JPS6049216A - Angular velocity sensor - Google Patents

Angular velocity sensor

Info

Publication number
JPS6049216A
JPS6049216A JP58158236A JP15823683A JPS6049216A JP S6049216 A JPS6049216 A JP S6049216A JP 58158236 A JP58158236 A JP 58158236A JP 15823683 A JP15823683 A JP 15823683A JP S6049216 A JPS6049216 A JP S6049216A
Authority
JP
Japan
Prior art keywords
oscillation
angular velocity
prism
plane
offset
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
JP58158236A
Other languages
Japanese (ja)
Inventor
Shinichi Yuga
信一 柚賀
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.)
Jeco Corp
Original Assignee
Jeco 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 Jeco Corp filed Critical Jeco Corp
Priority to JP58158236A priority Critical patent/JPS6049216A/en
Publication of JPS6049216A publication Critical patent/JPS6049216A/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
    • G01C19/56Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces

Landscapes

  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Gyroscopes (AREA)

Abstract

PURPOSE:To reduce an offset and detect even a small angular velocity by fitting two piezoelectric elements to parallel oscillation surfaces of an oscillation body constituted so that Coriolis force is received, and mixing the output signals of the piezoelectric elements in in-phase relation. CONSTITUTION:An angular velocity sensor has a prism 1 as the oscillation body, and the prism 1 has the 1st surface, i.e. oscillation surface parallel to a surface containing X-X' and Y-Y' and the 2nd surface perpendicular to the 1st surface, i.e. oscillation surface parallel to a plane containing X-X' and Z-Z'. Then, the piezoelectric elements 2a, 2b, and 2c are fitted to the respective oscillation surfaces. The prism 1 is supported by supporting members 3a and 3b as nodal points of oscillation. This constitution reduces an offset and detects even a small angle.

Description

【発明の詳細な説明】 〔発明の技術分野〕 この発明社回転体等の角速度を検出する角速度センサに
関するものである。
DETAILED DESCRIPTION OF THE INVENTION [Technical Field of the Invention] This invention relates to an angular velocity sensor that detects the angular velocity of a rotating body or the like.

〔従来技術〕[Prior art]

従来から、コリオリの力を利用して角速度を検出する揚
動ジャイロが各釉提案されていた。これは第1図に示す
ような角柱1を例えばz−z’力方向振動させ、x−x
’向1周りに回転力を与えると角柱1はY−Y’力方向
振動成分が現われ、Y−Y’力方向振幅はx−x’軸周
りの角速度に比fullするものである。このため、Y
−Y’力方向振促1h゛を月1[へ素子力どで電気信号
に変撲すれば、角速度にダJ Ii:、、した信号が得
られる。
Lifting gyros that detect angular velocity using the Coriolis force have been proposed for various glazes. This is done by vibrating a prism 1 as shown in Fig. 1 in the z-z' force direction, for example, and
When a rotational force is applied around the 'direction 1, a vibration component in the Y-Y' force direction appears in the prism 1, and the amplitude in the Y-Y' force direction is fully proportional to the angular velocity around the x-x' axis. For this reason, Y
-Y' If the force direction vibration 1h is converted into an electric signal by an element force, a signal with an angular velocity of 1h can be obtained.

しかしながら、このような従来のセンサは圧’Jj。However, such conventional sensors are limited to pressure 'Jj.

素子から得られる信号の振幅が小さく、甘だ角柱1の長
手方向の各面の面積が略同−であるため振動モードが似
通っているので、x−x’輔周りの角速度が与えられな
い時でもY−Y’力方向振動成分が若干現われるオフセ
ット現象かう6生じてし−まう。
Since the amplitude of the signal obtained from the element is small and the area of each surface in the longitudinal direction of the amada prism 1 is approximately the same, the vibration modes are similar, so when the angular velocity around the x-x' axis is not given. However, an offset phenomenon occurs in which the Y-Y' force direction vibration component appears slightly.

このオフセットを小さくしようとして長手方向の面のう
ち、水平面と垂IG面の面tI’j比を変えろことも考
えられるが、このようにすると−力の「11の面積が小
さく在り、圧電素子の面積も小さくんって出力信号の大
きさが小さくなってし廿うという欠点を有していた。
In order to reduce this offset, it is possible to change the plane tI'j ratio of the horizontal plane and the vertical IG plane among the longitudinal planes, but if you do this, the area of force 11 will be small, and the piezoelectric element will Since the area is small, the size of the output signal is also small.

〔発明の目的および(τ・7成J したがってこの発明の目的に11、出カイ11号の犬た
さを減少きせることなくオフセットを減少させ7)こと
ができる角速度センサを提供することにある。
[Objectives of the Invention and (τ·7) Therefore, the object of the present invention is to provide an angular velocity sensor that can reduce the offset without reducing the stiffness of the output.

このように目的を達成するためにこの発す]は、圧電素
子を振動面の両側に取付け、それぞれの圧R,!子から
得られる(H号を同位相となるようにして合成したもの
である。す、下、実施例を・示す図imを用いてこの発
明を訂卸]に説明する。
In order to achieve this purpose, piezoelectric elements are installed on both sides of the vibrating surface, and the respective pressures R,! The present invention will be explained below using figures showing examples.

〔実施例〕〔Example〕

第2図はこの発明に用いる振動体の一実施例を示す余[
親図である4、同図において、振動体である角柱1は第
10向すなわちx−x’およびy−y’會含む面に平行
な振動面と、第1の面と直角外電2のi’ii」すなわ
ちX−X′およびz−z’を含む面に平イjな振動面を
有しており、各振動面にそれぞれ圧電素子2a + 2
b + 2c 、 2dが取付けられている。そして、
角柱1は振動の釧゛jになるノーダルポイントを支持部
材3a、3bで支持されている。力お、角柱1は導電性
を有する材料で形成されている。
FIG. 2 shows an embodiment of the vibrating body used in the present invention.
4, which is the parent diagram, the prism 1 which is the vibrating body has a vibrating plane parallel to the tenth direction, that is, the plane containing x-x' and y-y', and an i 'ii', that is, a plane including X-X' and z-z', has a flat vibration surface, and each vibration surface has a piezoelectric element 2a + 2
b + 2c, 2d are attached. and,
The square column 1 is supported by support members 3a and 3b at its nodal point, which becomes the point of vibration. The square column 1 is made of a conductive material.

第3 hはこの発明の一笑絶倒全〉jミす回路図であり
、4a、4bは抵抗、5は圧電索子2dの出力信号の位
相を反転させ圧電素子2cの出力信号と合成する信号合
成回路である演算増幅器、6は出力端子である。
3h is a circuit diagram of this invention, in which 4a and 4b are resistors, and 5 is a signal that inverts the phase of the output signal of the piezoelectric element 2d and combines it with the output signal of the piezoelectric element 2c. 6 is an output terminal of an operational amplifier which is a combining circuit.

このようにtl”)成された回路の1モノ1作は次の′
)+E+りである。圧電素子2a 、 2b間に角柱1
の共振周波数を有する信号を供給すると角柱1は第2図
のZ−2′ 方向に振動する。ここで、x−x’同周9
回転力が与えらtしると角柱1はコリオリの力を父けY
y/方向にも振動を始めるので、圧電素子2c、2dに
信号が発生する。この時、圧”jjj+素子2c 、 
2dに発生する45号の位相は互いに逆位相であり、圧
1)14累子2dに発生ずる信号は演3υ“帽・、4器
5で位相反転でれ圧電素子2cに発生した1、1号と合
成され、端子6に供給される。圧電素子2dに発生する
信号は演算増幅器5で位相反転され圧電素子2cに発生
する411号と同位相となるので両イ菖号は′11ε川
加算され振幅が6デシベル増加する0、 一方、オフセット信号はコリオリの力による正規の振動
でないため、その周波級成分は角柱1の共振周波数だけ
でなく、その茜調波および低調波を含んでいるので、圧
電素子2c、2dK発生するオフセット信号の位相は互
いに相関性がない。こ 、のため、演算増幅器5で信号
合成した時、電力加算され3デシベルの増加となる。し
たがって端子6から送出される信号のS/Nは3デシベ
ル向上し、オフセットが減少したことになる。
Each circuit created in this way is as follows'
)+E+ri. A square column 1 is placed between the piezoelectric elements 2a and 2b.
When a signal having a resonant frequency is supplied, the prism 1 vibrates in the Z-2' direction in FIG. Here, x-x' same circumference 9
When a rotational force is applied t, the prism 1 exerts a Coriolis force Y
Since vibration also begins in the y/direction, signals are generated in the piezoelectric elements 2c and 2d. At this time, the pressure "jjj + element 2c,
The phases of No. 45 generated at piezoelectric element 2d are opposite to each other, and the signal generated at piezoelectric element 2d is inverted in phase by the piezoelectric element 2c. The signal generated at the piezoelectric element 2d is phase-inverted by the operational amplifier 5 and has the same phase as the signal 411 generated at the piezoelectric element 2c, so both the A signal and the signal are combined with the '11ε river summation. On the other hand, since the offset signal is not a regular vibration due to the Coriolis force, its frequency component includes not only the resonance frequency of the prism 1 but also its madder harmonics and subharmonics. The phases of the offset signals generated by the piezoelectric elements 2c and 2dK have no correlation with each other. Therefore, when the signals are combined by the operational amplifier 5, the power is added and the offset signal increases by 3 decibels. This means that the S/N ratio of the signal has improved by 3 decibels, and the offset has decreased.

以上の実施例は振動体として角柱を用いているが、これ
は互いに直交する振動面を有する振動体が剛体で結合さ
れていれば良いので、第4図〜7図に示すように2つの
U字状音叉が剛体で結合されるものであっても良い。こ
こで、第4図は正面図、第5図は平面図、第6図は左側
面図、第7図は右側面図であり、7a、7bは音叉、8
a、8bicl:支持部材である。
In the above embodiments, a rectangular column is used as the vibrating body, but since it suffices if the vibrating bodies having vibrating surfaces perpendicular to each other are connected by a rigid body, two U The character-shaped tuning fork may be connected by a rigid body. Here, Fig. 4 is a front view, Fig. 5 is a plan view, Fig. 6 is a left side view, and Fig. 7 is a right side view.
a, 8bicl: Supporting member.

〔発明の効果〕〔Effect of the invention〕

以上説明したようにこの発明に係る角速度センサは、コ
リオリの力を受けるように構成された振動体の平行な振
動面に取付けられた2つの庄Ttt ’j+<子の出力
信号が同位相になるようにして加えあわせたので、オフ
セットが減少し、小さな角速度寸で検出できるようにな
るという効果を有り々。
As explained above, in the angular velocity sensor according to the present invention, the output signals of the two sensors attached to the parallel vibration surfaces of the vibrating body configured to receive the Coriolis force are in phase. By adding them together in this way, the offset is reduced and detection can be performed with a small angular velocity, which has the effect of reducing the offset.

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

第1図は振動ジャイロの振動体を示す斜視図、第2図は
この発明に用いられる振動体に圧霜:素子を取伺けた状
態を示す斜視図、第3図はこの発明の一実施例を示す回
路図、第4図〜第7図は振ル;1体の他の実施例であり
、第4図は正面図、第5し1は平面図、第6図は左側面
図、第7図は右側面図である。 11111@参角柱、28〜2d11e−・圧電素子、
3a、3b * @ @ ”支持部材、4a、4b a
 * @ *抵抗、5・・・・演算増幅器、6ψ・・・
出力端子。 特許出願人 ジエコー(ニ(、式会社 代理人 山川政情(ほか1名)
Fig. 1 is a perspective view showing the vibrating body of a vibrating gyroscope, Fig. 2 is a perspective view showing the vibrating body used in this invention in a state in which a compressed frost element can be seen, and Fig. 3 is an embodiment of the present invention. Figures 4 to 7 are circuit diagrams showing other embodiments of the unit. Figure 4 is a front view, Figure 5 is a plan view, Figure 6 is a left side view, and Figure 6 is a left side view. Figure 7 is a right side view. 11111@Reference prism, 28~2d11e-・Piezoelectric element,
3a, 3b * @ @ ”Support member, 4a, 4b a
* @ *Resistor, 5... operational amplifier, 6ψ...
Output terminal. Patent applicant: Jieko (2), company agent: Seijo Yamakawa (and 1 other person)

Claims (1)

【特許請求の範囲】[Claims] 第1の面に平行々振動面と第1の面に直角な第2の面に
平行な振?VilJ面とを有する振動体と、各振動面に
取付けられた圧電素子と、第1または第2の面のいずれ
か一方の面と平行な圧電素子のうち一方の圧電素子から
得られる信号を位相反転させ他方の圧1わ:素子から得
られる信号と合成する(H+号合成回路とを備えた角速
度センサ。
A vibration plane parallel to the first plane and a vibration plane parallel to the second plane perpendicular to the first plane? A vibrating body having a VilJ plane, a piezoelectric element attached to each vibrating plane, and a signal obtained from one of the piezoelectric elements parallel to either the first or second plane. The other pressure is inverted and combined with the signal obtained from the element (angular velocity sensor equipped with an H+ synthesis circuit).
JP58158236A 1983-08-30 1983-08-30 Angular velocity sensor Pending JPS6049216A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP58158236A JPS6049216A (en) 1983-08-30 1983-08-30 Angular velocity sensor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP58158236A JPS6049216A (en) 1983-08-30 1983-08-30 Angular velocity sensor

Publications (1)

Publication Number Publication Date
JPS6049216A true JPS6049216A (en) 1985-03-18

Family

ID=15667246

Family Applications (1)

Application Number Title Priority Date Filing Date
JP58158236A Pending JPS6049216A (en) 1983-08-30 1983-08-30 Angular velocity sensor

Country Status (1)

Country Link
JP (1) JPS6049216A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0430418U (en) * 1990-07-05 1992-03-11
EP0520468A2 (en) * 1991-06-26 1992-12-30 Murata Manufacturing Co., Ltd. Vibratory gyroscope
US5569969A (en) * 1988-08-12 1996-10-29 Murata Manufacturing Co., Ltd. Vibrator and vibratory gyroscope using the same
US6016698A (en) * 1988-08-12 2000-01-25 Murata Manufacturing Co., Ltd. Vibratory gyroscope including piezoelectric electrodes or detectors arranged to be non-parallel and non-perpendicular to coriolis force direction

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3520195A (en) * 1965-10-11 1970-07-14 Gen Electric Solid state angular velocity sensing device
JPS54153970A (en) * 1978-05-22 1979-12-04 Gen Motors Corp Vibrative rotation senser

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3520195A (en) * 1965-10-11 1970-07-14 Gen Electric Solid state angular velocity sensing device
JPS54153970A (en) * 1978-05-22 1979-12-04 Gen Motors Corp Vibrative rotation senser

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5569969A (en) * 1988-08-12 1996-10-29 Murata Manufacturing Co., Ltd. Vibrator and vibratory gyroscope using the same
US6016698A (en) * 1988-08-12 2000-01-25 Murata Manufacturing Co., Ltd. Vibratory gyroscope including piezoelectric electrodes or detectors arranged to be non-parallel and non-perpendicular to coriolis force direction
US6016699A (en) * 1988-08-12 2000-01-25 Murata Manufacturing Co., Ltd. Vibrator including piezoelectric electrodes of detectors arranged to be non-parallel and non-perpendicular to Coriolis force direction and vibratory gyroscope using the same
US6161432A (en) * 1988-08-12 2000-12-19 Murata Manufacturing Co., Ltd. Vibrator and vibratory gyroscope using the same
JPH0430418U (en) * 1990-07-05 1992-03-11
EP0520468A2 (en) * 1991-06-26 1992-12-30 Murata Manufacturing Co., Ltd. Vibratory gyroscope

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