JPS6041818A - Timer device mounted on satellite - Google Patents

Timer device mounted on satellite

Info

Publication number
JPS6041818A
JPS6041818A JP14979283A JP14979283A JPS6041818A JP S6041818 A JPS6041818 A JP S6041818A JP 14979283 A JP14979283 A JP 14979283A JP 14979283 A JP14979283 A JP 14979283A JP S6041818 A JPS6041818 A JP S6041818A
Authority
JP
Japan
Prior art keywords
output
section
majority decision
gate circuit
clock signal
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
JP14979283A
Other languages
Japanese (ja)
Inventor
Toshio Seki
関 俊雄
Takeshi Kikuchi
毅 菊地
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.)
Panasonic Holdings Corp
Original Assignee
Matsushita Electric Industrial Co 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 Matsushita Electric Industrial Co Ltd filed Critical Matsushita Electric Industrial Co Ltd
Priority to JP14979283A priority Critical patent/JPS6041818A/en
Publication of JPS6041818A publication Critical patent/JPS6041818A/en
Pending legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H03ELECTRONIC CIRCUITRY
    • H03KPULSE TECHNIQUE
    • H03K17/00Electronic switching or gating, i.e. not by contact-making and –breaking
    • H03K17/28Modifications for introducing a time delay before switching

Landscapes

  • Electronic Switches (AREA)

Abstract

PURPOSE:To improve the reliability by constituting triply a clock signal generating section, a counter section and a program section to obtain an output from a majority decision gate circuit. CONSTITUTION:When a signal for two systems' share from clock signal generating sections 1a-1c formed as a triple system is outputted respectively via majority decision circuits 7a-7c, the majority decision is applied by the 2nd majority decision gate circuit 7d via counter sections 2a-2c and program sections 3a-3c, and a control signal is outputted to a load side by a decode section 8 and an output section 4. The control signal is outputted normally even if one optional system of the input is missing, and no output is given out of the majority decision gate circuit even if any of the systems mulfunctions as runaway or the like, then the high reliability is attained.

Description

【発明の詳細な説明】 産業上の利用分野 本発明は衛星に搭載され、あらかじめプログラムされた
時刻に衛星の点火、切断を行うために使用する衛星搭載
用タイマ装置に関するものである。
DETAILED DESCRIPTION OF THE INVENTION Field of the Invention The present invention relates to a timer device mounted on a satellite and used to ignite and disconnect the satellite at preprogrammed times.

従来例の構成とその問題点 従来の衛星に搭載されるタイマ装置としては、第1図に
示すシングル方式或いは第2図に示すデュアル方式のも
のがあった。
Conventional configurations and their problems Conventional timer devices mounted on satellites include a single type timer device as shown in FIG. 1 or a dual type timer device as shown in FIG. 2.

第1図のシングル方式のタイマ装置では、クロック信号
発生部1の出力をカウンタ部2で開数し、カウント値が
あらかじめプログラム部3で定めた値に達すると出力部
4を介して制御信号を出力し、この制御信号によシ衛星
搭載ロケットの点火或いは切断の制御を行う、ようにな
っていた。まだ第2図のデュアル方式のものでは、クロ
ック信号の発生をクロック信号発生部1a及び1bの2
組設け、捷だ前記クロック信号出力の片方が停止すると
他方に切替えるクロック信号切替回路5を設けて信頼性
の向上を図っている。
In the single type timer device shown in FIG. 1, the output of the clock signal generator 1 is multiplied by the counter unit 2, and when the count value reaches a value predetermined by the program unit 3, a control signal is outputted via the output unit 4. This control signal was used to control the ignition or disconnection of the rocket carrying the satellite. In the dual system shown in FIG. 2, the clock signal is generated by two clock signal generators 1a and 1b.
In order to improve reliability, a clock signal switching circuit 5 is provided which switches to the other one of the clock signal outputs when one of the clock signal outputs stops.

しかしながら、第1図のシングル方式のタイマ装置では
、クロック信号発生部1の発振停止或いは発振周波数ず
れが起きたり、カウンタ部2.プログラム部3.出力部
4のいずれかの不動作や誤動作によシ出力誤差を生じ、
衛星の失販の原因となる問題点があった。また第2図の
デュアル方式のものでも、クロック切替回路6以降の段
がシングル方式であるため十分な信頼性が得られなかっ
た。
However, in the single type timer device shown in FIG. 1, the oscillation of the clock signal generating section 1 may stop or the oscillation frequency may shift, and the counter section 2. Program section 3. Output errors may occur due to non-operation or malfunction of any of the output units 4,
There were problems that caused the satellite to lose sales. Further, even in the dual system shown in FIG. 2, sufficient reliability could not be obtained because the stages after the clock switching circuit 6 were of the single system.

発明の目的 本発明は上記従来例の欠点を除去し、信頼度の高い衛星
搭載タイマ装置を提供することを目的とする。
OBJECTS OF THE INVENTION It is an object of the present invention to eliminate the drawbacks of the above-mentioned conventional examples and to provide a highly reliable satellite-mounted timer device.

発明の構成 本発明は上記目的を達成するために、前記タイマ装置の
中でクリティカルなブロックであるクロック信号発生部
とカウンタ部とプログラム部とをトリプル構成とし、さ
らに多数決ゲート回路により3系統の信号のうち2系統
以上のみ入力がある時に出力するように構成して、高い
信頼性を得るようにしたものである。
Structure of the Invention In order to achieve the above object, the present invention has a triple configuration of the clock signal generation section, the counter section, and the program section, which are critical blocks in the timer device, and furthermore, a majority gate circuit is used to generate three systems of signals. High reliability is achieved by configuring the system to output when only two or more systems are input.

実施例の説明 以下に本発明の一実施例を図面と共に説明する。Description of examples An embodiment of the present invention will be described below with reference to the drawings.

第3図において、1a〜1cはクロック信号発生部、7
a〜7cは第1の多数決ゲート回路、2a〜2Cはカウ
ンタ部、3a〜3Cはプログラム部で、これらはいずれ
も3組から成りトリプル系になっている。7dは第2の
多数決ゲート回路、8はデコード部、4は出力部である
In FIG. 3, 1a to 1c are clock signal generators, 7
Reference numerals a to 7c are first majority gate circuits, 2a to 2C are counter sections, and 3a to 3C are program sections, all of which are comprised of three sets, forming a triple system. 7d is a second majority gate circuit, 8 is a decoding section, and 4 is an output section.

次に動作を説明する。クロック信号発生部1a〜1Cで
それぞれIHzの信号を出力し、第1の多数決回路7a
〜7Cにそれぞれ3系統の入力を並列入力する。各第1
の多数決回路78〜7Cでは、前記3系統の入力のうち
2系統が存在すれば出力するようになっている。金策1
の多数決ゲート回路7a〜7Cの入力信号をA、B、C
とし、また出力信号をFl 〜F3で表わすと、Fl 
=A・B+A−C+B会C・・・・ ・・・ (1)F
2=A−B+A@C+B拳C・・・・・・・・ (2)
F3=A@B+A−C+B−C・・・・・・・・ (3
)のように(1)〜(3)式で表わされるから、仮にA
の入力が無くても、Fl 〜F3は正常に出力される。
Next, the operation will be explained. Each of the clock signal generators 1a to 1C outputs an IHz signal, and the first majority circuit 7a outputs an IHz signal.
Input three input systems in parallel to each of ~7C. each first
The majority circuits 78 to 7C are configured to output if two of the three input systems exist. Money plan 1
The input signals of the majority gate circuits 7a to 7C are A, B, and C.
And if the output signal is represented by Fl ~ F3, then Fl
=A・B+A−C+B meeting C・・・・・ (1)F
2=A-B+A@C+B fist C... (2)
F3=A@B+A-C+B-C・・・・・・・・・(3
) is expressed by equations (1) to (3), so if A
Even if there is no input, Fl to F3 are output normally.

一方、Aが暴走し、B、C入力に対し早い時間に入力さ
れると、Fl 〜F3は出力されなくなる。
On the other hand, if A goes out of control and is input earlier than inputs B and C, Fl to F3 will no longer be output.

前記第1の多数決回路7a〜7Cの出力はそれぞれ、カ
ウンタ部28〜2c、 プログラム部3a〜3Cを介し
て第2の多数決ゲート回路7dに入力される。プログラ
ム部3a〜3cは、タイマ出力 l信号の前記秒時設定
信号を例えばプログラマブル−リードオンリーメモリ(
P−ROM)にょシ記憶する場所で、前記カウンタ部2
a〜2cの出力信号を前記P−ROMのアドレスに入力
し、その出力を前記第2の多数決ゲート回路7dに入力
することにより、入力のうち任意の一系統を欠いても出
力されタイマ装置の動作に影響を及はさないように作動
する。また、何れかの一系統が暴走等により誤動作出力
しても第2の多数決ゲート回路了dは出力しない。なお
、第2の多数決ゲート回路7dの出力はデコード部8で
デコードして出力部4より負荷側に制御信号として約1
秒間出力し、点火、切断等の制御を行う。
The outputs of the first majority circuits 7a to 7C are input to the second majority gate circuit 7d via counter sections 28 to 2c and program sections 3a to 3C, respectively. The program units 3a to 3c convert the second time setting signal of the timer output l signal into a programmable read-only memory (
P-ROM) where the counter section 2 is stored.
By inputting the output signals of a to 2c to the addresses of the P-ROM and inputting their outputs to the second majority gate circuit 7d, even if any one of the inputs is missing, the output signals can be outputted to the timer device. It operates in such a way that it does not affect the operation. Further, even if one of the systems outputs a malfunction due to runaway or the like, the second majority gate circuit d does not output. The output of the second majority gate circuit 7d is decoded by the decoding section 8 and sent as a control signal from the output section 4 to the load side.
Outputs for seconds and controls ignition, cutting, etc.

発明の詳細 な説明したように、本発明によれば信頼性の要求される
個所をトリプル構成にし、しかも多数決判定により出力
を決定しているので、クロック信号の停止或いは暴走、
さらに各段の誤動作に対し高い信頼性が確保出来る利点
を有する。
As described in detail, according to the present invention, the parts where reliability is required are configured in a triple configuration, and the output is determined by majority decision, so that there is no possibility of the clock signal stopping or running out of control.
Furthermore, it has the advantage of ensuring high reliability against malfunctions at each stage.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図および第2図は従来の衛星搭載タイマ装置の構成
を示すブロック図、第3図は本発明の一実施例における
衛星搭載タイマ装置の構成を示すブロック図である。 1a〜1C・・・・・・クロック信号発生部、2a〜2
C・・・・・・カウンタ部、3a〜3C・・・・・・プ
ログラム部、4・・・・・・出力部、7a〜7d・・・
・・・多数決ゲート回路、8・・・・・・デコード部。
1 and 2 are block diagrams showing the structure of a conventional satellite-mounted timer device, and FIG. 3 is a block diagram showing the structure of a satellite-mounted timer device according to an embodiment of the present invention. 1a to 1C...Clock signal generation section, 2a to 2
C...Counter section, 3a-3C...Program section, 4...Output section, 7a-7d...
. . . Majority gate circuit, 8 . . . Decoding section.

Claims (1)

【特許請求の範囲】[Claims] 複数個のクロック信号発生部と、前記複数個のクロック
信号発生部の出力がいずれも入力される複数組の第1の
多数決ゲート回路と、前記第1の多数決ゲート回路の出
力をそれぞれ計時用のカウンタ部を介して入力し、あら
かじめ設定された秒時設定値を越えると信号を出力する
複数組のプログラム部と、前記複数組のプログラム部の
出力が入力される第2の多数決ゲート回路とを備え、前
記第2の多数決ゲート回路の出力をデコードしてタイマ
制御信号を得るようにしてなる衛星搭載タイマ装置。
a plurality of clock signal generators, a plurality of sets of first majority gate circuits into which the outputs of the plurality of clock signal generators are input, and a clock circuit that receives the outputs of the first majority gate circuits, respectively. a plurality of program sections that receive input via a counter section and output a signal when a preset second setting value is exceeded; and a second majority gate circuit that receives the outputs of the plurality of program sections. A satellite-mounted timer device, comprising: decoding the output of the second majority gate circuit to obtain a timer control signal.
JP14979283A 1983-08-17 1983-08-17 Timer device mounted on satellite Pending JPS6041818A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP14979283A JPS6041818A (en) 1983-08-17 1983-08-17 Timer device mounted on satellite

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP14979283A JPS6041818A (en) 1983-08-17 1983-08-17 Timer device mounted on satellite

Publications (1)

Publication Number Publication Date
JPS6041818A true JPS6041818A (en) 1985-03-05

Family

ID=15482814

Family Applications (1)

Application Number Title Priority Date Filing Date
JP14979283A Pending JPS6041818A (en) 1983-08-17 1983-08-17 Timer device mounted on satellite

Country Status (1)

Country Link
JP (1) JPS6041818A (en)

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