JPH0278961A - Angular velocity detecting device - Google Patents
Angular velocity detecting deviceInfo
- Publication number
- JPH0278961A JPH0278961A JP63230271A JP23027188A JPH0278961A JP H0278961 A JPH0278961 A JP H0278961A JP 63230271 A JP63230271 A JP 63230271A JP 23027188 A JP23027188 A JP 23027188A JP H0278961 A JPH0278961 A JP H0278961A
- Authority
- JP
- Japan
- Prior art keywords
- detector
- angular velocity
- temperature
- circuit
- bias
- 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
- 238000006073 displacement reaction Methods 0.000 claims 2
- 230000003321 amplification Effects 0.000 claims 1
- 238000003199 nucleic acid amplification method Methods 0.000 claims 1
- 238000012937 correction Methods 0.000 abstract description 2
- 238000001514 detection method Methods 0.000 description 9
- 238000005259 measurement Methods 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000005286 illumination Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
Landscapes
- Gyroscopes (AREA)
Abstract
Description
【発明の詳細な説明】 〔産業上の利用分野〕 この発明は人工衛星等の飛しよう体に搭載され。[Detailed description of the invention] [Industrial application field] This invention can be mounted on flying objects such as artificial satellites.
角速度を検出する角速度検出装置に関するものである。The present invention relates to an angular velocity detection device that detects angular velocity.
従来のこの種装置としては、第2図に示すものがあった
。図において(1)は検出器、+21ijジヤイロ。A conventional device of this type is shown in FIG. In the figure, (1) is a detector, +21ij gyro.
(3)はトルカ、(4)はピックオフ、(51はアンプ
、(6Iは電流検出器である。(3) is a torquer, (4) is a pickoff, (51 is an amplifier, and (6I is a current detector).
図において検出器口)に角速度が加わると、ジンバル等
で固定されたジャイロ(2)が変位する。ピックオフ(
41でその移動量を検出し、アンプ(5)で増幅した後
、トルカ(31でジャイロ(2珈;原点に止まる様にサ
ーボループを構成すると、トルカ131のドライブ電流
を電流検出器(6)により検出する事により検出器(1
)に加わった角速度が計測される。When an angular velocity is applied to the detector port (in the figure), the gyro (2) fixed with a gimbal or the like is displaced. Pickoff (
After detecting the amount of movement with 41 and amplifying it with an amplifier (5), the torquer (31 with a gyro (2)) configures a servo loop so that it stops at the origin, and the drive current of the torquer 131 is detected with a current detector (6). The detector (1
) is measured.
しかし従来のこの種装置では、検出器(11内のトルカ
131及びピックオフ(4)等の温度変化による特性変
化のため正確な測定が行えなかった、更に一般に人工衛
星等では、その環境温度範囲がきわめて広いので精密な
測定はできなかった。However, with conventional devices of this type, accurate measurements could not be made due to changes in the characteristics of the detector (the torquer 131 in the detector 11 and the pickoff (4), etc.) due to temperature changes. It was so wide that precise measurements could not be made.
この発明は上1のような課Iを解決するためになされた
もので、簡単な方法により検出器等の温度変化があって
も正確な測定の行える角速度検出装置を提供するもので
ある。The present invention has been made in order to solve the problem I mentioned above, and provides an angular velocity detection device that can perform accurate measurement even if there is a temperature change of the detector etc. using a simple method.
この発明に係る角速度検出装置は、検出器(1)付近の
温度を検出し、これにより電流検出器(6)の出力信号
のゲイン及びバイアス値を切り換える事により温度変化
に依存しない出力信号を得るものである。The angular velocity detection device according to the present invention detects the temperature near the detector (1), and thereby obtains an output signal that is independent of temperature changes by switching the gain and bias value of the output signal of the current detector (6). It is something.
この発明における角速度検出装置1d、温度補正を自動
的に行う事により、正確な角速度の計測が行える。The angular velocity detection device 1d of the present invention can accurately measure angular velocity by automatically performing temperature correction.
以下図面を用いてこの発明の一実施例について説明する
。An embodiment of the present invention will be described below with reference to the drawings.
第1図はこの発明の一実施例を示す構成ブロック図であ
る。図において(7)はゲイン切替回路、(8)はバイ
アス付加回μ、(9)はサーミスタ、 flGは定電流
口μ、α11け温度検出回路、α2はA/Dコンバータ
、(1(はROMである。FIG. 1 is a block diagram showing an embodiment of the present invention. In the figure, (7) is a gain switching circuit, (8) is a bias addition circuit μ, (9) is a thermistor, flG is a constant current port μ, α11 is a temperature detection circuit, α2 is an A/D converter, (1 (is a ROM) It is.
検出器(1)内のジャイロ+21. トルカ(3)、
ピックオフ(41及びアンプ(51電流検出器(61に
より角速度を検出するのは従来装置と同じである、図に
おいて。Gyro in detector (1) +21. Toluca (3),
In the figure, the angular velocity is detected by a pickoff (41) and an amplifier (51) and a current detector (61), as in the conventional device.
サーミスタ+91は検出器(1)の近傍に西装置され、
検出器(1)近傍の温度変化によりその抵抗値が変化す
るので、定電流回路α[I′EIび検出口gfll+に
より検出器(1)の温度が検出される。また温度検出回
路011の出力信号は、A/Dコンバータ(IX5によ
りディジタル信号に変換され、 ROM(13のアド
レスラインに接続される、従って検出器(1)の近傍の
温度に従った内容のデータが、 ROMα3から呼び出
される。まだROM +13のデータの内容として、地
上試験により測定された校正データとして、各温度にお
いて電流検出器(6)の出力信号に適切なゲイン及びバ
イアスを付加し誤差信号が最小となる様に、ゲイン切替
回路(7+ EIびバイアス付加回路イ8)を選択する
ためのデータを入力しておけば、バイアス付加回路(8
)の出力信号は、検出器flG内のトルカ(31,ピッ
クオフ+41の温度変化によらず常に正確な角速度を示
すものである。Thermistor +91 is installed near the detector (1),
Since the resistance value of the detector (1) changes due to a change in temperature near the detector (1), the temperature of the detector (1) is detected by the constant current circuit α[I'EI and the detection port gfll+. In addition, the output signal of the temperature detection circuit 011 is converted into a digital signal by the A/D converter (IX5), and is connected to the address line of the ROM (13). is called from ROMα3.The content of the data in ROM+13 is the calibration data measured in the ground test, and an error signal is generated by adding appropriate gain and bias to the output signal of the current detector (6) at each temperature. If you input the data for selecting the gain switching circuit (7 + EI and bias addition circuit A 8) so that the bias addition circuit (8
) always indicates an accurate angular velocity regardless of temperature changes of the torquer (31, pickoff +41) in the detector flG.
なお、上gr例では、サーミスタにより温度検出を行う
様にしたが、温度センサとしてサーミスタに限定される
ものでない。In addition, in the above gr example, the temperature is detected using a thermistor, but the temperature sensor is not limited to the thermistor.
以上の様にこの発明によれば、検出器(1)の温度を(
ill定し、 ROMを使用した簡単な回路により補
正する稟により環境温度に依存しないで正確な測定の行
える角速度検出装置が得られるものである。As described above, according to the present invention, the temperature of the detector (1) is
An angular velocity detection device that can perform accurate measurements without depending on the environmental temperature can be obtained by correcting the illumination using a simple circuit using a ROM.
第1図はこの発明による角速度検出装置の一実施例を示
す構成ブロック図、第2図は従来の角速度検出装置を示
す構成ブロック因である。
図中、(1)は検出器、(2)はジャイロ、(3)はト
ルカ。
(4)はピックオフ、(51はアンプ、(6)は電流検
出器。
(7)げゲイン切替回路、 181はバイアス付加回路
、(91はサーミスタ、 aaは定電流回路、a11は
温度検出回路、 (12はA/Dコンバータ、α3はR
OMである。
なお1図中同一あるいは相当部分には、同一符号を付し
て示しである。FIG. 1 is a block diagram showing an embodiment of an angular velocity detecting device according to the present invention, and FIG. 2 is a block diagram showing a conventional angular velocity detecting device. In the figure, (1) is a detector, (2) is a gyro, and (3) is a torquer. (4) is a pickoff, (51 is an amplifier, (6) is a current detector. (7) is a gain switching circuit, 181 is a bias addition circuit, (91 is a thermistor, aa is a constant current circuit, a11 is a temperature detection circuit, (12 is A/D converter, α3 is R
It's OM. Note that the same or corresponding parts in FIG. 1 are designated by the same reference numerals.
Claims (1)
度を検出するセンサにおいて、飛しよう体の角速度を検
出するジャイロと、このジャイロの変位を計測するピッ
クオフと、このピックオフの出力を増巾するアンプと、
このアンプの出力電流により前記ジャイロの変位を修正
するトルカと、このトルカの電流を検出する電流検出器
と、周辺温度を計測する温度計測器と、温度計測器の出
力をディジタル信号に変換するA/D変換器と、A/D
変換器の出力をアドレス入力とするROMと、前記電流
検出器出力を入力とし前記ROMのデータの内容に従つ
てゲイン切替及びバイアス付加する回路からなる事を特
徴とする角速度検出装置。A sensor mounted on a flying object such as an artificial satellite that detects the angular velocity of the flying object includes a gyro that detects the angular velocity of the flying object, a pickoff that measures the displacement of this gyro, and an amplification of the output of this pickoff. An amplifier that
A torquer that corrects the displacement of the gyro using the output current of this amplifier, a current detector that detects the current of this torquer, a temperature measuring device that measures the surrounding temperature, and an A that converts the output of the temperature measuring device into a digital signal. /D converter and A/D
An angular velocity detecting device comprising: a ROM having the output of the converter as an address input; and a circuit having the output of the current detector as the input and performing gain switching and bias addition according to the contents of data in the ROM.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP63230271A JPH0278961A (en) | 1988-09-14 | 1988-09-14 | Angular velocity detecting device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP63230271A JPH0278961A (en) | 1988-09-14 | 1988-09-14 | Angular velocity detecting device |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH0278961A true JPH0278961A (en) | 1990-03-19 |
Family
ID=16905185
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP63230271A Pending JPH0278961A (en) | 1988-09-14 | 1988-09-14 | Angular velocity detecting device |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH0278961A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2395322A1 (en) | 2010-06-14 | 2011-12-14 | Eurocopter | Improved inertial measurement device and aircraft carrying such a device |
-
1988
- 1988-09-14 JP JP63230271A patent/JPH0278961A/en active Pending
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2395322A1 (en) | 2010-06-14 | 2011-12-14 | Eurocopter | Improved inertial measurement device and aircraft carrying such a device |
US8738317B2 (en) | 2010-06-14 | 2014-05-27 | Airbus Helicopters | Inertial measurement device and an aircraft including such a device |
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