JPS59610A - Optical fiber gyroscope - Google Patents

Optical fiber gyroscope

Info

Publication number
JPS59610A
JPS59610A JP57109918A JP10991882A JPS59610A JP S59610 A JPS59610 A JP S59610A JP 57109918 A JP57109918 A JP 57109918A JP 10991882 A JP10991882 A JP 10991882A JP S59610 A JPS59610 A JP S59610A
Authority
JP
Japan
Prior art keywords
light
optical fiber
optical
output
output end
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
JP57109918A
Other languages
Japanese (ja)
Inventor
Shigefumi Masuda
増田 重史
Akira Okamoto
明 岡本
Takeo Iwama
岩間 武夫
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.)
Fujitsu Ltd
Original Assignee
Fujitsu 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 Fujitsu Ltd filed Critical Fujitsu Ltd
Priority to JP57109918A priority Critical patent/JPS59610A/en
Publication of JPS59610A publication Critical patent/JPS59610A/en
Pending legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • G01C19/58Turn-sensitive devices without moving masses
    • G01C19/64Gyrometers using the Sagnac effect, i.e. rotation-induced shifts between counter-rotating electromagnetic beams
    • G01C19/72Gyrometers using the Sagnac effect, i.e. rotation-induced shifts between counter-rotating electromagnetic beams with counter-rotating light beams in a passive ring, e.g. fibre laser gyrometers

Landscapes

  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Optics & Photonics (AREA)
  • Electromagnetism (AREA)
  • Power Engineering (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Gyroscopes (AREA)
  • Lasers (AREA)

Abstract

PURPOSE:To improve an S/N, by providing optical fiber separately to left rotating light and right rotating light. CONSTITUTION:As left rotating light and right rotating light transfer respectively different optical fibers 2-1, 2-1, even if there is return light at incident terminals T1, T2 by Rayleigh scattering, etc., the return light does not have effects on outputting light of output terminals T3, T4. Therefore, an S/N in output signal of a differential amplifier 5 is improved.

Description

【発明の詳細な説明】 fil  発明の技術分野 本発明は角速度センサとして作用する光ファイバを用い
た光フアイバジャイロスコープに関する。
DETAILED DESCRIPTION OF THE INVENTION fil Technical Field of the Invention The present invention relates to fiber optic gyroscopes that use optical fibers to act as angular velocity sensors.

(2)技術の背景 ジャイロスコープは周囲の状況と無関係に最初に設定し
た一定の方向を指示する1件質を利用したものであシ、
りとえば、ジャイロスコープを搭載した動体の角速度を
検出し、運動方向、速度等を決定できる。従って、ジャ
イロスコープは飛行機、船舶等の長距離を運行する乗物
の方向指示、姿勢制御等に必須のものである。
(2) Background of the technology Gyroscopes use a single characteristic that indicates a fixed direction that is initially set regardless of the surrounding situation.
For example, it is possible to detect the angular velocity of a moving object equipped with a gyroscope and determine the direction of movement, speed, etc. Therefore, gyroscopes are essential for direction indication, attitude control, etc. of vehicles that operate over long distances, such as airplanes and ships.

一般に、ジャイロスコープは回転体の慣性モーメントを
利用した機械的なものが主流であったが、最近、小型、
低電力、低価格等の利点を有する光フアイバジャイロス
コープが提案されている。
In general, gyroscopes were mainly mechanical ones that utilized the moment of inertia of a rotating body, but recently, gyroscopes have become smaller and
Fiber optic gyroscopes have been proposed which have advantages such as low power consumption and low cost.

(3)従来技術と問題点 従来の光フアイバジャイロスコープにおいては、1本の
光ファイバをコイル状に多数回巻回している。この光フ
ァイバの両端から左回り光および右回り光を入射させる
と、ジャイロスコープの角速度Qに応じて左右両回り光
間に位相差Δθが発生する。これはザブナック効果と呼
ばれ、位相差△θは次式で表わされる。
(3) Prior Art and Problems In a conventional fiber optic gyroscope, a single optical fiber is wound into a coil many times. When counterclockwise light and clockwise light are input from both ends of this optical fiber, a phase difference Δθ is generated between the left and right lights depending on the angular velocity Q of the gyroscope. This is called the Zabnak effect, and the phase difference Δθ is expressed by the following equation.

8πLR Δθン□Ω λC ただし、Lは7アイパ長 Rはファイバコイルの曲線半径 λは光波長 Cは真空中の光速度 左回)光および右回り光は単一モードファイバで行って
いるので、光ファイバの入力端は出力端でもあり、この
結果、光ファイバの出力端(入力端)で光分岐が必要で
ある。
8πLR Δθn□Ω λC However, L is 7 eye length R is the radius of the curve of the fiber coil λ is the light wavelength C is the speed of light in vacuum. The input end of an optical fiber is also the output end, and as a result, an optical branch is required at the output end (input end) of the optical fiber.

しかしながら、光ファイバの中では、微細な鴨折率のゆ
らぎがあり、主としてレイリー散乱と呼ばれる散乱損失
が多かれ少なかれ発生する。従って、たとえば、左回り
光の出力光と右回り光の入射光とを光ファイバの出力端
(入力端)で分岐すると、左回り光の出力光には必ず右
回り光の入射光の散乱による戻り光が雑音として混入す
る。この結果、S/N(信月/雑音)比が低いという問
題点がある。
However, within an optical fiber, there are minute fluctuations in the refractive index, and a scattering loss called Rayleigh scattering occurs to a greater or lesser extent. Therefore, for example, if the output light of the counterclockwise light and the input light of the clockwise light are split at the output end (input end) of an optical fiber, the output light of the counterclockwise light will always be affected by the scattering of the incident light of the clockwise light. Return light mixes in as noise. As a result, there is a problem that the S/N (signal/noise) ratio is low.

(4)発明の目的 本発明の目的は、コイル状に巻回された光ファイバを左
右回り光に対[2て別個に設けるという構想にもとづき
、光ファイバの入力端および出力端を識別するようにし
、これにより、光ファイバの出力端においてたとえば左
回り光の出力光に右回り光の戻り光を混入しないように
して、87N比を向上せしめ、上述の従来形における問
題点を解決することにある。
(4) Purpose of the Invention The purpose of the present invention is to provide a method for identifying the input end and the output end of the optical fiber based on the concept of separately providing a coiled optical fiber for left and right directions. As a result, the return light of the clockwise light is prevented from being mixed with the output light of the counterclockwise light at the output end of the optical fiber, thereby improving the 87N ratio and solving the above-mentioned problems with the conventional type. be.

(5)発明の構成 本発明によれば、コイル状に且つ互いに平行に多数回巻
回された一対の光ファイバと、各光ファイバの入力端に
左回シ光および右回多光を同時に入射させるレーザ発生
手段と、前記各光ファイバの出力端における出力光を電
気信号に変換する第1、第2の変換手段と、該第1、第
2の変換手段の電気信号の差分を増幅する差動増幅手段
とを具備することを特徴とする光フアイバジャイロスコ
ープが提供される。
(5) Structure of the Invention According to the present invention, a pair of optical fibers are wound many times parallel to each other in a coil shape, and a left-handed beam and a right-handed beam are simultaneously input to the input end of each optical fiber. first and second conversion means for converting the output light at the output end of each optical fiber into an electrical signal; and a difference for amplifying the difference between the electrical signals of the first and second conversion means. A fiber optic gyroscope is provided, characterized in that it comprises dynamic amplification means.

また、本発明によれば、コイル状に且つ互いに平行に多
数回巻回された一対の光ファイバと、該光ファイバの一
方の出力端に設けられた光反射−と、レーザ発生手段と
、該レーザ発生手段のレーザ光を前記各党ファイバの入
力端に左回り光および右回り光として入射させ且つ前記
各党ファイバの入力端における戻り光を受光するための
光方向性結合器と、該光方向結合器の戻如光成分を電気
信号に変換する第1の変換手段と、前記光ファイバの他
方の出力端における出力光を電気信号に変換する第2の
変換手段と、該第1、第2の変換手段の電気信号の差分
を増幅する差動増幅手段とを具備することを特徴とする
光フアイバジャイロスコープが提供される。
Further, according to the present invention, a pair of optical fibers are wound many times in a coil shape and parallel to each other, a light reflection device provided at one output end of the optical fiber, a laser generating means, and a light reflection device provided at one output end of the optical fiber. an optical directional coupler for making the laser beam of the laser generating means enter the input end of each party fiber as counterclockwise light and clockwise light, and receiving the returned light at the input end of each party fiber; and the light directional coupler. a first converting means for converting the returned light component of the optical fiber into an electrical signal; a second converting means for converting the output light at the other output end of the optical fiber into an electrical signal; There is provided an optical fiber gyroscope characterized by comprising differential amplification means for amplifying a difference between electrical signals of the conversion means.

(6)発明の実施例 以下、図面によシ本発明の詳細な説明する。(6) Examples of the invention Hereinafter, the present invention will be explained in detail with reference to the drawings.

第1図は本発明に係る光フアイバジャイロスコープの第
1の実施例を示す図である。第1図において、1は両巻
きの光7アイパコイルであって、一対の光ファイバ2−
1.2−2が互いに平行に多数回巻回されている。この
場合、光ファイバ2−1は左回り光用であり、光ファイ
バ2−2は右回り光用である。光ファイバ2−1の入力
端T1および光ファイバ2−2の入力端T2には、レー
ザ発生手段たとえばレーザダイオード2がら光方向性結
合器(3端子)3およびレンズ(図示せず)を介してレ
ーザ光が同時に入射される。また、光ファイバ2−1の
出力端T5および光ファイバ2−2の出力端T4 から
の出力光はレンズ(図示せず)を介して光/′#を気変
換器4−1゜4−またとえばPIN7オトダイオード、
アヴアランシェフォトダイオード(APD)に供給され
て電気信号に変換される。しかる後に、各変換器4−1
.4−2の出力信号の差分が差動増幅器5によって増幅
される。
FIG. 1 is a diagram showing a first embodiment of an optical fiber gyroscope according to the present invention. In FIG. 1, reference numeral 1 denotes a double-wound optical 7-eyeper coil, and a pair of optical fibers 2-
1.2-2 are wound many times parallel to each other. In this case, the optical fiber 2-1 is for counterclockwise light, and the optical fiber 2-2 is for clockwise light. A laser generating means such as a laser diode 2 is connected to the input end T1 of the optical fiber 2-1 and the input end T2 of the optical fiber 2-2 through an optical directional coupler (three terminals) 3 and a lens (not shown). Laser beams are simultaneously incident. Further, the output light from the output end T5 of the optical fiber 2-1 and the output end T4 of the optical fiber 2-2 is transmitted through a lens (not shown) to the air converter 4-1. For example, PIN7 otodiode,
The signal is supplied to an Avalanche photodiode (APD) and converted into an electrical signal. After that, each converter 4-1
.. The difference between the output signals 4-2 is amplified by the differential amplifier 5.

たとえば、角速度Ωに対して左回り光の位相偏移が2Δ
θで光/it気変気密換器1に与えられると、右回り光
の位相偏移は一2Δθで光/′シ気変換器4−2に与え
られる。すなわち、差動増幅器5の出力には位相偏移4
Δθが現われることになる。
For example, the phase shift of counterclockwise light with respect to the angular velocity Ω is 2Δ
When the light is applied to the air/air converter 1 at θ, the phase shift of the clockwise light is applied to the air/air converter 4-2 at -2Δθ. That is, the output of the differential amplifier 5 has a phase shift of 4
Δθ will appear.

第1図においては、左回り光および右回り光はそれぞれ
異なる光ファイバ2−1.2−2を伝達するので、k二
とえレイリ散乱等により入力端TI。
In FIG. 1, since the left-handed light and the right-handed light are transmitted through different optical fibers 2-1, 2-2, the input end TI is affected by Rayleigh scattering and the like.

T2 に戻り光があっても、その戻〃光は出力端T5゜
T4  における出力光に影響を及はさない。従って、
差動増幅器5の出力信号における87N比は向上する。
Even if there is returned light at T2, the returned light does not affect the output light at the output end T5°T4. Therefore,
The 87N ratio in the output signal of the differential amplifier 5 is improved.

第2図は本発明に係る元ファイバジャイロスコープの第
2の実施例を示す図である。第2図においては、第1図
の場合と異なシ、光ファイバ2−2の出力端T4にはほ
ぼ100%の光反射端6が設けられており、また、光/
電気変換器4−2は光方向性結合器(4端子)3′を介
して光ファイバ2−1の入力端T1  および光ファイ
バ2−2の入力端T21cおける戻り光を受光する。た
だし、この場合、特に、光ファイバ2−2の出力端T4
には光反射端6艇設けられているので光ファイバ2−2
の入力端T2における戻り光を受光することになる。こ
の戻り光の位相偏移は一2Δθ(右回如)+2Δθ(左
回り)=0であって、主にレイリ散乱光に相当する。従
って、光/¥IL気変換器4−2の出力を適切な減衰器
(図示せず)を介して差動増幅器5に供給すれば、差動
増幅器5の出力にはレイリ散乱光等の影響を低減できる
。なお、この場合、差動増幅器5の出力における位相偏
移は2Δθである。
FIG. 2 is a diagram showing a second embodiment of the original fiber gyroscope according to the present invention. In FIG. 2, unlike the case in FIG. 1, the output end T4 of the optical fiber 2-2 is provided with an end 6 that reflects almost 100% of the light.
The electrical converter 4-2 receives the returned light at the input end T1 of the optical fiber 2-1 and the input end T21c of the optical fiber 2-2 via the optical directional coupler (four terminals) 3'. However, in this case, in particular, the output end T4 of the optical fiber 2-2
Since the optical fiber 2-2 is equipped with 6 light reflecting ends,
The returned light at the input end T2 of the input terminal T2 is received. The phase shift of this returned light is -2Δθ (clockwise rotation)+2Δθ (counterclockwise rotation)=0, and mainly corresponds to Rayleigh scattered light. Therefore, if the output of the optical/IL converter 4-2 is supplied to the differential amplifier 5 through an appropriate attenuator (not shown), the output of the differential amplifier 5 will be affected by Rayleigh scattered light, etc. can be reduced. Note that in this case, the phase shift in the output of the differential amplifier 5 is 2Δθ.

第3図は本発明に係る光フアイバジャイロスコープの第
3の実施例を示す図である。第3図においては、第2図
の要素に対して半透明の光反射端7が光ファイバ2−1
の出力端T3 に付加されている。従って、この場合、
光/電気変換器4−2は光ファイバ2−1の入力端T1
 における戻り光も多く受光することになる。しかし、
差動増幅器5の出力は第2図の場合とほぼ同様である。
FIG. 3 is a diagram showing a third embodiment of the optical fiber gyroscope according to the present invention. In FIG. 3, the translucent light-reflecting end 7 is connected to the optical fiber 2-1 relative to the element of FIG.
It is attached to the output terminal T3 of. Therefore, in this case,
The optical/electrical converter 4-2 is connected to the input end T1 of the optical fiber 2-1.
This means that a large amount of return light will be received. but,
The output of the differential amplifier 5 is almost the same as in FIG.

(7)発明の詳細 な説明したように本発明によれば、左右回り光に対して
光ファイバを別個に設けたので、たとえば左回り光の出
力には右回り光の戻り光が混入しなくなり、従って、S
/N比を向上させることができる。
(7) As described in detail, according to the present invention, separate optical fibers are provided for the left and right lights, so that, for example, the return light of the clockwise light does not mix into the output of the counterclockwise light. , therefore, S
/N ratio can be improved.

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

第1図、第2図、第3図は、それぞれ、本発明に係る光
フアイバジャイロスコープの第1、第2、第3の実施例
を示す図である。 1:光フアイバコイル、 2−1=左回り光用光ファイバ、 2−2:右回受光用光ファイバ、 3.57a光方向性結合器、 4−1.4−2:光/電気変換器、 5:差動増幅器、 6:光反射端、 7:半透明の光反射端。 特許出願人 富士通株式会社 特許出願代理人 弁理士 青 木   朗 弁理士西舘和之 弁理士内田幸男 弁理士 山 口 昭 之
FIG. 1, FIG. 2, and FIG. 3 are diagrams showing first, second, and third embodiments of the optical fiber gyroscope according to the present invention, respectively. 1: Optical fiber coil, 2-1 = Optical fiber for counterclockwise light, 2-2: Optical fiber for right-handed light reception, 3.57a optical directional coupler, 4-1.4-2: Optical/electrical converter , 5: Differential amplifier, 6: Light reflection end, 7: Translucent light reflection end. Patent applicant: Fujitsu Limited Patent application agent: Akira Aoki, patent attorney: Kazuyuki Nishidate, patent attorney: Yukio Uchida, patent attorney: Akira Yamaguchi

Claims (1)

【特許請求の範囲】 1、 コイル状に且つ互いに平行に巻回された一対の光
ファイバと、各光ファイバの入力端に左回り光および右
回り光を同時に入射させるレーザ発生手段と、前記各党
7アイパの出力端における出力光を電気信号に変換する
第1.第2の変換手段と、該第1.第2の変換手段の電
気信号の差分を増幅する差動増幅手段とを具備するとと
を特徴とする光フアイバジャイロスコープ。 λ コイル状に且つ互いに平行に巻回された一対の光フ
ァイバと、該光ファイバの一方の出力端に設けられた光
反射端と、レーザ発生手段と、該レーザ発生手段のレー
ザ光を前記各光ファイバの入力端に左回り光および右回
り光として入射させ且つ前記各党ファイバの入力端にお
ける戻り光を受光するための光方向性結合器と、該光方
向結合器の戻り光成分を電気信号に変換する第1の変換
手段と、前記光ファイバの他方の出方端における出力光
を電気信号に変換する第2の変換手段と、該第1.第2
の変換手段の蝋気層号の差分を増幅する差動増幅手段と
を具備することを%漱とする光フアイバジャイロスコー
プ。 五 前記光ファイバの他方の出力端に半透明の光反射端
を付加した特許請求の範囲第2項に記載の光フアイバジ
ャイロスコープ。
[Claims] 1. A pair of optical fibers wound parallel to each other in a coil shape, a laser generating means for simultaneously inputting counterclockwise light and clockwise light into the input end of each optical fiber, and each of the above-mentioned optical fibers. 7. The first converts the output light at the output end of the eyeper into an electrical signal. a second converting means; An optical fiber gyroscope comprising: differential amplification means for amplifying the difference between the electrical signals of the second conversion means. λ A pair of optical fibers wound in a coil shape in parallel to each other, a light reflecting end provided at one output end of the optical fiber, a laser generating means, and a laser beam of the laser generating means An optical directional coupler for inputting counterclockwise light and clockwise light into the input end of an optical fiber and receiving returned light at the input end of each fiber, and converting the returned light component of the optical directional coupler into an electrical signal. a first converting means for converting the output light at the other output end of the optical fiber into an electrical signal; Second
A fiber optic gyroscope is provided with differential amplification means for amplifying the difference between the two layers of the conversion means. 5. The optical fiber gyroscope according to claim 2, wherein a translucent light reflecting end is added to the other output end of the optical fiber.
JP57109918A 1982-06-28 1982-06-28 Optical fiber gyroscope Pending JPS59610A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP57109918A JPS59610A (en) 1982-06-28 1982-06-28 Optical fiber gyroscope

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP57109918A JPS59610A (en) 1982-06-28 1982-06-28 Optical fiber gyroscope

Publications (1)

Publication Number Publication Date
JPS59610A true JPS59610A (en) 1984-01-05

Family

ID=14522430

Family Applications (1)

Application Number Title Priority Date Filing Date
JP57109918A Pending JPS59610A (en) 1982-06-28 1982-06-28 Optical fiber gyroscope

Country Status (1)

Country Link
JP (1) JPS59610A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59170718A (en) * 1983-02-23 1984-09-27 Kyohei Sakuta Optical fiber gyroscope
WO1986002721A1 (en) * 1984-10-29 1986-05-09 Martin Marietta Corporation Fiber-optic rotation rate sensor having dual interferometer loops
FR2611897A1 (en) * 1987-03-05 1988-09-09 Smiths Industries Plc APPARATUS FOR MEASURING PHASE MODULATION IN OPTICAL FIBER
JPS6442418U (en) * 1987-09-07 1989-03-14

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS58214809A (en) * 1982-06-09 1983-12-14 Nippon Telegr & Teleph Corp <Ntt> Fiber gyro

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS58214809A (en) * 1982-06-09 1983-12-14 Nippon Telegr & Teleph Corp <Ntt> Fiber gyro

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59170718A (en) * 1983-02-23 1984-09-27 Kyohei Sakuta Optical fiber gyroscope
WO1986002721A1 (en) * 1984-10-29 1986-05-09 Martin Marietta Corporation Fiber-optic rotation rate sensor having dual interferometer loops
US4639138A (en) * 1984-10-29 1987-01-27 Martin Marietta Corporation Fiber-optic rotation rate sensor having dual interferometer loops
FR2611897A1 (en) * 1987-03-05 1988-09-09 Smiths Industries Plc APPARATUS FOR MEASURING PHASE MODULATION IN OPTICAL FIBER
JPS6442418U (en) * 1987-09-07 1989-03-14

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