[go: up one dir, main page]

JPS61226609A - Optical fiber gyro - Google Patents

Optical fiber gyro

Info

Publication number
JPS61226609A
JPS61226609A JP60068771A JP6877185A JPS61226609A JP S61226609 A JPS61226609 A JP S61226609A JP 60068771 A JP60068771 A JP 60068771A JP 6877185 A JP6877185 A JP 6877185A JP S61226609 A JPS61226609 A JP S61226609A
Authority
JP
Japan
Prior art keywords
optical fiber
wound
edge
bobbin
edge part
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
JP60068771A
Other languages
Japanese (ja)
Inventor
Toshihiko Yoshino
俊彦 芳野
Nobuaki Yoshida
宣昭 吉田
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.)
Nikon Corp
Original Assignee
Nippon Kogaku KK
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 Nippon Kogaku KK filed Critical Nippon Kogaku KK
Priority to JP60068771A priority Critical patent/JPS61226609A/en
Publication of JPS61226609A publication Critical patent/JPS61226609A/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
    • G01C19/721Details
    • G01C19/722Details of the mechanical construction

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)
  • Light Guides In General And Applications Therefor (AREA)

Abstract

PURPOSE:To remove the noise which occurs due to the local distortion of the optical fiber by a local temperature change, etc., applied to the optical fiber, and to obtain the optical fiber gyro with a high measuring accuracy by winding one optical fiber so that the part of the equal distance can be close from the center. CONSTITUTION:A central part 12c of the optical fiber is fixed to one edge part 11a of a bobbin 11, one edge 12a is clogged and wound from one edge 11a of the bobbin 11 to other edge part 11b, and next, other edge 12b of the optical fiber is clogged and wound from one edge part 11a to other edge part 11b in the reverse direction on it. Here, for the winding direction of the optical fiber, when respective edges 12a and 12b are wound, they are wound in the opposite direction, and the optical fiber as a whole is finally wound so that it can be the same direction. Next, one edge 12a of the optical fiber is clogged and wound from other edge part 11b of the bobbin 11 to one edge part 11a as the third layer. Further, other edge 12b of the optical fiber is also clogged and wound from other edge part 11b of the bobbin 11 to one edge 11a as the fourth layer.

Description

【発明の詳細な説明】 (発明の技術分野) 本発明は光ファイバループを用いて角速度を検出する光
ファイバジャイロに関する。
DETAILED DESCRIPTION OF THE INVENTION (Technical Field of the Invention) The present invention relates to an optical fiber gyro that detects angular velocity using an optical fiber loop.

(発明の背景) 従来の光ファイバループを用いた光ファイバジャイロは
光ファイバループのサニアック効果による位相差を検出
して光ファイバループの回転角速度を検出するものであ
りその出力は 5=cos  Δφ となる、しかしこの出力では微小な回転角速度(Ω)に
対する感度が低いと言う欠点がある。この欠点を解決す
る方法として位相変調法が良(用いられる。位相の変調
法としてはピエゾ素子(PZT等)によって光ファイバ
の長さを伸縮させる方法が良く用いられる。
(Background of the Invention) An optical fiber gyro using a conventional optical fiber loop detects the rotational angular velocity of the optical fiber loop by detecting the phase difference due to the Saniac effect of the optical fiber loop, and its output is 5=cos Δφ. However, this output has the disadvantage of low sensitivity to minute rotational angular velocities (Ω). A phase modulation method is often used as a method to solve this drawback.As a phase modulation method, a method of expanding and contracting the length of an optical fiber using a piezo element (such as PZT) is often used.

ここで、位相変調信号をf(t) = a sinω、
tとし、変調点から光ファイバの両出力端に至るまでの
時間をT、、T、とすると干渉出力信号Sは5=cos
  (Δφ+r 1I(t  Tt)  f # (t
−Tz)]ζΔφJ+(77) Xcosω−a  (
t −+(Tt +h) )+(ω、の高調波成分) イ旦しrt =2a 5ini (Tt  Tt) (
al+aとなるので、これをω、の周波数でロック・イ
ン(lock−in)検波する事により S″qJt(η)Δφ となり、測定したい角速度Ωに比例した信号を高感度に
検出できる。このことを以下図面をもって更に詳しく説
明する。第3図は従来の光ファイバジャイロの原理を示
す図であって、1は光ファイバループ、2は光源部、3
はハーフミラ−14は光ディテクタ、5はピエゾ素子に
光ファイバを固く巻回してなる変調部である。光源部2
からの光はハーフミラ−3で反射される光と透過される
光に分けられ、これらの光は光フプイノくループをそれ
ぞれ右回りに進行する光と左回りに進行する光となる。
Here, the phase modulation signal is f(t) = a sinω,
t, and the time from the modulation point to both output ends of the optical fiber is T,,T, the interference output signal S is 5=cos
(Δφ+r 1I(t Tt) f # (t
−Tz)]ζΔφJ+(77) Xcosω−a (
t −+ (Tt + h) ) + (harmonic component of ω) Itanshirt = 2a 5ini (Tt Tt) (
al+a, so by lock-in detection of this at the frequency of ω, it becomes S″qJt(η)Δφ, and a signal proportional to the angular velocity Ω to be measured can be detected with high sensitivity. will be explained in more detail below with reference to the drawings. Fig. 3 is a diagram showing the principle of a conventional optical fiber gyro, in which 1 is an optical fiber loop, 2 is a light source section, and 3 is a diagram showing the principle of a conventional optical fiber gyro.
A half mirror 14 is a light detector, and 5 is a modulation section formed by tightly winding an optical fiber around a piezo element. Light source part 2
The light is divided into light reflected by the half mirror 3 and light transmitted, and these lights travel clockwise and counterclockwise through the optical loop, respectively.

光ファイバループをそれぞれ進行した光は前記ハーフミ
ラ−3でそれぞれ反射、透過されて光ディテクタ4に入
射する。上述の光ファイバループを右回りに進行する光
と左回りに進行する光とは該光ディテクタ4の受光面で
干渉する。この時光ファイバループが回転すると角速度
Ωに応じてサニアック効果が生ずる。サニテック効果に
よる光波の位相のシフト量Δφは次式で表される。
The light traveling through the optical fiber loops is reflected and transmitted by the half mirror 3 and enters the optical detector 4. The light traveling clockwise through the optical fiber loop and the light traveling counterclockwise interfere with each other on the light receiving surface of the optical detector 4. At this time, when the optical fiber loop rotates, a Saniac effect occurs depending on the angular velocity Ω. The phase shift amount Δφ of the light wave due to the Sanitec effect is expressed by the following equation.

Δφ=8πANΩ/λに こでAは光ファイバループによって囲まれる面積、Nは
光ファイバの巻回数、λは真空中の光の波長、Cは真空
中の光速度である。
Δφ=8πANΩ/λ where A is the area surrounded by the optical fiber loop, N is the number of turns of the optical fiber, λ is the wavelength of light in vacuum, and C is the speed of light in vacuum.

変調部5はピエゾ素子を一定周波数で駆動させる事によ
り該ピエゾ素子に固く巻回された光ファイバを伸縮せし
める。この光ファイバの伸縮により光ファイバループを
左回りに進行する光と右回りに進行する光は位相変調さ
れ、その結果光ディテクタ4の受光面での干渉光の基本
波成分は次式で与えられる。゛ S、=にΩJ+(η) cos ω11  (t−4(
T+  +Tz) )・−・−・−−−−一・−・・−
・−・−・−・−−−−−−−−・・・−(1)ここで
Kは定数、J、(η)は前述の1次第1種Be5sel
関数である。
The modulator 5 expands and contracts the optical fiber tightly wound around the piezo element by driving the piezo element at a constant frequency. Due to this expansion and contraction of the optical fiber, the phase of the light traveling counterclockwise and the light traveling clockwise in the optical fiber loop is modulated, and as a result, the fundamental wave component of the interference light on the light receiving surface of the optical detector 4 is given by the following equation. .゛S, = ΩJ+(η) cos ω11 (t-4(
T+ +Tz) )・−・−・−−−−1・−・・−
・−・−・−・−−−−−−−−・・・−(1) Here, K is a constant, J, and (η) are the above-mentioned 1st order 1st type Be5sel
It is a function.

(1)式に於いて η=2asin÷(↑+−Tt)ω。(1) In equation η=2asin÷(↑+−Tt)ω.

−2asin  (gf、T) である。-2asin (gf, T) It is.

ここでf、は位相変調の変調周波数、aは変調の振幅、
Tは光ファイバループの光伝播時間である。
Here, f is the modulation frequency of phase modulation, a is the amplitude of modulation,
T is the optical propagation time in the optical fiber loop.

光ディテクタ4の出力を同期検波する事によりΔφ即ち
角速度Ωに比例した出力が得られ、特に角速度の小さい
場合であっても検出可能のものであることが理解される
It is understood that by synchronously detecting the output of the optical detector 4, an output proportional to Δφ, that is, the angular velocity Ω, is obtained, and that detection is possible even when the angular velocity is particularly small.

但しJ+(0)=OなのでT、≠T8となるように変調
点を光ファイバの中心からずらしておく事が必要である
However, since J+(0)=O, it is necessary to shift the modulation point from the center of the optical fiber so that T,≠T8.

従ってこの方法では微小角速度の検出は可能であるが、
変調点以外では光ファイバ中央から等距離にある部分が
同時に同一のノイズ原因を発生した時にはそのノイズは
キャンセルするがそれ以外ではそのままノイズが出力信
号に現れてしまうという欠点を有する。
Therefore, although it is possible to detect minute angular velocities with this method,
If the same noise source occurs at the same time in parts other than the modulation point that are equidistant from the center of the optical fiber, the noise is canceled, but otherwise the noise appears as it is in the output signal.

ところで、ノイズは光ファイバに加わる局部的な温度変
化等による局部的な伸びやストレス等が原因で発生する
。即ち T、≠TzO点でノイズが生じるのが一般的で
あり、その場合はノイズが出力信号中に含まれてしまう
、即ち、この構成によると光ファイバループ自体の温度
変化等による局部的伸縮を補償不能である為結局のとこ
ろ高精度の測定が出来ないと言う問題点があった。
Incidentally, noise is generated due to local elongation, stress, etc. due to local temperature changes applied to the optical fiber. In other words, noise generally occurs at the point T, ≠ TzO, and in that case, the noise is included in the output signal.In other words, this configuration prevents local expansion and contraction due to temperature changes in the optical fiber loop itself. Since compensation is impossible, there is a problem in that highly accurate measurements cannot be made after all.

(発明の目的) 本発明は以上の欠点を解決し、簡単な構成により光ファ
イバループに局部的に加わる温度変化による局部的な光
ファイバループの伸縮や局部的に加わるストレス等に起
因する測定誤差の補正が可能で測定精度の高い光ファイ
バジャイロを得る事を目的とする。
(Objective of the Invention) The present invention solves the above-mentioned drawbacks and uses a simple configuration to prevent measurement errors caused by local expansion and contraction of the optical fiber loop due to temperature changes locally applied to the optical fiber loop, stress applied locally, etc. The purpose of this study is to obtain an optical fiber gyro that is capable of correction and has high measurement accuracy.

(発明の概要) 本発明は光ファイバジャイロにおいて、位相変調法によ
る場合光ファイバの全長の蚤の点(中央部)から同一の
距離にある2つの点に同一のノイズ発生原因が加わって
も該ノイズはキャンセルされて出力には現れないという
性質に着目し、一本の光ファイバの中央から互いに等距
離にある光ファイバ部分が近接する様全体として一方向
に巻回したとを技術的要点としている。
(Summary of the Invention) The present invention provides an optical fiber gyro that uses the phase modulation method even if the same noise generation source is applied to two points at the same distance from the flea point (center) of the entire length of the optical fiber. Focusing on the property that noise is canceled and does not appear in the output, the technical point is that the optical fiber is wound in one direction as a whole so that the optical fiber parts that are equidistant from the center of one optical fiber are close to each other. There is.

(実施例) 第1図は本発明の実施例で、光ファイバループをボビン
へ巻回する順序を(a)〜(d)に順に示す。
(Embodiment) FIG. 1 shows an embodiment of the present invention, in which (a) to (d) show the order in which an optical fiber loop is wound around a bobbin.

第1図において、11はボビン、12は光ファイバであ
る。
In FIG. 1, 11 is a bobbin, and 12 is an optical fiber.

光ファイバの一端を12a、他端を12b、中央部を1
2C、ボビンの一端部を11a、他端部を11bとする
と、 光ファイバループの巻き方は、以下の順序で行われる。
One end of the optical fiber is 12a, the other end is 12b, and the center part is 12a.
2C, one end of the bobbin is 11a, and the other end is 11b.The optical fiber loop is wound in the following order.

第1図(a)・−・・・−−一−−・−前記光ファイバ
の中央部12Cをボビン11の一端部11aに固定し、
光ファイバの一端12aをボビン11の一端部11aか
ら他端部11b迄詰めて巻回し、 第1図(b) (c)−・−・・・・・・−・次に光フ
ァイバの他端12bをその上に前記巻回方向と逆方向に
ボビン11の一端部11aから他端部11b迄詰めて巻
回する。
FIG. 1(a) - - - - - - Fixing the central part 12C of the optical fiber to one end 11a of the bobbin 11,
One end 12a of the optical fiber is packed and wound from one end 11a of the bobbin 11 to the other end 11b, and then the other end of the optical fiber is wound. 12b is packed and wound thereon from one end 11a to the other end 11b of the bobbin 11 in the opposite direction to the winding direction.

ここで、光ファイバの巻回方向は前述の通り光ファイバ
の各端12a、12bを巻回するときは反対方向に巻回
するが、光ファイバ全体としては結局同一方向となるよ
うに巻回する。
Here, the winding direction of the optical fiber is as described above, when each end 12a, 12b of the optical fiber is wound, it is wound in the opposite direction, but the optical fiber as a whole is wound in the same direction after all. .

第1図(d ) −・・−・−・次に光ファイバの一端
12aを第3層目としてボビン11の他端部11bから
一端部11a迄詰めて巻回し、 さらに光ファイバの他端12bを同様に第411目とし
てボビン11の他端部11bから一端部11a迄詰めて
巻回する。′ 尚ここで、光ファイバを巻回した後シリコン樹脂等を充
填すると、外部からの温度変化や力による光ファイバの
歪が原因となって発生するノイズを軽減する事が出来る
FIG. 1(d) --- Next, one end 12a of the optical fiber is wound as the third layer from the other end 11b of the bobbin 11 to the one end 11a, and then the other end 12b of the optical fiber is wound. Similarly, as the 411th stitch, the bobbin 11 is wound from the other end 11b to the one end 11a. ' Note that if the optical fiber is filled with silicone resin or the like after being wound, noise generated due to distortion of the optical fiber due to external temperature changes or forces can be reduced.

更に光ファイバとして金属コートしたものを使用し、ボ
ビン11に巻回しおわった後、半田等で光ファイバどう
しを接触させておけば局部的に加わる温度変化による光
ファイバの歪は軽減されノイズの発生を軽減する事が出
来る。
Furthermore, if the optical fibers are coated with metal and the optical fibers are brought into contact with each other with solder or the like after being wound around the bobbin 11, the distortion of the optical fibers due to locally applied temperature changes will be reduced and the generation of noise will be reduced. can be reduced.

第2図は本発明の他の実施例である。FIG. 2 shows another embodiment of the invention.

本実施例では前記光ファイバの中央部12Cをボビン1
1の一端部11aに固定し、光ファイバの一端12aを
ボビン11の一端部11aから他端部11b迄詰めずに
隙間を設けて巻回する。
In this embodiment, the central portion 12C of the optical fiber is connected to the bobbin 1.
1, and one end 12a of the optical fiber is wound from the one end 11a of the bobbin 11 to the other end 11b with a gap provided without crowding.

次に光ファイバの他端12bをその上に前記巻回方向と
逆方向にボビン11の一端部11aから他端部11b迄
光ファイバの一端12aの巻回した隙間に巻回する。
Next, the other end 12b of the optical fiber is wound thereon in the opposite direction to the winding direction from one end 11a of the bobbin 11 to the other end 11b in the gap where the one end 12a of the optical fiber is wound.

ここで、光ファイバの巻回方向は前述の通り光ファイバ
の各端12a、12bを巻回するときは反対方向に巻回
するが、光ファイバ全体としては結局同一方向となるよ
うに巻回する事は前述の通りである。
Here, the winding direction of the optical fiber is as described above, when each end 12a, 12b of the optical fiber is wound, it is wound in the opposite direction, but the optical fiber as a whole is wound in the same direction after all. The matter is as described above.

(発明の効果) 本発明によれば、一本の光ファイバをその中央から等距
離の部分が近接する様に巻回するという簡単な構成によ
り、光ファイバに加わる局部的な温度変化等による光フ
ァイバの局部的な歪が原因で発生するノイズを除去する
事ができ、測定精度の高い光ファイバジャイロを得る事
が出来る。
(Effects of the Invention) According to the present invention, a simple structure in which a single optical fiber is wound so that the parts equidistant from the center are close to each other allows light to be absorbed by local temperature changes applied to the optical fiber. Noise caused by local distortion of the fiber can be removed, and an optical fiber gyro with high measurement accuracy can be obtained.

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

第1図、第2図は本発明の実施例を示す図、第3図は従
来の光ファイバジャイロを示す図である。 (主要部分の符号の説明) 1・−・・・−・−・光ファイバループ2・・−−−−
一−−・−・・光源部 3・・・−−−−−−−・ハーフミラ−4・−・−−−
−−−−一光ディテクタ11・−−−−−−−−・・・
ボビン 12・−・−・・光ファイバ
1 and 2 are diagrams showing an embodiment of the present invention, and FIG. 3 is a diagram showing a conventional optical fiber gyro. (Explanation of symbols of main parts) 1. --- Optical fiber loop 2. ---
1---・---・Light source section 3------・Half mirror 4・------
-----One light detector 11------------
Bobbin 12 --- Optical fiber

Claims (1)

【特許請求の範囲】 一本の光ファイバを中央を起点として一端側を一定方向
に巻回し、 他端側を反対方向に巻回することによって前記起点から
互いに等距離にある光ファイバ部分が近接した状態で光
ファイバ全体として同一巻回方向となる様巻回したこと
を特徴とする光ファイバジャイロ。
[Claims] By winding one end of a single optical fiber in a fixed direction with the center as a starting point and winding the other end in the opposite direction, optical fiber sections that are equidistant from the starting point are brought into close proximity. An optical fiber gyro characterized in that the optical fiber is wound in the same winding direction as a whole when the optical fiber is in the same state.
JP60068771A 1985-04-01 1985-04-01 Optical fiber gyro Pending JPS61226609A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP60068771A JPS61226609A (en) 1985-04-01 1985-04-01 Optical fiber gyro

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP60068771A JPS61226609A (en) 1985-04-01 1985-04-01 Optical fiber gyro

Publications (1)

Publication Number Publication Date
JPS61226609A true JPS61226609A (en) 1986-10-08

Family

ID=13383327

Family Applications (1)

Application Number Title Priority Date Filing Date
JP60068771A Pending JPS61226609A (en) 1985-04-01 1985-04-01 Optical fiber gyro

Country Status (1)

Country Link
JP (1) JPS61226609A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01305310A (en) * 1988-06-03 1989-12-08 Japan Aviation Electron Ind Ltd fiber optic coil
EP0488255A2 (en) * 1990-11-28 1992-06-03 Matsushita Electric Industrial Co., Ltd. Fiber-optic coil and method of manufacturing same
US5405485A (en) * 1994-01-14 1995-04-11 Litton Systems, Inc. Robotic fiber optic quadrupole coil winder
JP2010096761A (en) * 2008-10-14 2010-04-30 Honeywell Internatl Inc Bifilar optical fiber stowage for fiber-optic gyroscope

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01305310A (en) * 1988-06-03 1989-12-08 Japan Aviation Electron Ind Ltd fiber optic coil
EP0488255A2 (en) * 1990-11-28 1992-06-03 Matsushita Electric Industrial Co., Ltd. Fiber-optic coil and method of manufacturing same
US5405485A (en) * 1994-01-14 1995-04-11 Litton Systems, Inc. Robotic fiber optic quadrupole coil winder
JP2010096761A (en) * 2008-10-14 2010-04-30 Honeywell Internatl Inc Bifilar optical fiber stowage for fiber-optic gyroscope

Similar Documents

Publication Publication Date Title
JP2769924B2 (en) Optical fiber rotation sensor
KR900008266B1 (en) Solid state interferometor
JP5362180B2 (en) Asynchronous demodulation of fiber optic gyroscope
JPS6337212A (en) Method for reading rotational speed by passive optical resonator
EP0198081A1 (en) Fiber-optic rotation rate sensor having dual interferometer loops
JPH05508221A (en) Interferometer signal analysis with modulation switching
JPS61226609A (en) Optical fiber gyro
JPS61169714A (en) Optical fiber gyro
JPS62135719A (en) Method and device for measuring number of revolution by sagnac interferometer
JPH0350964B2 (en)
JPH04270914A (en) Synchronous detector
JPS63138208A (en) Optical fiber gyro by phase modulation system
JP2625608B2 (en) Navigation system
JPS6280512A (en) Optical fiber gyro
JPH05215558A (en) Synchronous wave detection system of optic fiber gyro
JP3271019B2 (en) Fiber optic gyro
JPS60140115A (en) Optical fiber rate sensor
JPH02189412A (en) Optical fiber gyroscope
JPH063155A (en) Fiber optic gyro
JPH0464411B2 (en)
JPH05288557A (en) Optical fiber gyroscope
JPS622121A (en) Optical fiber gyroscope
JPH05196470A (en) Optical fiber gyro
JPH02145911A (en) fiber optic gyro
JPH07128074A (en) Optical fiber gyro signal processing method