration and integration.

【0007】この発明の目的は、前記従来技術の問題点
を解消し、同じ送信機を使用した場合でも、受信局に対
し無指向性アンテナに比べ強い電波を送信可能な方法を
提供し、また従来の指向性アンテナを用いた送信方法と
比較してもより指向制の程度を向上させ、強い電波を送
信可能とする電波送信方法を提供するものである。
An object of the present invention is to solve the above-mentioned problems of the prior art, and to provide a method capable of transmitting a radio wave stronger than a nondirectional antenna to a receiving station even when the same transmitter is used. An object of the present invention is to provide a radio wave transmission method that can improve the degree of directivity and can transmit a strong radio wave as compared with a conventional transmission method using a directional antenna.

【0008】[0008]

【課題を解決するための手段】この発明に係る電波送信
方法は、指向性アンテナを備えた空中投下型電波機器を
打ち上げロケットや航空機等から投下し、その落下中に
上記電波機器から電波を送信し、移動体(車、航空機、
飛翔体、船舶など)や地上の受信局で受信を行うものに
おいて、空中投下型電波機器には空中での自己方位の取
得のために地磁気センサを搭載し、この地磁気センサの
方位を自己基準として受信局方向へ指向性アンテナを向
けるに際し、指向性アンテナの正回転または逆回転のい
ずれかの内、受信局方向への最小動作角を算出し、その
最小動作角に従って指向性アンテナ軸の回転制御を行う
ようにしたものである。
According to a radio transmission method according to the present invention, an air-drop radio device equipped with a directional antenna is dropped from a launch vehicle or an aircraft, and radio waves are transmitted from the radio device during the fall. Mobile objects (cars, aircraft,
(E.g., flying objects, ships, etc.) and receiving stations on the ground, airborne radio equipment is equipped with a geomagnetic sensor to acquire its own orientation in the air, and the orientation of this geomagnetic sensor is used as a self-reference. When directing the directional antenna toward the receiving station, the minimum operation angle toward the receiving station is calculated from either the forward rotation or the reverse rotation of the directional antenna, and the rotation of the directional antenna axis is controlled according to the minimum operation angle. Is performed.

【0009】また、空中投下型電波機器に遠隔方位操作
受信部を搭載し、この遠隔方位操作受信部を通して、地
磁気センサによるアンテナ軸回転制御とは別に、随時ア
ンテナ軸回転制御を行い指向性アンテナの方向を変更可
能としたものである。
[0009] Further, a remote azimuth operation receiving unit is mounted on the air-drop radio device, and through this remote azimuth operation receiving unit, antenna axis rotation control is performed at any time separately from the antenna axis rotation control by the geomagnetic sensor to control the directional antenna. The direction can be changed.

【0010】また、落下中の空中投下型電波機器の自己
回転による地磁気センサの出力データ変化に応じてアン
テナ軸回転制御を行い、指向性アンテナ方向を受信局方
向へ向けるようにしたものである。
In addition, the antenna axis rotation is controlled in accordance with a change in the output data of the geomagnetic sensor due to the self-rotation of the dropped air-drop radio equipment, so that the directional antenna is directed toward the receiving station.

【0011】また、落下中の空中投下型電波機器の自己
回転による地磁気センサの出力データの履歴から、落下
中の空中投下型電波機器の自己回転の傾向(定角速度、
定角加速度や落下傘降下時などで発生しやすい定ねじれ
振動、ねじれ減衰振動など)を計算予測し、この予測値
と地磁気センサの出力とによりアンテナ軸回転制御を行
い、指向性アンテナを受信局方向へ向けるようにしたも
のである。
Also, based on the history of the output data of the geomagnetic sensor due to the self-rotation of the falling air-drop radio equipment, the tendency of the self-rotation of the falling air-drop radio equipment (constant angular velocity,
Calculates and predicts constant torsional vibration, torsional damping vibration, etc., which are likely to occur at constant angular acceleration, parachute descent, etc.), controls the antenna axis rotation based on this predicted value and the output of the geomagnetic sensor, and moves the directional antenna toward the receiving station. It is intended to turn to.

【0012】また、遠隔方位操作受信部を備え、この遠
隔方位操作受信部を通して、地磁気センサによるアンテ
ナ軸回転制御とは別に、随時アンテナ軸回転制御を行い
指向性アンテナ方向を変更可能としたものである。
Also, a remote azimuth operation receiving section is provided, and through this remote azimuth operation receiving section, antenna axis rotation control can be performed at any time separately from the antenna axis rotation control by the geomagnetic sensor so that the direction of the directional antenna can be changed. is there.

【0013】また、指向性アンテナを備えた空中投下型
電波機器を打ち上げロケットや航空機等から投下し、そ
の落下中に上記電波機器から電波を送信し、移動体
(車、航空機、飛翔体、船舶など)や地上の受信局で受
信を行うものにおいて、上記空中投下型電波機器はプロ
ペラもしくは回転安定翼を持ち、空中投下型電子機器の
回転1周ごとに電子機器の指向性アンテナから複数また
は単独の受信局に電波を送信するようにしたものであ
る。
In addition, an air-drop radio device equipped with a directional antenna is dropped from a launch vehicle, an aircraft, or the like, and a radio wave is transmitted from the radio device while the radio device is falling, and the mobile device (car, aircraft, flying object, ship) The above-mentioned air-drop radio equipment has a propeller or a rotation stabilizing wing, and a plurality of or a single directional antenna from the directional antenna of the air-drop electronic equipment rotates every rotation of the air-drop electronic equipment. The radio wave is transmitted to the receiving station.

【0014】[0014]

【発明の実施の形態】実施の形態1.この発明の実施の
形態1を図について説明する。図1において、1は空中
投下型電波機器、2は受信局、3は上記空中投下型電波
機器1に搭載された指向性アンテナ、4は送信機、5は
モータ、6はアンテナ軸回転制御部、7は地磁気センサ
である。8は落下傘、9は指向性アンテナ3から放射さ
れる送信電波である。
DESCRIPTION OF THE PREFERRED EMBODIMENTS Embodiment 1 Embodiment 1 of the present invention will be described with reference to the drawings. In FIG. 1, 1 is an air-drop radio device, 2 is a receiving station, 3 is a directional antenna mounted on the air-drop radio device 1, 4 is a transmitter, 5 is a motor, and 6 is an antenna axis rotation control unit. , 7 are geomagnetic sensors. 8 is a parachute, 9 is a transmission radio wave radiated from the directional antenna 3.

【0015】次に動作を説明する。本実施の形態1で
は、一例として落下傘8で投下する空中投下型電波機器
1を図示しているが、内部に、送信機4、地磁気センサ
7、アンテナ軸回転制御部6、モータ5、指向性アンテ
ナ3を搭載し、予め投下場所からの受信局方位がアンテ
ナ軸回転制御部6にデータとして記憶されているもので
あればどのような投下型電波機器でもよい。
Next, the operation will be described. In the first embodiment, the air-drop radio device 1 that is dropped by the parachute 8 is shown as an example, but the transmitter 4, the geomagnetic sensor 7, the antenna shaft rotation control unit 6, the motor 5, the directivity Any type of drop-type radio equipment may be used as long as the antenna 3 is mounted and the direction of the receiving station from the drop location is stored in advance in the antenna axis rotation control unit 6 as data.

【0016】落下の最中には、空中投下型電波機器1は
地面に対しての相対的な自己方位が失われているため、
例えば北のような基準方位が不明である。そのため地磁
気センサ7で、磁北の方向を求め、その方向を基準にア
ンテナ軸回転制御部6で指向性アンテナ3を向ける方向
を正回転または逆回転させるが、その際、どちらがより
最小動作の回転角度か、そしてその回転角度は何度かを
計算し、その最小動作角度に従って必要なだけモータ5
を回転する。ここで、アンテナ軸回転制御部6の内部で
磁北と真北とのズレを計算補正してもよい。なお、地磁
気センサ7からアンテナ軸制御部6を経由して指向性ア
ンテナ3を回転させる一連の方法は、アナログ制御回路
またはソフトウェアを利用するデジタル制御回路のいず
れでもよい。さらに、その制御回路にはフィードバック
回路を含むもの、含まないものいずれでもよい。
During the fall, the air-drop radio device 1 loses its own orientation relative to the ground.
For example, the reference direction such as north is unknown. Therefore, the direction of magnetic north is determined by the geomagnetic sensor 7, and the direction in which the directional antenna 3 is directed is rotated forward or backward by the antenna axis rotation control unit 6 based on the direction. And the rotation angle is calculated several times, and the motor 5 is required only according to the minimum operation angle.
To rotate. Here, the deviation between magnetic north and true north may be calculated and corrected inside the antenna axis rotation control unit 6. Note that a series of methods for rotating the directional antenna 3 from the geomagnetic sensor 7 via the antenna axis control unit 6 may be either an analog control circuit or a digital control circuit using software. Further, the control circuit may or may not include a feedback circuit.

【0017】このような構成による送信方法では、空中
投下型電波機器1の投下後、指向性アンテナ3は常に受
信局2に向けて送信電波が放射されることになり、特定
方位に存在する受信局2に対して、指向性アンテナ3に
よる強い送信電波9の放射が可能となる。
In the transmission method having such a configuration, the directional antenna 3 always emits a transmission radio wave toward the receiving station 2 after the air-drop radio device 1 is dropped, and the reception radio wave existing in a specific direction is received. The directional antenna 3 can radiate the strong transmission radio wave 9 to the station 2.

【0018】実施の形態2.図2はこの発明の実施の形
態2を示すもので、図において、10は移動受信局、1
1は空中投下型電波機器1に搭載されている遠隔方位操
作受信部、12は例えば地上に設置されている遠隔方位
操作送信部である。
Embodiment 2 FIG. FIG. 2 shows a second embodiment of the present invention, in which 10 is a mobile receiving station, 1
Reference numeral 1 denotes a remote azimuth operation receiving unit mounted on the air-drop radio device 1, and reference numeral 12 denotes a remote azimuth operation transmitting unit installed on the ground, for example.

【0019】上記実施の形態1では、空中投下型電波機
器1が落下中に風に流されて受信局との方位が変わった
り、投下の前または落下中に移動受信局10が移動した
場合、指向性アンテナ3が受信局10の方位方向からは
ずれるが、空中投下型電波機器1に搭載されたアンテナ
を含む遠隔方位操作受信部11により、地上等に設置さ
れた外部のアンテナを含む遠隔方位操作送信部12でア
ンテナ軸回転制御部6に新しい受信局方位のデータを送
信してデータを更新し、指向性アンテナ3をより正確に
移動受信局10方向へ指向させることにより、強い送信
電波9の放射を行うことが可能となる。
In the first embodiment, when the air-drop radio device 1 is swept by the wind during a fall to change the azimuth with the receiving station, or when the mobile receiving station 10 moves before the drop or during the drop, Although the directional antenna 3 deviates from the azimuth direction of the receiving station 10, the remote azimuth operation including the external antenna installed on the ground or the like is performed by the remote azimuth operation receiving unit 11 including the antenna mounted on the airborne radio wave device 1. The transmitting unit 12 transmits data of the new receiving station direction to the antenna axis rotation control unit 6 to update the data, and directs the directional antenna 3 toward the mobile receiving station 10 more accurately. It is possible to emit radiation.

【0020】実施の形態3.図3はこの発明の実施の形
態3を示すものである。この実施の形態では、地磁気セ
ンサ7による磁北の取得を落下中に繰り返すことによ
り、落下中の空中投下型電波機器1の自己回転に対して
も指向性アンテナの方位ずれを修正するようにしたもの
である。図3において、矢印Aのように空中投下型電波
機器1が回転した場合、地磁気センサ7の出力によりア
ンテナ軸回転制御部6を制御し、指向性アンテナ3の方
向を随時修正し、常に受信局2の方向を向くようにす
る。
Embodiment 3 FIG. 3 shows a third embodiment of the present invention. In this embodiment, the acquisition of magnetic north by the geomagnetic sensor 7 is repeated during a fall, so that the directional deviation of the directional antenna is corrected even for the self-rotation of the air-drop radio device 1 during the fall. It is. In FIG. 3, when the air-drop radio device 1 rotates as indicated by an arrow A, the antenna axis rotation control unit 6 is controlled by the output of the geomagnetic sensor 7, the direction of the directional antenna 3 is corrected as needed, and the receiving station is constantly controlled. Turn to the direction of 2.

【0021】実施の形態4.図4はこの発明の実施の形
態4を示すものである。図において、13はプロペラも
しくは回転安定翼、15は空中投下型電波機器1に搭載
された予測制御計算部であり、図3(a)はねじれ振動
投下の例を、図3(b)は定角速度や定角加速度投下の
例を示している。
Embodiment 4 FIG. FIG. 4 shows a fourth embodiment of the present invention. In the figure, 13 is a propeller or a rotation stabilizing wing, 15 is a predictive control calculation unit mounted on the air-drop radio equipment 1, FIG. 3 (a) shows an example of torsional vibration drop, and FIG. An example of dropping an angular velocity or a constant angular acceleration is shown.

【0022】本実施の形態4では、上記実施の形態3と
同様、磁気センサ7による磁北の取得を落下中に繰り返
すことにより、地磁気センサ7の取得データの履歴か
ら、空中投下型電波機器1の回転運動の傾向(定角速度
運動、定角加速度運動、定ねじれ振動運動、ねじれ減衰
振動運動等)を読み取り、瞬時先の自己回転角度の予測
角16(破線で示す)を予測制御計算部15で演算して
予測し、指向性アンテナ3の方位ずれを予め予測値で修
正しておくことにより修正の時間遅れを少なくしてより
正確に修正することが可能となる。
In the fourth embodiment, as in the third embodiment, the acquisition of magnetic north by the magnetic sensor 7 is repeated during the fall, so that the history of the acquired data of the geomagnetic sensor 7 allows the The tendency of the rotational movement (constant angular velocity movement, constant angular acceleration movement, constant torsional vibration movement, torsional damping vibration movement, etc.) is read, and the predicted angle 16 (shown by a broken line) of the instantaneous self-rotation angle is calculated by the prediction control calculation unit 15. By calculating and predicting and correcting the azimuth deviation of the directional antenna 3 with a predicted value in advance, it is possible to reduce the time delay of the correction and correct the correction more accurately.

【0023】実施の形態5.図5はこの発明の実施の形
態5を示すものである。本実施の形態は、上記実施の形
態の2と実施の形態4を組み合わせたもので、遠隔方位
操作送信部12および受信部11による移動受信局10
方向への指向性アンテナ3の制御と、予測制御計算部1
5による指向性アンテナ3の方向修正との両方で、移動
受信局10に対してもより正確でより迅速な指向性アン
テナ3による強い送信電波9の放射が可能となる。
Embodiment 5 FIG. 5 shows a fifth embodiment of the present invention. The present embodiment is a combination of Embodiment 2 and Embodiment 4 described above, and includes a mobile receiving station 10 by a remote direction operation transmitting unit 12 and a receiving unit 11.
The control of the directional antenna 3 in the direction and the prediction control calculation unit 1
Both the correction of the direction of the directional antenna 3 and the direction of the directional antenna 3 enable the mobile receiving station 10 to emit the strong transmission radio wave 9 more accurately and more quickly by the directional antenna 3.

【0024】実施の形態6.図6はこの発明の実施の形
態6を示すものである。本実施の形態の空中投下型電波
機器1はプロペラもしくは回転翼13により投下時に回
転するものであり、内部には送信機4と指向性アンテナ
3のみを搭載している。
Embodiment 6 FIG. FIG. 6 shows a sixth embodiment of the present invention. The air-drop radio device 1 according to the present embodiment rotates when dropped by a propeller or a rotary wing 13, and has only a transmitter 4 and a directional antenna 3 mounted therein.

【0025】これは受信局側での電波受信が間欠的に行
われればよい場合に適用されるもので、空中投下型電波
機器1は落下中に回転しながら電波送信を行い、回転1
周毎にこれを複数または単独の受信局で受信する。この
実施の形態では、複数の受信局に対して強い間欠の電波
送信が可能となる。
This is applied to the case where the radio wave reception at the receiving station only needs to be performed intermittently. The air-drop radio equipment 1 performs radio wave transmission while rotating while falling, and
This is received by a plurality of or a single receiving station every week. In this embodiment, strong intermittent radio wave transmission to a plurality of receiving stations is possible.

【0026】[0026]

【発明の効果】以上のように、この発明によれば、指向
性アンテナを使用することが可能となり、同一の送信機
を用いた場合でも従来と比較して受信局に対し、より強
い電波送信が実現できる。
As described above, according to the present invention, a directional antenna can be used, and even when the same transmitter is used, a stronger radio wave transmission to a receiving station can be performed as compared with the conventional one. Can be realized.

【0027】また、例えば地上から、空中投下型電子機
器に搭載された遠隔方位操作受信部を通して指向性アン
テナ方向を変更できるので、受信局の移動等にも対応し
て受信局へ向けて確実に電波送信ができる。
Also, since the direction of the directional antenna can be changed from the ground through a remote azimuth operation receiving unit mounted on the air-drop type electronic device, it is possible to reliably move toward the receiving station in response to movement of the receiving station. Radio transmission is possible.

【0028】また、空中投下型電子機器の落下中の自己
回転に追従する出力を地磁気センサから取り出すことに
より、指向精度の高い電波送信が可能である。
In addition, by extracting from the geomagnetic sensor an output that follows the self-rotation of the air-drop type electronic device during its fall, radio transmission with high directivity is possible.

【0029】また、地磁気センサの取得データ履歴から
空中投下型電子機器の落下中の自己回転を予測すること
により、指向精度が高くかつ速動性のある指向性アンテ
ナによる電波送信が可能である。
Further, by predicting the self-rotation of the aerial drop-type electronic device during the fall from the history of data acquired by the geomagnetic sensor, it is possible to transmit radio waves with a directional antenna having high directivity and high speed.

【0030】また、指向性アンテナを用いて、複数の受
信局に間欠的に強い電波送信を行うことができる。
Also, strong radio waves can be transmitted intermittently to a plurality of receiving stations by using a directional antenna.

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

【図1】 この発明の実施の形態1に係る電波送信方法
を示す概念図である。
FIG. 1 is a conceptual diagram showing a radio wave transmission method according to Embodiment 1 of the present invention.

【図2】 この発明の実施の形態2に係る電波送信方法
を示す概念図である。
FIG. 2 is a conceptual diagram showing a radio wave transmission method according to Embodiment 2 of the present invention.

【図3】 この発明の実施の形態3に係る電波送信方法
を示す概念図である。
FIG. 3 is a conceptual diagram showing a radio wave transmission method according to Embodiment 3 of the present invention.

【図4】 この発明の実施の形態4に係る電波送信方法
を示す概念図である。
FIG. 4 is a conceptual diagram showing a radio wave transmission method according to Embodiment 4 of the present invention.

【図5】 この発明の実施の形態5に係る電波送信方法
を示す概念図である。
FIG. 5 is a conceptual diagram showing a radio wave transmission method according to Embodiment 5 of the present invention.

【図6】 この発明の実施の形態6に係る電波送信方法
を示す概念図である。
FIG. 6 is a conceptual diagram showing a radio wave transmission method according to Embodiment 6 of the present invention.

【図7】 従来の電波送信方法を示す概念図である。FIG. 7 is a conceptual diagram showing a conventional radio wave transmission method.

【符号の説明】[Explanation of symbols]

1 空中投下型電波機器、 2 受信局、
3 指向性アンテナ、 4 送信機、
5 モータ、 6 アンテナ
軸回転制御部、7 地磁気センサ、
8 落下傘、9 送信電波、
10 移動受信局、11 アンテナを含む遠隔方位操作
受信部、12 アンテナを含む遠隔方位操作送信部、1
3 プロペラもしくは回転安定翼、15 予測制御計算
部、 16 予測角。
1 air-drop radio equipment, 2 receiving station,
3 directional antennas, 4 transmitters,
5 motor, 6 antenna axis rotation controller, 7 geomagnetic sensor,
8 parachute, 9 transmitted radio wave,
REFERENCE SIGNS LIST 10 mobile receiving station, 11 remote directional operation receiving section including antenna, 12 remote directional operation transmitting section including antenna, 1
3 propeller or rotation stabilizing wing, 15 predictive control calculator, 16 predictive angle.

Claims (6)

【特許請求の範囲】[Claims] 【請求項1】 指向性アンテナを備えた空中投下型電波
機器を打ち上げロケットや航空機等から投下し、その落
下中に上記電波機器から電波を送信し、移動体(車、航
空機、飛翔体、船舶など)や地上の受信局で受信を行う
電波送信方法において、空中投下型電波機器には空中で
の自己方位の取得のために地磁気センサを搭載し、この
地磁気センサの方位を自己基準として受信局方向へ指向
性アンテナを向けるに際し、指向性アンテナの正回転ま
たは逆回転のいずれかの内、受信局方向への最小動作角
を算出し、その最小動作角に従って指向性アンテナ軸の
回転制御を行うようにしたことを特徴とする電波送信方
法。
An air-drop radio device equipped with a directional antenna is dropped from a launch vehicle, an aircraft, or the like, and a radio wave is transmitted from the radio device during the fall, and the mobile device (car, aircraft, flying object, ship, etc.) Radio wave transmission method for receiving at a receiving station on the ground, etc., the airborne radio equipment is equipped with a geomagnetic sensor to acquire its own direction in the air, and the receiving station uses the direction of this geomagnetic sensor as its own reference. When directing the directional antenna in the direction, either the forward rotation or the reverse rotation of the directional antenna, the minimum operation angle toward the receiving station is calculated, and the rotation of the directional antenna axis is controlled according to the minimum operation angle. A radio wave transmission method characterized in that:
【請求項2】 空中投下型電波機器に遠隔方位操作受信
部を搭載し、この遠隔方位操作受信部を通して、地磁気
センサによるアンテナ軸回転制御とは別に、随時アンテ
ナ軸回転制御を行い指向性アンテナの方向を変更可能と
したことを特徴とする請求項1記載の電波送信方法。
2. An airborne radio wave device is equipped with a remote direction operation receiving unit, and through this remote direction operation receiving unit, independently of antenna axis rotation control by a geomagnetic sensor, performs antenna axis rotation control at any time to control a directional antenna. 2. The radio wave transmission method according to claim 1, wherein the direction can be changed.
【請求項3】 落下中の空中投下型電波機器の自己回転
による地磁気センサの出力データ変化に応じてアンテナ
軸回転制御を行い、指向性アンテナ方向を受信局方向へ
向けるようにしたことを特徴とする請求項1または請求
項2記載の電波送信方法。
3. An antenna axis rotation control is performed in accordance with a change in output data of a geomagnetic sensor due to a self-rotation of a dropped air-drop radio device, and a directional antenna is directed to a receiving station. The radio wave transmission method according to claim 1 or 2, wherein:
【請求項4】 落下中の空中投下型電波機器の自己回転
による地磁気センサの出力データの履歴から、落下中の
空中投下型電波機器の自己回転の傾向(定角速度、定角
加速度や落下傘降下時などで発生しやすい定ねじれ振
動、ねじれ減衰振動など)を計算予測し、この予測値と
地磁気センサの出力とによりアンテナ軸回転制御を行
い、指向性アンテナを受信局方向へ向けるようにしたこ
とを特徴とする請求項3記載の電波送信方法。
4. The tendency of self-rotation of a falling airdrop type radio device during self-rotation (constant angular velocity, constant angular acceleration, Calculation and prediction of constant torsional vibration, torsional damping vibration, etc., which are likely to occur due to such factors as, etc., and control the antenna axis rotation based on this predicted value and the output of the geomagnetic sensor, and direct the directional antenna toward the receiving station. The radio wave transmission method according to claim 3, wherein:
【請求項5】 遠隔方位操作受信部を備え、この遠隔方
位操作受信部を通して、地磁気センサによるアンテナ軸
回転制御とは別に、随時アンテナ軸回転制御を行い指向
性アンテナ方向を変更可能としたことを特徴とする請求
項4記載の電波送信方法。
5. A remote azimuth operation receiving unit, wherein the antenna directional rotation control can be performed at any time through the remote azimuth operation receiving unit, separately from the antenna axis rotation control by the geomagnetic sensor, so that the directional antenna direction can be changed. The radio wave transmission method according to claim 4, wherein:
【請求項6】 指向性アンテナを備えた空中投下型電波
機器を打ち上げロケットや航空機等から投下し、その落
下中に上記電波機器から電波を送信し、移動体(車、航
空機、飛翔体、船舶など)や地上の受信局で受信を行う
電波送信方法において、上記空中投下型電波機器はプロ
ペラもしくは回転安定翼を持ち、空中投下型電子機器の
回転1周ごとに電子機器の指向性アンテナから複数また
は単独の受信局に電波を送信するようにしたことを特徴
とする電波送信方法。
6. An air-drop radio device equipped with a directional antenna is dropped from a launch vehicle, an aircraft, or the like, and a radio wave is transmitted from the radio device during the fall, and the mobile device (car, aircraft, flying object, ship) Radio wave transmission method for receiving at a receiving station on the ground, the above-mentioned air-drop radio equipment has a propeller or a rotation stabilizing wing, and a plurality of directional antennas of the electronic equipment are provided for each rotation of the air-drop electronic equipment. Alternatively, a radio wave transmission method characterized by transmitting radio waves to a single receiving station.
JP29890399A 1999-10-20 1999-10-20 Radio transmission method Pending JP2001119227A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP29890399A JP2001119227A (en) 1999-10-20 1999-10-20 Radio transmission method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP29890399A JP2001119227A (en) 1999-10-20 1999-10-20 Radio transmission method

Publications (1)

Publication Number Publication Date
JP2001119227A true JP2001119227A (en) 2001-04-27

Family

ID=17865670

Family Applications (1)

Application Number Title Priority Date Filing Date
JP29890399A Pending JP2001119227A (en) 1999-10-20 1999-10-20 Radio transmission method

Country Status (1)

Country Link
JP (1) JP2001119227A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010259069A (en) * 2009-04-27 2010-11-11 Honeywell Internatl Inc Self-stabilizing antenna base
JP2015124938A (en) * 2013-12-26 2015-07-06 株式会社Ihiエアロスペース Top attack device and top attack device control method

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010259069A (en) * 2009-04-27 2010-11-11 Honeywell Internatl Inc Self-stabilizing antenna base
JP2015124938A (en) * 2013-12-26 2015-07-06 株式会社Ihiエアロスペース Top attack device and top attack device control method

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