JPS63169200A - Constructing method for large capacity communication network for emergency use - Google Patents
Constructing method for large capacity communication network for emergency useInfo
- Publication number
- JPS63169200A JPS63169200A JP62000754A JP75487A JPS63169200A JP S63169200 A JPS63169200 A JP S63169200A JP 62000754 A JP62000754 A JP 62000754A JP 75487 A JP75487 A JP 75487A JP S63169200 A JPS63169200 A JP S63169200A
- Authority
- JP
- Japan
- Prior art keywords
- flying object
- destination
- communication network
- constructing
- communication
- 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
Links
- 238000000034 method Methods 0.000 title claims abstract description 20
- 230000005540 biological transmission Effects 0.000 claims abstract description 18
- 239000013307 optical fiber Substances 0.000 claims abstract description 10
- 238000001514 detection method Methods 0.000 claims description 2
- 238000006243 chemical reaction Methods 0.000 description 10
- 230000003287 optical effect Effects 0.000 description 6
- 238000010586 diagram Methods 0.000 description 3
- 230000007123 defense Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 230000003213 activating effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
Landscapes
- Electric Cable Installation (AREA)
- Selective Calling Equipment (AREA)
Abstract
Description
【発明の詳細な説明】
(産業上の利用分野)
本発明は、災害や防衛上の要求から、緊急に大容量の通
信網を設置する必要が生じた場合に使用される、緊急用
大容量通信網の構築方法に関する。Detailed Description of the Invention (Industrial Application Field) The present invention is an emergency large-capacity communication network that is used when it is necessary to urgently install a large-capacity communication network due to disaster or defense requirements. Related to communication network construction methods.
(従来技術)
従来、災害対策などのために大容量の通信網を設置する
必要が生じた場合、地表に沿って通信用ケーブルを順次
施設する以外に方法はなく、緊急を要する場合にも、た
とえば施設用の車両を利用しても、施設に非常に時間が
かかる、という問題がある。緊急目的のために、電波に
よる通信網の設置も考えられるが、これは、音声程度の
小容量の通信網の設置には使用できても、画像情報の伝
達のための通信網の設置には適していない。また、電波
は、防衛上の見地からすると、電波妨害などを受ける恐
れもある。(Prior art) Conventionally, when it became necessary to install a large-capacity communication network for disaster countermeasures, etc., there was no other way than to install communication cables sequentially along the ground. For example, even if a facility vehicle is used, there is a problem in that it takes a very long time to get to the facility. For emergency purposes, it is possible to install a communication network using radio waves, but although this can be used to install a communication network with a small capacity such as voice, it is not suitable for setting up a communication network for transmitting image information. Not suitable. Furthermore, from a defense standpoint, radio waves may be subject to interference.
(発明が解決しようとする問題点)
本発明は、従来技術の上述した問題を解決し、広い範囲
にわたり迅速に大容量の通信網を設置することができる
緊急大容量通信網の構築方法を提供することを目的とす
る。(Problems to be Solved by the Invention) The present invention solves the above-mentioned problems of the prior art and provides a method for constructing an emergency large-capacity communication network that can quickly set up a large-capacity communication network over a wide area. The purpose is to
(問題点を解決するための手段)
上記問題点を解決するため、本発明による方法は、通信
伝達用の線をミサイルのような飛しょう体により、目的
地まで展開することを特徴とする。(Means for Solving the Problems) In order to solve the above-mentioned problems, the method according to the present invention is characterized in that a line for communication transmission is deployed to the destination by a projectile such as a missile.
すなわち、本発明による緊急大容量通信網の構築方法は
、通信伝達用の線を巻いたリールと、目標検出手段と、
軟着陸補助手段と、遠隔操縦手段とを存する飛しょう体
を、前記通信伝達用の線を地上に繰り出しながら目的地
に向けて飛行させ、前記遠隔操縦装置により前記目的地
に到達したとき前記軟着陸装置を作動させて前記飛しょ
う体を目的地に着陸させ、前記通信伝達用の線を飛しょ
う体発射地点と前記目的地の送受信設備とに接続するこ
とからなるものである。この場合、通信伝達用の線とし
ては、伝達容量と重量の関係から、光ブアイバを使用す
ることが好ましく、光ファイバは、一端を飛しょう体発
射地点の送受信設備に接続しておき、この送受信設備と
の間に伝達される信号により、飛しょう体を遠隔操縦す
ることが望ましい。That is, the method for constructing an emergency large-capacity communication network according to the present invention includes a reel wound with a wire for communication transmission, target detection means,
A spacecraft having a soft landing assisting means and a remote control means is flown toward a destination while extending the communication transmission line above the ground, and when the spacecraft reaches the destination using the remote control device, the soft landing device The method consists of activating the aircraft to land the aircraft at its destination, and connecting the communications transmission line to the aircraft launch site and the transmitting/receiving equipment at the destination. In this case, it is preferable to use an optical fiber as the line for communication transmission due to the relationship between transmission capacity and weight.One end of the optical fiber is connected to the transmission and reception equipment at the projectile launch point, and the transmission and reception It is desirable to remotely control the flying object by signals transmitted to and from the equipment.
(作 用)
本発明の方法においては、飛しよう体により通信伝達用
の線を繰り出しながら飛しよう体を飛行させ、目的地に
到達したとき、パラシュートのような軟着陸手段を操作
して、飛しよう体を目的地に軟着陸させる。そして、目
的地にあらかじめ準備した送受信設備を飛しよう体の接
続用端子に接続することにより通信網を完成させること
ができる。(Function) In the method of the present invention, the flying object is made to fly while sending out lines for communication transmission, and when it reaches the destination, it operates a soft landing means such as a parachute to fly away. Make a soft landing with your body at your destination. The communication network can then be completed by connecting the transmitting/receiving equipment prepared in advance at the destination to the connecting terminals of the flying object.
(実施例)
第1図は、本発明の方法に使用される飛しよう体及び発
射地点の送受信設備の一例を示す。飛しょう体は、ロケ
ットなどの推進手段を有する飛しょう鉢本体1からなり
、該層しよう鉢本体10尾部には光ファイバ2aを巻い
たリール2が搭載され、前部には位置検出手段であるテ
レビカメラ3が搭載されている。また、本体1の中間部
には、軟着陸手段を構成するバラシュート4が格納され
ている。テレビカメラ3は、光電変換装置5に接続され
、該テレビカメラ3が発生する画像電気信号は、光電変
換装置5により光信号に変換される。(Example) FIG. 1 shows an example of a flying vehicle used in the method of the present invention and a transmitting/receiving equipment at a launch site. The flying body consists of a flying bowl main body 1 having a propulsion means such as a rocket, a reel 2 wound with an optical fiber 2a is mounted on the tail of the layered flying bowl main body 10, and a position detecting means is mounted on the front. Equipped with 3 TV cameras. Further, a barachute 4 constituting a soft landing means is stored in the intermediate portion of the main body 1. The television camera 3 is connected to a photoelectric conversion device 5, and the image electrical signal generated by the television camera 3 is converted into an optical signal by the photoelectric conversion device 5.
また、搭載機器の作動のために、本体1には電源6が搭
載されている。Further, the main body 1 is equipped with a power source 6 for operating the on-board equipment.
飛しょう体発射地点の送受信設備Aは、飛しょう鉢本体
1に搭載されたリール2からの光ファイバ2aに接続さ
れる光電変換装置7を有し、この光電変換装置7は送受
信装置8、飛しょう体操縦装置9及び表示装置10に接
続されている。これら地上の機器は、電源11からの電
力の供給を受ける。光電変換装置7は、光ファイバ2a
から送られて来る光信号を電気信号に変換して送受信装
装置8、操縦装置9、表示装置10に送る。また、光電
変換装置7は、送受信装置8及び操縦装置9からの信号
を光信号に変換して飛しよう体に送る。The transmitting/receiving equipment A at the projectile launching point has a photoelectric conversion device 7 connected to the optical fiber 2a from the reel 2 mounted on the flyball body 1, and this photoelectric conversion device 7 is connected to the transmitting/receiving device 8 and the flying ball. It is connected to a body control device 9 and a display device 10. These devices on the ground receive power from the power source 11. The photoelectric conversion device 7 is an optical fiber 2a
The optical signal sent from the controller is converted into an electrical signal and sent to the transmitter/receiver device 8, the control device 9, and the display device 10. Further, the photoelectric conversion device 7 converts signals from the transmitting/receiving device 8 and the control device 9 into optical signals and sends the optical signals to the flying object.
飛しょう鉢本体1には、光電変換装置6に接続された外
部接続用の接続端子12と、該接続端子12に接続する
ことのできる送受信装置13が搭載されている。The flyball body 1 is equipped with a connection terminal 12 for external connection connected to the photoelectric conversion device 6, and a transmitting/receiving device 13 that can be connected to the connection terminal 12.
第2図は、第1図に示す飛しょう体を用いて通信網を設
置する状態を示すもので、飛しょう体は、光ファイバ2
aを繰り出しながら目的地に向けて飛行していく。この
過程において、飛しよう体は、テレビカメラ3により地
上の画像を捕らえ、画像信号を発生する。この画像信号
は、光電変換装置6により光信号に変換され、発射地点
の光電変換装置7に送られる。光電変換装置7は、受信
した光信号を電気信号に変換し、この信号を表示装置1
0に送る。操縦者は、この表示装置10の画像を観察し
ながら飛しょう体操縦装置9により飛しょう体の遠隔操
縦を行ない、飛しょう体が目的地に到達したとき、遠隔
操作によりパラシュート4を開き飛しょう体を目的地に
軟着陸させる。Figure 2 shows how a communication network is installed using the flying object shown in Figure 1.
Fly towards the destination while releasing a. During this process, the flying object captures an image of the ground with the television camera 3 and generates an image signal. This image signal is converted into an optical signal by the photoelectric conversion device 6 and sent to the photoelectric conversion device 7 at the emission point. The photoelectric conversion device 7 converts the received optical signal into an electrical signal and transmits this signal to the display device 1.
Send to 0. The pilot remotely controls the flying object using the flying object control device 9 while observing the image on the display device 10, and when the flying object reaches the destination, he opens the parachute 4 by remote control and lets the flying object fly away. Make a soft landing with your body at your destination.
次いで、第3図に示すように、飛しょう体に搭載した送
受信装置13を飛しょう体の本体から降ろし、電源14
に接続するとともに飛しょう体の接続端子12に接続す
る。このようにして、飛しょう体の発射地点と目的地と
の間に通信網が設定される。Next, as shown in FIG.
It is connected to the connecting terminal 12 of the flying object. In this way, a communication network is established between the launch point and the destination of the projectile.
(効 果)
以上述べたように、本発明においては、通信伝達用の線
を巻いたリールを飛しょう体に搭載し、この通信伝達用
の線を繰り出しながら飛しょう体を目的地に向けて飛行
させ、目的地において飛しょう体を軟着陸装置により軟
着陸゛させるので、緊急時に迅速に大容量の通信網を設
置することが可能になる。とくに、通信伝達用の線とし
て光ファイバを使用すると、軽量で通信伝達容量が大き
いため、飛しょう体により長距離の通信網も設置するこ
とができるようになる。(Effects) As described above, in the present invention, a reel wound with a wire for communication transmission is mounted on a flying object, and the flying object is directed toward a destination while reeling out the wire for communication transmission. By flying the aircraft and making a soft landing at the destination using the soft landing gear, it becomes possible to quickly set up a large-capacity communication network in the event of an emergency. In particular, when optical fibers are used as communication lines, they are lightweight and have a large communication capacity, making it possible to install long-distance communication networks using flying objects.
第1図は、本発明の方法に使用される飛しょう体及び地
上設備の一例を示す概略図、第2図は、本発明による通
信網設置方法の一例を示す概略図、第3図は、通信網設
置状°態を示す概略図である。
l・・・・飛しょう鉢本体、
2・・・・リール、
2a・・・・光ファイバ、
4・・・・パラシュート、
8.13・・・・送受信装置、
11.14・・・・電源。FIG. 1 is a schematic diagram showing an example of a flying object and ground equipment used in the method of the present invention, FIG. 2 is a schematic diagram showing an example of the communication network installation method according to the present invention, and FIG. FIG. 2 is a schematic diagram showing a communication network installation state. l...Blow pot body, 2...Reel, 2a...Optical fiber, 4...Parachute, 8.13...Transmitting/receiving device, 11.14...Power source .
Claims (6)
と、軟着陸補助手段と、遠隔操縦手段とを有する飛しょ
う体を、前記通信伝達用の線を地上に繰り出しながら目
的地に向けて飛行させ、前記遠隔操縦装置により前記目
的地に到達したとき前記軟着陸装置を作動させて前記飛
しょう体を目的地に着陸させ、前記通信伝達用の線を飛
しょう体発射地点と前記目的地の送受信設備とに接続す
ることからなる、緊急用大容量通信網の構築方法。(1) Direct a flying object having a reel wound with a wire for communication transmission, a target detection means, a soft landing aid means, and a remote control means toward a destination while letting out the wire for communication transmission above the ground. When the object reaches the destination using the remote control device, the soft landing system is activated to land the object at the destination, and the communication line is connected between the object's launch point and the destination. A method for constructing an emergency large-capacity communication network, which consists of connecting to transmitting and receiving equipment.
通信伝達用の線は、光ファイバである、緊急用大容量通
信網の構築方法。(2) The method according to claim (1), wherein the communication transmission line is an optical fiber.
において、前記通信伝達用の線は、一端が飛しょう体発
射地点の送受信設備に接続され、他端が飛しょう体に設
けた接続端子に接続された緊急用大容量通信網の構築方
法。(3) In the method according to claim (1) or (2), one end of the communication transmission line is connected to a transmitting/receiving facility at a projectile launching point, and the other end is connected to a projectile launch point. A method for constructing an emergency high-capacity communication network connected to connection terminals provided in
法のいずれかにおいて、前記軟着陸手段はパラシュート
である緊急用大容量通信網の構築方法。(4) A method for constructing an emergency large-capacity communication network according to any one of claims (1) to (3), wherein the soft landing means is a parachute.
法のいずれかにおいて、前記遠隔操縦装置は、飛しょう
体に搭載したテレビカメラを含む緊急用大容量通信網の
構築方法。(5) A method for constructing an emergency large-capacity communication network in any of the methods set forth in claims (1) to (4), wherein the remote control device includes a television camera mounted on a flying object. .
法のいずれかにおいて、前記通信伝達用の線は、一端が
飛しょう体発射地点の地上送受信設備に接続され、前記
通信伝達用の線を通じて伝達される信号により遠隔操縦
されることを特徴とする緊急用大容量通信網の構築方法
。(6) In any of the methods set forth in claims (1) to (5), one end of the communication transmission line is connected to ground transceiver equipment at a projectile launch site, and the communication A method for constructing an emergency large-capacity communication network, characterized in that it is remotely controlled by signals transmitted through a transmission line.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP75487A JPH0736658B2 (en) | 1987-01-06 | 1987-01-06 | How to construct an emergency large capacity communication network |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP75487A JPH0736658B2 (en) | 1987-01-06 | 1987-01-06 | How to construct an emergency large capacity communication network |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS63169200A true JPS63169200A (en) | 1988-07-13 |
JPH0736658B2 JPH0736658B2 (en) | 1995-04-19 |
Family
ID=11482485
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP75487A Expired - Lifetime JPH0736658B2 (en) | 1987-01-06 | 1987-01-06 | How to construct an emergency large capacity communication network |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH0736658B2 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0447080A1 (en) * | 1990-03-10 | 1991-09-18 | United Kingdom Atomic Energy Authority | Reconnaissance device |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS4833838A (en) * | 1971-09-02 | 1973-05-14 | ||
JPS4915989A (en) * | 1972-06-07 | 1974-02-12 | ||
JPS54126997A (en) * | 1978-03-24 | 1979-10-02 | Taisei Corp | Cross drawing apparatus for and method of ropeeshaped body |
JPS5647005A (en) * | 1979-09-26 | 1981-04-28 | Sumitomo Electric Ind Ltd | Laying method of optical cable |
-
1987
- 1987-01-06 JP JP75487A patent/JPH0736658B2/en not_active Expired - Lifetime
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS4833838A (en) * | 1971-09-02 | 1973-05-14 | ||
JPS4915989A (en) * | 1972-06-07 | 1974-02-12 | ||
JPS54126997A (en) * | 1978-03-24 | 1979-10-02 | Taisei Corp | Cross drawing apparatus for and method of ropeeshaped body |
JPS5647005A (en) * | 1979-09-26 | 1981-04-28 | Sumitomo Electric Ind Ltd | Laying method of optical cable |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0447080A1 (en) * | 1990-03-10 | 1991-09-18 | United Kingdom Atomic Energy Authority | Reconnaissance device |
Also Published As
Publication number | Publication date |
---|---|
JPH0736658B2 (en) | 1995-04-19 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US11884175B2 (en) | Self-powered drone tether | |
CN104503349A (en) | Monitoring device based on unmanned aerial vehicle | |
CN109450515A (en) | A kind of large and medium-sized UAV Communication relay system | |
CN205336281U (en) | Aerial relay , data link system and emergent monitoring system | |
US4236234A (en) | Radio frequency seismic gathering system employing an airborne blimp | |
EP0393237A2 (en) | Communication link between moving bodies | |
WO2019058116A1 (en) | System and method for controlling a pilotless device | |
US9102405B2 (en) | Cable-tethered helicopter surveillance system | |
KR102149858B1 (en) | Transport drOne system equipped with wired relay drone and its operatiOn method | |
CN111114725B (en) | Autonomous underwater vehicle based on optical fiber communication buoy | |
US10651881B2 (en) | Launchable communications device for a distributed communication system | |
WO2019204997A1 (en) | Autonomous mobile platform, control end and autonomous mobile platform system | |
US20180273171A1 (en) | Aircraft, radio network, and method for transmitting information | |
KR102209503B1 (en) | Wireless communication system of Intelligent UAV | |
JPS63169200A (en) | Constructing method for large capacity communication network for emergency use | |
CN110769364B (en) | Unmanned aerial vehicle flight data and image transmission system | |
US6427944B1 (en) | Systems and methods for using airborne communication nodes | |
CN109405650A (en) | A kind of unmanned plane integrated combat system based on Man-in-loop control | |
JPH10285099A (en) | Unmanned aircraft system | |
JP5412379B2 (en) | Projection type projectile | |
CN114614880A (en) | Long-distance unmanned aerial vehicle signal relay system of low time delay | |
CN206524902U (en) | Radio transmission apparatus for the aerial dirigible system of line walking | |
KR101130625B1 (en) | A observation system using pilotless mooring blimp by a fiber-optic high intensity cable | |
KR102219954B1 (en) | Drone integrated control server and integrated control system including the same | |
CN109327873B (en) | Equipment switching method and device and data transmission system |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
EXPY | Cancellation because of completion of term | ||
S533 | Written request for registration of change of name |
Free format text: JAPANESE INTERMEDIATE CODE: R313533 |
|
R350 | Written notification of registration of transfer |
Free format text: JAPANESE INTERMEDIATE CODE: R350 |