JPH07220200A - Aircraft control transfer system for offshore airspace - Google Patents
Aircraft control transfer system for offshore airspaceInfo
- Publication number
- JPH07220200A JPH07220200A JP6009655A JP965594A JPH07220200A JP H07220200 A JPH07220200 A JP H07220200A JP 6009655 A JP6009655 A JP 6009655A JP 965594 A JP965594 A JP 965594A JP H07220200 A JPH07220200 A JP H07220200A
- Authority
- JP
- Japan
- Prior art keywords
- control
- aircraft
- position information
- navigation position
- navigation
- 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
Links
Landscapes
- Navigation (AREA)
- Traffic Control Systems (AREA)
Abstract
(57)【要約】
【目的】洋上空域を航行する航空機の航行位置情報をリ
アルタイムで取得し、航行位置把握の精度向上と、管制
移管業務の確実な実行を図る洋上空域の航空機管制移管
システムの提供。
【構成】航空機管制移管システム１００は、航法装置で
ある位置検出装置１１１と位置情報通報装置１１２を搭
載する航空機１１０と、航行位置情報を通信衛星１２０
を介して中継する衛星通信回線１１５，１２５と、通信
衛星地球局１３０から管制システム１４０，１５０に航
行位置情報を伝送する通信回線１３５，１３６とを含
む。計算機１４１，１５１で航行位置情報をそれぞれ可
視化処理し、ＣＲＴ画面１４２，１５２に航行位置情報
を可視化表示する管制システム１４０と、管制移管情報
を伝送する通信回線１４５と、計算機１５１で管制移管
情報を可視化処理し、ＣＲＴ画面１５２に可視化表示す
る。
(57) [Summary] [Purpose] An aircraft control and transfer system in the offshore airspace that acquires the navigation position information of the aircraft navigating in the air over the sea in real time to improve the accuracy of the navigation position and ensure the execution of control and control operations. Offer. [Structure] An aircraft control transfer system 100 includes an aircraft 110 equipped with a position detection device 111, which is a navigation device, and a position information reporting device 112, and a communication satellite 120 that transmits navigation position information.
Satellite communication lines 115 and 125 for relaying via the satellite and communication lines 135 and 136 for transmitting navigation position information from the communication satellite earth station 130 to the control systems 140 and 150. Computers 141 and 151 visualize navigation position information, respectively, and control system 140 that visualizes and displays navigation position information on CRT screens 142 and 152, communication line 145 that transmits control transfer information, and computer 151 displays control transfer information. It is visualized and displayed on the CRT screen 152.
Description
【０００１】[0001]
【産業上の利用分野】この発明は、洋上空域を航行する
航空機の管制移管に関し、特に通信衛星を介して航空機
の航行位置情報をリアルタイムで取得して前記航行位置
情報を可視化表示し、管制移管業務を実施する洋上空域
の航空機管制移管システムに関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to control transfer of an aircraft traveling in the oceanic airspace, and particularly to acquiring navigation position information of an aircraft in real time via a communication satellite to visualize and display the navigation position information and transfer control. The present invention relates to an aircraft control transfer system in the airspace over the sea where operations are performed.
【０００２】[0002]
【従来の技術】従来の洋上空域を航行する航空機は、パ
イロットが、航行空域を管轄する管制センターとＨＦ無
線通話回線を通じて交信することによって管制を受けて
いる。パイロットの航行位置通報を管制センターの管制
官が聞き取り、航行位置を把握し、パイロットに管制指
示を通報することによって、管制業務は実施されてい
る。この従来技術を説明する図３を参照すると、航空機
２１０には、航法装置である位置検出装置２１１と、パ
イロットが位置通報を行うＨＦ帯無線通話装置２１３
と、が搭載され、パイロットが通話するＨＦ帯無線通信
回線２１７によって更新する地上の管制センター２４０
および２５０には、通話を受信するＨＦ帯無線通話装置
２４３および２５３と、航行位置情報を入手し、可視化
処理する計算機２４１および２５１と、可視化処理され
た航行位置情報を可視化表示するＣＲＴ画面２４２およ
び２５２と、管制センター２４０および２５０を接続す
る電話回線２４７を有する。機上のパイロットは航法装
置のロランあるいはＩＮＳによって、航行位置を知り、
ＨＦ帯無線通話装置２１３によって、管制センター２４
０に位置通報を行う。位置通報は管制官によって計算機
２４１に入力されＣＲＴ画面２４２に可視化表示され
る。管制官はＣＲＴ画面に可視化表示されている航空機
の航行位置が、管轄する管制空域の境界を越え、隣接の
管制空域に入ることを隣接の管制センター２５０に電話
回線２４７を通じて通報し、該航空機の管制移管を行っ
ている。2. Description of the Related Art A conventional aircraft navigating over the sea is controlled by a pilot communicating with a control center in charge of the navigating airspace through an HF radio communication line. The control operation is carried out by the pilot of the control center listening to the pilot's navigation position notification, grasping the navigation position, and notifying the pilot of control instructions. Referring to FIG. 3 for explaining this conventional technique, the aircraft 210 has a position detecting device 211, which is a navigation device, and an HF band wireless communication device 213, in which a pilot makes a position notification.
And is installed, and the ground control center 240 is updated by the HF band wireless communication line 217 with which the pilot talks.
And 250, HF band wireless communication devices 243 and 253 for receiving a call, computers 241 and 251 for obtaining and visualizing navigation position information, and a CRT screen 242 for visualizing and displaying the visualized navigation position information. 252 and a telephone line 247 connecting the control centers 240 and 250. The pilot on board knows the navigation position by Loran or INS of the navigation system,
The control center 24 is controlled by the HF band wireless communication device 213.
Report position to 0. The position notification is input to the computer 241 by the controller and visualized and displayed on the CRT screen 242. The controller notifies the adjacent control center 250 via the telephone line 247 that the navigation position of the aircraft visually displayed on the CRT screen exceeds the boundary of the control airspace under its control and enters the adjacent control airspace. We are transferring control.
【０００３】[0003]
【発明が解決しようとする課題】上述した従来の洋上空
域における航行位置情報では、航空機の位置通報の時間
間隔が長く、管制官が航行位置をリアルタイムに把握で
きないため、航行位置把握の精度を確保することが難し
い。更に、ＨＦ帯無線通話の安定性と通話効率が低く、
管制移管業務に対する管制官の業務負荷を過重にしてい
る。したがって、航行位置把握の精度を確保し、かつ位
置通報のリアルタイムで安定した取得を図ることによっ
て、管制移管業務の信頼度の向上と、業務負荷を軽減を
図る。In the above-mentioned conventional navigation position information in the offshore airspace, since the time interval of aircraft position notification is long and the controller cannot grasp the navigation position in real time, the accuracy of the navigation position confirmation is ensured. Difficult to do. Furthermore, the stability and call efficiency of HF band wireless calls are low,
The work load of the controller on the control transfer work is overloaded. Therefore, by ensuring the accuracy of navigation position grasping and obtaining stable position notifications in real time, the reliability of control transfer work will be improved and the work load will be reduced.
【０００４】[0004]
【課題を解決するための手段】この発明の目的は、洋上
を航行する航空機の航行位置情報をリアルタイムで取得
し、航行位置把握の精度向上と、管制移管業務の確実な
実施を図ることにある。SUMMARY OF THE INVENTION An object of the present invention is to obtain navigation position information of an aircraft navigating in the sea in real time, improve the accuracy of navigation position confirmation, and reliably carry out control transfer work. .
【０００５】そのため、航空機の航行位置情報を取得
し、前記航行位置情報を可視化表示し、可視化表示され
た航行位置情報に基づいて、航空機の管制移管業務を実
施する航空機管制移管システムにおいて、洋上空域を航
行する航空機の航行位置情報をリアルタイムで取得する
手段と、航行位置情報を可視化表示し、リアルタイムで
取得する航行位置情報によって前記可視化表示を更新す
る手段と、航空機の航行位置情報をそれぞれに可視化表
示する第１の管制システムと第２の管制システムが前記
航空機の管制移管情報を交換する手段と、を備える。Therefore, in an aircraft control and transfer system that acquires navigation position information of an aircraft, visualizes and displays the navigation position information, and carries out control and control operations of the aircraft based on the visually displayed navigation position information, A means for acquiring the navigation position information of the aircraft traveling in real time, a means for visualizing and displaying the navigation position information, a means for updating the visualization display with the navigation position information acquired in real time, and a visualization of the navigation position information of the aircraft respectively. The first control system and the second control system for displaying have means for exchanging control transfer information of the aircraft.
【０００６】[0006]
【実施例】次に、この発明について図面を参照して説明
する。DESCRIPTION OF THE PREFERRED EMBODIMENTS Next, the present invention will be described with reference to the drawings.
【０００７】この発明の一実施例のシステム構成を示す
図１を参照すると、洋上空域の航空機管制移管システム
１００は、航行位置を検出する航法装置である位置検出
装置１１１と航行位置情報を通信衛星１２０に衛星通信
回線１１５を通じて伝送する位置情報通報装置１１２を
搭載する航空機１１０と、航行位置情報を通信衛星１２
０を介して中継する衛星通信回線１２５と、通信衛星地
球局１３０に航行位置情報を伝送する通信回線１３５
と、通信衛星地球局１３０から管制システム１４０およ
び１５０に航行位置情報を伝送する通信回線１３５およ
び１３６と、計算機１４１および１５１で航行位置情報
をそれぞれ可視化処理し、ＣＲＴ画面１４２および１５
２に航行位置情報をそれぞれ可視化表示する管制システ
ム１４０および１５０と、航行位置情報に基づく管制移
管情報を隣接する空域を管轄する管制センターの管制シ
ステム１５０に伝送する通信回線１４５と、管制移管情
報を可視化処理し、航行位置情報と管制移管情報をＣＲ
Ｔ画面１５２に可視化表示する管制システム１５０と、
を含む。Referring to FIG. 1, which shows the system configuration of an embodiment of the present invention, an aircraft control and transfer system 100 for offshore airspace includes a position detecting device 111 which is a navigation device for detecting a navigation position, and a navigation satellite for providing navigation position information. 120 and an aircraft 110 equipped with a position information reporting device 112 that transmits via satellite communication line 115, and communication satellite 12
Satellite communication line 125 for relaying via 0 and communication line 135 for transmitting navigation position information to the communication satellite earth station 130.
, Communication lines 135 and 136 for transmitting navigation position information from the communication satellite earth station 130 to the control systems 140 and 150, and visualization processing of navigation position information by computers 141 and 151, respectively, and CRT screens 142 and 15
2, control systems 140 and 150 for visualizing and displaying navigation position information, a communication line 145 for transmitting control transfer information based on the navigation position information to the control system 150 of the control center that controls the adjacent airspace, and control transfer information. Visualization processing and CR of navigation position information and control transfer information
A control system 150 that visualizes and displays on the T screen 152,
including.
【０００８】次に、移管対象の航空機の航行位置に対応
する管制移管業務の推移を説明する図２（ａ）乃至
（ｄ）を援用し、この実施例の動作を説明すと、先ず図
２（ａ）を参照すると、管制システム１４０，１５０の
ＣＲＴ画面１４２，１５２には、移管対象の航空機の航
行状況がそれぞれ可視化表示されている。該航空機を管
制しているとき、△のシンボルに、また管制対象でない
とき／のシボルに、該航空機の属性を表わすデータブロ
ックをそれぞれに付加し、ＣＲＴ画面１４２，１５２に
それぞれ可視化表示されている。Next, the operation of this embodiment will be described with reference to FIGS. 2 (a) to 2 (d) for explaining the transition of the control transfer work corresponding to the navigation position of the aircraft to be transferred. Referring to (a), the navigation status of the aircraft to be transferred is visualized and displayed on the CRT screens 142 and 152 of the control systems 140 and 150, respectively. When controlling the aircraft, a data block representing the attribute of the aircraft is added to the symbol of Δ, and to the symbol of / when it is not a control target, which are respectively visualized and displayed on the CRT screens 142 and 152. .
【０００９】次に、図２（ｂ）を参照すると、該航空機
が管制空域境界に近付き、該境界の直前に達したとき管
制移管が開始される。管制システム１４０から移管開始
の管制移管情報を管制システム１５０に送付すると、／
のシンボルに付されいるデータブロックに移管開始を示
すＨＮＤがそれぞれ可視化表示される。更に、該航空機
が境界を通過するとき、移管完了の管制移管情報を管制
システム１４０から管制イステム１５０に送付され、移
管完了を示すＯＶＲがそれぞれのデータブロックに可視
化表示され、一定時間経過後、ＯＶＲが消えて、該航空
機の管制移管業務を完了する。Next, referring to FIG. 2B, control transfer is started when the aircraft approaches the control airspace boundary and reaches just before the boundary. When the control transfer information of the transfer start from the control system 140 is sent to the control system 150,
HNDs indicating the start of transfer are visualized and displayed in the data blocks attached to the symbols. Further, when the aircraft crosses the boundary, the control transfer information indicating the transfer completion is sent from the control system 140 to the control system 150, and the OVR indicating the transfer completion is visualized and displayed in each data block. Disappears, and the control transfer work of the aircraft is completed.
【００１０】以上の説明からリアルタイムで航行位置情
報を取得することによって、管制移管を確実に実施でき
る管制移管システムが構築できる。From the above description, by acquiring the navigation position information in real time, it is possible to construct the control transfer system which can surely execute the control transfer.
【００１１】[0011]
【発明の効果】以上説明したように、この発明によれ
ば、通信衛星を介して、リアルタイムで航空機の航行位
置情報を取得することによって、航行位置把握の精度の
向上と、確実な管制移管が実施できる。As described above, according to the present invention, by obtaining the navigation position information of an aircraft in real time via the communication satellite, it is possible to improve the accuracy of navigation position confirmation and ensure the control transfer. Can be implemented.
【図１】この発明の一実施例を示すシステム構成を示す
図である。FIG. 1 is a diagram showing a system configuration showing an embodiment of the present invention.
【図２】子図（ａ），（ｂ），（ｃ），（ｄ）は、それ
ぞれ航空機の移管前の状況を示すＣＲＴ画面、移管中の
状況を示すＣＲＴ画面，移管完了の状況を示すＣＲＴ画
面、およびＣＲＴ画面に可視化表示されるデータブロッ
クおよびシンボルを、説明する図である。2A to 2C are child charts (a), (b), (c), and (d) respectively showing a CRT screen showing a situation before transfer of an aircraft, a CRT screen showing a situation during transfer, and a status of transfer completion. It is a figure explaining a CRT screen and a data block and a symbol visualized and displayed on a CRT screen.
【図３】従来技術を説明する図である。FIG. 3 is a diagram illustrating a conventional technique.
１００ 洋上空域の航空機管制移管システム １１０ 航空機 １１１ 位置検出装置 １１２ 位置通報装置 １１５ 衛星通信回線 １２０ 通信衛星 １２５ 衛星通信回線 １３０ 通信衛星地球局 １３５ 通信回線 １３６ 通信回線 １４０ 管制システム １４１ 計算機 １４２ ＣＲＴ画面 １５０ 管制システム １５１ 計算機 １５２ ＣＲＴ画面 100 Aircraft control transfer system in the ocean airspace 110 Aircraft 111 Position detection device 112 Position notification device 115 Satellite communication line 120 Communication satellite 125 Satellite communication line 130 Communication satellite earth station 135 Communication line 136 Communication line 140 Control system 141 Computer 142 CRT screen 150 Control System 151 Computer 152 CRT screen
Claims (1)
行位置情報を可視化表示し、可視化表示された航行位置
情報に基づいて、航空機の管制移管業務を実施する航空
機管制移管システムにおいて、 洋上空域を航行する航空機の航行位置情報をリアルタイ
ムで取得する手段と、 航行位置情報を可視化表示し、リアルタイムで取得する
航行位置情報によって前記可視化表示を更新する手段
と、 航空機の航行位置情報をそれぞれに可視化表示する第１
の管制システムと第２の管制システムが前記航空機の管
制移管情報を交換する手段と、 を備え、 前記第１の管制システムと第２の管制システムの間で、
前記洋上空域を航行する航空機の管制移管業務を実施す
ることを特徴とする洋上空域の航空機管制移管システ
ム。1. An aircraft control and transfer system that acquires navigation position information of an aircraft, visualizes and displays the navigation position information, and carries out control and control operations of the aircraft based on the visualized and displayed navigation position information. A means for acquiring the navigation position information of the aircraft that is navigating in real time, a method for visualizing and displaying the navigation position information and updating the visualization display with the navigation position information that is acquired in real time, and a visualization of the navigation position information of the aircraft. First to display
And a means for the second control system to exchange control transfer information of the aircraft, between the first control system and the second control system,
An aircraft control and transfer system for offshore airspace, which carries out control and control operations for aircraft flying in the above airspace.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP6009655A JPH07220200A (en) | 1994-01-31 | 1994-01-31 | Aircraft control transfer system for offshore airspace |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP6009655A JPH07220200A (en) | 1994-01-31 | 1994-01-31 | Aircraft control transfer system for offshore airspace |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH07220200A true JPH07220200A (en) | 1995-08-18 |
Family
ID=11726238
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP6009655A Pending JPH07220200A (en) | 1994-01-31 | 1994-01-31 | Aircraft control transfer system for offshore airspace |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH07220200A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1999037651A1 (en) * | 1998-01-21 | 1999-07-29 | Millenium Pharmaceuticals, Inc. | Chemokine receptor antagonists and methods of use therefor |
| JP2012068972A (en) * | 2010-09-24 | 2012-04-05 | Navicom Aviation Corp | Aircraft management system, ground device, ground control device, ground device program, ground control device program, and information processing method |
-
1994
- 1994-01-31 JP JP6009655A patent/JPH07220200A/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1999037651A1 (en) * | 1998-01-21 | 1999-07-29 | Millenium Pharmaceuticals, Inc. | Chemokine receptor antagonists and methods of use therefor |
| JP2012068972A (en) * | 2010-09-24 | 2012-04-05 | Navicom Aviation Corp | Aircraft management system, ground device, ground control device, ground device program, ground control device program, and information processing method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| A02 | Decision of refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A02 Effective date: 20000208 |