JPH0325599A - Flying data collector - Google Patents

Flying data collector

Info

Publication number
JPH0325599A
JPH0325599A JP15826789A JP15826789A JPH0325599A JP H0325599 A JPH0325599 A JP H0325599A JP 15826789 A JP15826789 A JP 15826789A JP 15826789 A JP15826789 A JP 15826789A JP H0325599 A JPH0325599 A JP H0325599A
Authority
JP
Japan
Prior art keywords
telemeter
data
time
flying
ground
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
JP15826789A
Other languages
Japanese (ja)
Inventor
Masato Takeno
竹埜 正人
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 JP15826789A priority Critical patent/JPH0325599A/en
Publication of JPH0325599A publication Critical patent/JPH0325599A/en
Pending legal-status Critical Current

Links

Abstract

PURPOSE:To perform the flying analysis of a rocket, etc., more accurately than ever by storing measuring data under the worse transmission condition of a telemeter in a memory device, and telemeter-transmitting storage to the ground by reading out at a time when the telemeter transmission condition is stabilized and also, no collection of flying data is required. CONSTITUTION:The measuring data via a low-pass filter 1 and an A/D (analog/ digital) converter 2 is stored in the memory device 3 at a time when the defect of the transmission condition is predicted. The measuring data stored in the memory device 3 is read out with a signal from a timer 8 at a time when, for example, no measurement of the flying data is required such as the rocket drops, etc., and is transmitted to the ground from a switch 5 after passing a D/A converter 4 via a telemeter device not shown in figure. Thus, since the measuring data at a time when the transmission condition is worse is stored transiently with the timer 8 and it is transmitted to the ground by reading out at a time when no collection of the measuring data is required, the analysis of the flying data can be performed more accurately than ever.

Description

【発明の詳細な説明】 (産業上の利用分野) 本発明は、宇宙It測ロケット等の飛翔体に搭載し,各
種の飛翔データを正確に収集するための飛翔データ収集
装置に関する。
DETAILED DESCRIPTION OF THE INVENTION (Field of Industrial Application) The present invention relates to a flight data collection device that is mounted on a flying object such as a space probe rocket and is used to accurately collect various kinds of flight data.

(従来の技術) 従来、たとえば宇宙am用ロケットの飛翔中に計測した
各種の自動計測データは、直接,テレメータによって地
上に送られてモニタされ、あるいは解析されている。
(Prior Art) Conventionally, various types of automatic measurement data measured during the flight of, for example, a space rocket have been directly sent to the ground using a telemeter and monitored or analyzed.

(発明が解決しようとするW題) しかしながら、高速に飛翔するロケットからのテレメー
タ信号は、ロケットエンジンの燃焼中に電界の乱れを発
生してロックオフし、計測データの収集に欠落を生ずる
大きな欠点を有している。
(Problem W to be solved by the invention) However, the telemeter signal from a rocket flying at high speed has a major drawback in that it locks off due to disturbances in the electric field during combustion of the rocket engine, resulting in missing measurement data. have.

本発明は上述のような、高飛翔体の飛翔データ収集上の
欠点を排除した飛翔データ収集装置の提供を目的とする
. (課題を解決するための手段) 本発明は上記の目的を、飛翔体に設置した飛翔データ計
測装置とテレメータ装置との間に記憶装置を設け、ロケ
ットエンジン燃焼時等に発生するテレメータ伝送条件不
良時の、上記飛翔データ計測装置の計測データを上記記
憶装置に記憶させ,その記憶をテレメータ伝送条件が安
定し、かつ飛翔データの収集が不要な時間に読みださせ
て、地上にテレメータ伝送する構或により達成する。
An object of the present invention is to provide a flight data collection device that eliminates the above-mentioned drawbacks in collecting flight data of high-flying objects. (Means for Solving the Problems) The present invention achieves the above object by providing a storage device between a flight data measuring device installed on a flying object and a telemeter device, and by providing a storage device between a flight data measuring device installed on a flying object and a telemeter device. The measurement data of the flight data measurement device is stored in the storage device at the time of the flight, and the stored data is read out at a time when telemeter transmission conditions are stable and collection of flight data is unnecessary, and the data is telemeter transmitted to the ground. Achieved by some means.

(作 用) 本発明によれば、テレメータ伝送条件が不良時でも計測
データが欠落せず、地上において安全に収集可能である
から、ロケットの飛翔データの解析をより正確に行なう
ことが可能になる。
(Function) According to the present invention, measurement data is not lost even when telemeter transmission conditions are poor and can be safely collected on the ground, making it possible to analyze rocket flight data more accurately. .

(実施例) 以下、本発明を図面を用いて詳細に説明する.図面は本
発明の一実施例の構成要部を示すブロック図で、1はロ
ーバスフィルタであり入力端子T1から印加される、図
示しない自動計測装置からのロケット飛翔データの周波
数帯域範囲を決めており.その出力データはA/D(ア
ナログ/ディジタル)変換器2を経てメモリ装置3に入
力され一時記憶される。4はメモリ装置3から読みだし
た出力を図示しないテレメータ装置に送出するためのD
/A(ディジタル/アナログ)変換器,5はテレメータ
伝送条件の良否によって切換えられる切換器で、その出
力は出力端子T2からテレメータ装置に印加され地上に
テレメータ伝送される。
(Example) Hereinafter, the present invention will be explained in detail using the drawings. The drawing is a block diagram showing the main components of an embodiment of the present invention, in which 1 is a low-pass filter that determines the frequency band range of rocket flight data from an automatic measuring device (not shown), which is applied from an input terminal T1. Ori. The output data is input to a memory device 3 via an A/D (analog/digital) converter 2 and temporarily stored. 4 is D for sending the output read from the memory device 3 to a telemeter device (not shown).
The /A (digital/analog) converter 5 is a switch that is switched depending on the quality of telemeter transmission conditions, and its output is applied to the telemeter device from the output terminal T2 and transmitted by telemeter to the ground.

また、6はメモリ装置3に書き込み、または読みだしの
タイミングを調整するクロックパルス発生器、7はメモ
リ装置3の記憶に必要なアドレスカウンタであり、8は
切換器5に切換信号を印加するためのタイマである。
Further, 6 is a clock pulse generator that adjusts the timing of writing to or reading from the memory device 3, 7 is an address counter necessary for storing data in the memory device 3, and 8 is for applying a switching signal to the switching device 5. This is the timer.

以上のようにM或した本発明の飛翔データ収集装置は、
まず、図示しない自動計測装置からの飛翔データ出力を
、ローパスフィルタ1に加え周波数帯域が決められてA
/D変換器2、および切換器5に印加される。タイマ8
はテレメータ伝送条件の良否を予測してオンオフ時間が
ブリセットされており、伝送条件を良好と予測した時間
中の計測データはローパスフィルタ1から直接、切換器
5を介し出力端子T2を経て,図示しないテレメータ装
置により地上に伝送される。反対に伝送条件を不良に予
測した時間の間はローバスフィルタ1、およびA/D変
換器2を経た計測データをメモリ装置3に記憶させる。
As described above, the flight data collection device of the present invention has M.
First, flight data output from an automatic measurement device (not shown) is applied to a low-pass filter 1, and a frequency band is determined.
/D converter 2 and switch 5. timer 8
The on/off time is preset by predicting whether the telemeter transmission conditions are good or not, and the measurement data during the time when the transmission conditions are predicted to be good is directly transmitted from the low-pass filter 1, via the switch 5, and through the output terminal T2, as shown in the figure. It is transmitted to the ground by a telemeter device that does not. On the other hand, during the time when the transmission conditions are predicted to be poor, the measurement data that has passed through the low-pass filter 1 and the A/D converter 2 is stored in the memory device 3.

上記のようにしてメモリ装置3に記憶された計測データ
は、たとえば飛翔データの測定を必要としないロケット
落下時等の時間に、タイマ8からの信号によって読みだ
され、D/A変換器4を経て切換85から図示しないテ
レメータ装置を介して地上に伝送される。
The measurement data stored in the memory device 3 as described above is read out by the signal from the timer 8 at times such as when the rocket falls, and the D/A converter 4 is The signal is then transmitted from the switch 85 to the ground via a telemeter device (not shown).

本発明は、以上説明したようにタイマ8により伝送条件
が悪い時間の計測データを一時記憶させておき、計測デ
ータの収集が不要な時間に読みだして地上にテレメータ
伝送するから、計測データは欠落なく完全に収集可能で
あり,飛翔データの解析をより正確にすることができる
As explained above, the present invention uses the timer 8 to temporarily store measurement data during times when transmission conditions are poor, reads it out at times when measurement data collection is unnecessary, and transmits it to the ground via telemeter, so that measurement data may be lost. It is possible to collect data completely without any problems, and the analysis of flight data can be made more accurate.

(発明の効果) 以上、説明して明らかなように本発明は、テレメータの
伝送条件によっては収集に欠落を生ずる計測データを、
伝送条件に関係なく完全に収集可能となるから、したが
ってロケット等の飛翔解析をより正確なものにする効果
があり、ロケット技術等の発展に大いに貢献する。
(Effects of the Invention) As is clear from the above explanation, the present invention can collect measurement data that may be missing depending on the transmission conditions of the telemeter.
Since it is possible to completely collect data regardless of transmission conditions, it has the effect of making rocket flight analysis more accurate, and greatly contributes to the development of rocket technology.

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

図面は本発明の一実施例の構或要部を示すブロック図で
ある。 l ・・・ ローパスフィルタ、 2 ・・・A/D変
換器、 3 ・・・メモリ装置、 4 ・・・D/A変
換器5 5・・・切換器、 6・・・クロックパルス発
生器、 7 ・・・アドレスカウンタ、 8・・・タイ
マ。
The drawing is a block diagram showing a main part of an embodiment of the present invention. 1...Low pass filter, 2...A/D converter, 3...Memory device, 4...D/A converter 5 5...Switcher, 6...Clock pulse generator, 7...Address counter, 8...Timer.

Claims (1)

【特許請求の範囲】[Claims] 飛翔体に設置した飛翔データ計測装置とテレメータ装置
との間に記憶装置を設け、ロケットエンジン燃焼時等に
発生するテレメータ伝送条件不良時の、上記飛翔データ
計測装置の計測データを上記記憶装置に記憶させ、その
記憶をテレメータ伝送条件が安定し、かつ飛翔データの
収集が不要な時間に読みださせて、地上にテレメータ伝
送する構成を特徴とする飛翔データ収集装置。
A storage device is provided between a flight data measurement device installed on a flying object and a telemeter device, and measurement data of the flight data measurement device is stored in the storage device when telemeter transmission conditions are poor, such as during rocket engine combustion. A flight data collection device characterized by a configuration in which the data is read out at a time when telemeter transmission conditions are stable and collection of flight data is unnecessary, and telemeter transmitted to the ground.
JP15826789A 1989-06-22 1989-06-22 Flying data collector Pending JPH0325599A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP15826789A JPH0325599A (en) 1989-06-22 1989-06-22 Flying data collector

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP15826789A JPH0325599A (en) 1989-06-22 1989-06-22 Flying data collector

Publications (1)

Publication Number Publication Date
JPH0325599A true JPH0325599A (en) 1991-02-04

Family

ID=15667878

Family Applications (1)

Application Number Title Priority Date Filing Date
JP15826789A Pending JPH0325599A (en) 1989-06-22 1989-06-22 Flying data collector

Country Status (1)

Country Link
JP (1) JPH0325599A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8136899B2 (en) 2006-07-05 2012-03-20 Sanyo Electric Co., Ltd. Rack device and incubator having the same

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8136899B2 (en) 2006-07-05 2012-03-20 Sanyo Electric Co., Ltd. Rack device and incubator having the same

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