JPS58101900A - Working control system - Google Patents
Working control systemInfo
- Publication number
- JPS58101900A JPS58101900A JP19979181A JP19979181A JPS58101900A JP S58101900 A JPS58101900 A JP S58101900A JP 19979181 A JP19979181 A JP 19979181A JP 19979181 A JP19979181 A JP 19979181A JP S58101900 A JPS58101900 A JP S58101900A
- Authority
- JP
- Japan
- Prior art keywords
- control
- equipment
- satellite
- unit
- control system
- 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
Abstract
(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.
Description
【発明の詳細な説明】
本発明は各株の人工衛星に対してその衛星追跡管制設備
を自動運用管制した運用管制方式に関するものである。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an operation and control system that automatically controls satellite tracking and control equipment for each type of artificial satellite.
一般に1人工衛星の運用管制のために衛星追跡管制設備
が用いられている。この追跡管制設備は、人工衛星の運
用作業項目、運用時間、その各種運用モードなどが衛星
ごとに異るため、衛星単位で運用管制を行う必要がある
。このため従来は対象とする衛星が追加になるたびに、
その衛星に対する運用管制プログラムを追加するととも
に運用管制設備内の外部記憶装置を追加しなければなら
ないという欠点があった。Satellite tracking and control equipment is generally used to control the operation of a single artificial satellite. This tracking and control equipment must perform operation and control on a satellite-by-satellite basis because the operational work items, operation hours, and various operation modes of the satellites differ from satellite to satellite. For this reason, conventionally, each time a target satellite was added,
This method has the disadvantage that it is necessary to add an operation control program for the satellite as well as an external storage device within the operation and control facility.
本発明の目的は、各人工衛星に対して設定パラメータを
入力するだけで容易に運用できるようにして、運用管制
作業の省力化、正確化、迅速化を図った人工衛星の運用
管制方式を提供することKある。The purpose of the present invention is to provide an operation and control system for artificial satellites that can be easily operated by simply inputting setting parameters for each satellite, thereby saving labor, making the operation and control work more accurate, and speeding it up. There's K things to do.
本発明の運用管制方式は%複数の人工衛星の運用を制御
する管制率に運用対象となる人工衛星石。The operation control method of the present invention controls the operation of multiple artificial satellites at a control rate of %.
その運用作業項目、その運用時間を含む設定信号を入力
して連用スケジ、−ル部へ連絡し、この連絡を受けた前
記運用スケジ、−ル部は、複数の設備単位の運用制御部
のうち必要な個所を選択して運用スケジ、−ルを定め、
予め定められたパラメータと前記管制率の指令とに従っ
て前記選択された運用側@部が管制制御されることを特
徴とする。The setting signal including the operation work item and the operation time is inputted and communicated to the continuous scheduler section, and the operation scheduler section that receives this notification is one of the operation control sections of the plurality of equipment units. Select the necessary locations and determine the operation schedule and rules.
The selected operational side @ section is controlled according to predetermined parameters and the command of the control rate.
本発明によれば、煩雑な衛星連用作業を操作者に代わっ
て自動的に行えること、衛星運用に係る全設備の自動制
御や運用履歴の取得が行えること、運用対象の衛轟が追
加されてもその衛星の運用に必嶽な設備の組み合わせが
容易にできることなどの効果がある。According to the present invention, complicated satellite operation work can be automatically performed in place of the operator, all equipment related to satellite operation can be automatically controlled and operation history can be acquired, and satellites to be operated can be added. This also has the advantage of making it easier to combine the equipment necessary for the operation of the satellite.
以下図面により本発明の詳細な説明する。The present invention will be explained in detail below with reference to the drawings.
第1図は本発明の実施例のプp、り図であって、IFi
運用管制卓、2は運用計画入力部、3は運用監視制御部
、4は運用スケジューリング部、 5/fiパラメ一タ
設定部、6はn個の設備単位運用制御部、7は入出力制
御部、8は運用状態モニタ部、lOは運用管制設備、1
lFi局内各被運用設備である。FIG. 1 is a diagram of an embodiment of the present invention, in which IFi
Operation control console, 2 is an operation plan input unit, 3 is an operation monitoring control unit, 4 is an operation scheduling unit, 5/fi parameter setting unit, 6 is an operation control unit for n equipment units, 7 is an input/output control unit , 8 is an operation status monitor unit, IO is an operation control facility, 1
Each of the operating equipment within the IFi station.
この実施例の動作は次のとおりである。まず、運用管制
設備10中の運用管制率1の運用計画入力部2から運用
対象と六る人工衛星名、運用作業項目、運用時間、各種
違用モードを入力し、運用スケジューリング部4へ通知
する。この通知を受けた運用スケジューリング部4は、
その衛星運用に必景表設備をn個の設備単位運用制御部
6から選び出し、運用スケジュールを決定し、時刻をキ
ーにして運用管制制御を行う。各被運用設備11の制御
は、あらかじめパラメータ設定部5で定義づけられたパ
ラメータ値を使って、各被運用設備11に対応した設備
単位運用制御部6内モジ、−ルにより、入出力制御部7
を介して行われる。各被運用設備11の運用状態の監視
は、状態データが入出力制御部7を介して運用状態モニ
タ部8へ送られその状−を監視されるとともに運用管制
率1の運用監視制御部3へ出力される。このようにして
衛星運用に使用される全設備の制御および運用状態監視
を自動的に実行する。The operation of this embodiment is as follows. First, input the name of the artificial satellite to be operated, operation work items, operation time, and various misuse modes from the operation plan input unit 2 of the operation control rate 1 in the operation control facility 10, and notify the operation scheduling unit 4. . The operation scheduling unit 4 that received this notification,
A must-see equipment for the satellite operation is selected from n equipment unit operation control units 6, an operation schedule is determined, and operation control is performed using time as a key. The control of each operated equipment 11 is performed by the input/output control unit using the parameter values defined in advance by the parameter setting unit 5 and by the modules in the equipment unit operation control unit 6 corresponding to each operated equipment 11. 7
It is done through. Monitoring of the operational status of each operated equipment 11 is carried out by sending status data to the operational status monitoring unit 8 via the input/output control unit 7, where the status is monitored, and then sent to the operational monitoring and control unit 3 with an operational control rate of 1. Output. In this way, control and operation status monitoring of all equipment used for satellite operations are automatically executed.
したがって、この運用管制方式によれは、各人工衛星に
応じて、使用する設備を設備単位で自白に組み合わせて
スケジューリングできること、各設備の設定パラメータ
値も自由に衛JiK応じて変更できることを利用し、運
用管制すべき衛星が追加爆れても短期間で安価に対応す
ることができる。Therefore, this operation control method takes advantage of the fact that it is possible to schedule the equipment to be used in combination on an equipment-by-equipment basis according to each satellite, and that the setting parameter values of each equipment can also be freely changed according to the satellite. Even if additional satellites to be operated and controlled are detonated, it can be dealt with in a short period of time and at low cost.
また、運用対象となる全設備にわたり、運用管制するこ
とKより衛星運用の省力化、正確化、迅速化が図られる
。In addition, by controlling all the equipment to be operated, labor-saving, accurate, and speedy satellite operations can be achieved.
°以上説明したように、設備単位運用制御部内の各制御
モジ、−ルの組合せおよびノくラメータ設定部の設電パ
ラメータの指定により、極々の衛星に対しての運用管制
が可能であり、運用対象となる全設備にわたりて制御お
よび監視が対象とでき運用の省力化、迅速化、正確化が
図られる利点がある。°As explained above, by combining each control module and module in the facility unit operation control unit and specifying the power installation parameters in the parameter setting unit, it is possible to control the operation of extremely large satellites. It has the advantage of being able to control and monitor all target equipment, resulting in labor-saving, speedy, and accurate operations.
第1図は本発明の実施例の系統図である。 FIG. 1 is a system diagram of an embodiment of the present invention.
Claims (1)
る人工衛18.その運用作業項目、その運用時間を含む
設定信号を入力して運用スクジ。 −ル部へ連絡し、この連絡を受けた前記スヶジ。 −ル部は複数の設備単位の運用制御部のうち必要な個所
を選択して運用スケジ、&−ルを定め、予め定められた
パラメータと前記管制率の指令とに従って前記選択され
九運用制御部が管制制御されることを特徴とする運用管
制方式。[Scope of Claims] Artificial satellites 18. Input the setting signal including the operation work item and the operation time to complete the operation. - Said Sugaji contacted the Ru Department and received this message. - The control section selects the necessary locations from among the operation control sections of a plurality of equipment units, determines the operation schedule, and the control section, and selects the nine operation control sections selected according to the predetermined parameters and the command of the control rate. An operation control method characterized by the fact that the system is controlled.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP19979181A JPS58101900A (en) | 1981-12-11 | 1981-12-11 | Working control system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP19979181A JPS58101900A (en) | 1981-12-11 | 1981-12-11 | Working control system |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS58101900A true JPS58101900A (en) | 1983-06-17 |
Family
ID=16413668
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP19979181A Pending JPS58101900A (en) | 1981-12-11 | 1981-12-11 | Working control system |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS58101900A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2010208599A (en) * | 2009-03-12 | 2010-09-24 | Fujitsu Ltd | Path allocation program, path allocation device, and path allocation method |
-
1981
- 1981-12-11 JP JP19979181A patent/JPS58101900A/en active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2010208599A (en) * | 2009-03-12 | 2010-09-24 | Fujitsu Ltd | Path allocation program, path allocation device, and path allocation method |
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