JPS6489723A - Artifitial sattelite telemetry monitor equipment - Google Patents

Artifitial sattelite telemetry monitor equipment

Info

Publication number
JPS6489723A
JPS6489723A JP62246150A JP24615087A JPS6489723A JP S6489723 A JPS6489723 A JP S6489723A JP 62246150 A JP62246150 A JP 62246150A JP 24615087 A JP24615087 A JP 24615087A JP S6489723 A JPS6489723 A JP S6489723A
Authority
JP
Japan
Prior art keywords
supposing
value
telemetry
artifitial
sattelite
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
JP62246150A
Other languages
Japanese (ja)
Inventor
Masaru Oka
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.)
Toshiba Corp
Original Assignee
Toshiba 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 Toshiba Corp filed Critical Toshiba Corp
Priority to JP62246150A priority Critical patent/JPS6489723A/en
Publication of JPS6489723A publication Critical patent/JPS6489723A/en
Pending legal-status Critical Current

Links

Abstract

PURPOSE:To beforehand suppose an abnormality generation and to generate an alarm signal by supposing a telemetry value after a prescribed time with a supposing means and comparing it with the threshold set beforehand. CONSTITUTION:A telemetry value Da sent from a decoder is inputted to a feedback loop composed of a first computing element 8, a first adding register, a second adding register 10 and a multiplier 11. The output of the second adding register 10, after it is made (n)-fold by a multiplier 12, is inputted to a second computing element 13 together with the output of the first adding register 9. Thus, a telemetry supposing value Da' after (n) seconds is obtained. When the forerunning of an abnormality appears at the mounting device of the artifitial sattelite, the change rate become larger and the supposing value Da' after (n) seconds rises. For this reason, a threshold Dref is set so that the forerunning of the abnormality generation can be detected, the supposing value Da' is always compared and when the supposing value Da' exceeds the threshold Dref, an alarm signal is generated.
JP62246150A 1987-09-30 1987-09-30 Artifitial sattelite telemetry monitor equipment Pending JPS6489723A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP62246150A JPS6489723A (en) 1987-09-30 1987-09-30 Artifitial sattelite telemetry monitor equipment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP62246150A JPS6489723A (en) 1987-09-30 1987-09-30 Artifitial sattelite telemetry monitor equipment

Publications (1)

Publication Number Publication Date
JPS6489723A true JPS6489723A (en) 1989-04-04

Family

ID=17144231

Family Applications (1)

Application Number Title Priority Date Filing Date
JP62246150A Pending JPS6489723A (en) 1987-09-30 1987-09-30 Artifitial sattelite telemetry monitor equipment

Country Status (1)

Country Link
JP (1) JPS6489723A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH04321398A (en) * 1991-04-20 1992-11-11 Nec Corp Remote data measurement processing system
US7916452B2 (en) 2004-11-25 2011-03-29 Panasonic Corporation Method of producing a coin-type electrochemical element
RU181964U1 (en) * 2017-07-05 2018-07-30 Акционерное общество "Российская корпорация ракетно-космического приборостроения и информационных систем" (АО "Российские космические системы") Decoder for command-software and telemetry information of on-board equipment of command-measuring system

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH04321398A (en) * 1991-04-20 1992-11-11 Nec Corp Remote data measurement processing system
US7916452B2 (en) 2004-11-25 2011-03-29 Panasonic Corporation Method of producing a coin-type electrochemical element
US8248758B2 (en) 2004-11-25 2012-08-21 Panasonic Corporation Coin-type electrochemical element
RU181964U1 (en) * 2017-07-05 2018-07-30 Акционерное общество "Российская корпорация ракетно-космического приборостроения и информационных систем" (АО "Российские космические системы") Decoder for command-software and telemetry information of on-board equipment of command-measuring system

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