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JPH08201060A - Geomagnetic azimuth meter - Google Patents

Geomagnetic azimuth meter

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Publication number
JPH08201060A
JPH08201060A JP1009795A JP1009795A JPH08201060A JP H08201060 A JPH08201060 A JP H08201060A JP 1009795 A JP1009795 A JP 1009795A JP 1009795 A JP1009795 A JP 1009795A JP H08201060 A JPH08201060 A JP H08201060A
Authority
JP
Japan
Prior art keywords
magnetic field
axis
geomagnetic
detected
field strength
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
JP1009795A
Other languages
Japanese (ja)
Inventor
Manabu Aizawa
学 相澤
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.)
Sony Corp
Original Assignee
Sony 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 Sony Corp filed Critical Sony Corp
Priority to JP1009795A priority Critical patent/JPH08201060A/en
Publication of JPH08201060A publication Critical patent/JPH08201060A/en
Pending legal-status Critical Current

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  • Geophysics And Detection Of Objects (AREA)
  • Measuring Magnetic Variables (AREA)

Abstract

PURPOSE: To enhance accuracy and reliability in the measurement by detecting the geomagnetic azimuth angle in one arbitrary direction based on the phase angle of a rotating field where the strength of combined field of rotating field and geomagnetic field, detected by means of a field strength sensor, has a maximal or minimal absolute value. CONSTITUTION: X-axis coils 3, 4 and Y-axis coils 1, 2 are arranged symmetricaliy to YZ and XZ planes, respectively, while aligning the central axes with the X-axis and Y-axis. The coils 3, 4 and 1, 2 are connected, respectively, in series and fed with AC currents IX=cosϕ and IY=sinϕ from AC current sources 10, 9 to induce fields HX, HY proportional to the currents IX, IY in the directions of X-axis and Y-axis. Output from a field strength sensor 5 is then fed to a maximal value (minimal value) detector and the phase angle ϕof rotating field having maximal value (minimal value), the waveform of the current IX, IY or the instantaneous level of the current is detected by a level detector. Finally, the detection level is subjected to inverse cosine or sine transform thus detecting the azimuth angle ϕ (ϕ-180 deg.) of geomagnetism.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は地磁気方位計に関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a geomagnetic compass.

【0002】[0002]

【従来の技術】図5を参照して、従来の地磁気方位計に
ついて説明する。15は地磁気方位センサで、ある方向
及びこれと90°異なる方向の地磁気を検知する1対の
センサから構成される。HE は地磁気の水平分力を示
し、水平面(紙面)内にXY直交座標系を想定し、ある
方向をY軸方向、それと90°異なる方向をX軸方向と
する。かくすると、地磁気の方位角をY軸方向に対しθ
°とすると、地磁気方位センサ15から検出出力電圧で
あるcos θとsin θの2つの出力が得られ、これがA/
D変換器16、17に供給されてデジタル電圧に変換さ
れた後、コンピュータ18に供給されて、
2. Description of the Related Art A conventional geomagnetic compass will be described with reference to FIG. Reference numeral 15 denotes a geomagnetic direction sensor, which is composed of a pair of sensors that detect geomagnetism in a certain direction and a direction different from this by 90 °. H E represents the horizontal component force of the earth's magnetism, assuming an XY orthogonal coordinate system in the horizontal plane (paper surface), and a certain direction is the Y-axis direction and a direction different from it by 90 ° is the X-axis direction. Thus, the azimuth angle of the geomagnetism is θ with respect to the Y-axis direction.
If the angle is °, two outputs of the detected output voltage, cos θ and sin θ, are obtained from the geomagnetic direction sensor 15.
After being supplied to the D converters 16 and 17 and converted into a digital voltage, it is supplied to the computer 18,

【0003】[0003]

【数1】 [Equation 1]

【0004】によるデジタル演算が行われて、方位角θ
が検出される。
Azimuth angle θ
Is detected.

【0005】[0005]

【発明が解決しようとする課題】かかる従来の地磁気方
位計には次のような欠点がある。地磁気方位センサ15
のある方向及びこれと90°異なる方向の地磁気を検知
する1対のセンサの特性が揃っていない場合は、一対の
センサの検出出力電圧を一般的に、A1 sin θ+B1
2 cos θ+B2 とすると、これら係数A1 、A2 、B
1 、B2 間においては、処理回路におけるノイズの発
生、温度ドリフト等によって、A1 ≠A2 若しくはB1
≠B2 又はA1 ≠A2 且つB1 ≠B2 となり、地磁気方
位を正確に測定することはできなくなる。上述の数1の
演算を行うために、A/D変換器や、コンピュータを必
要とし、地磁気方位計の構成が複雑となると共に、価格
の上昇を招来する。地磁気方位センサ15の一対のセン
サの特性が上述のように揃っていない場合には、係数A
1 、A2 、B1 、B2 間において、A1 =A2 又は/及
びB1 =B2 にするための補正手段を必要とするため、
一層地磁気方位計の構造が複雑となり、価格の上昇を招
来する。地磁気方位の検出精度を一層高くするために
は、地磁気方位センサ15の一対のセンサから検出出力
電圧をダイナッミックに補正する必要があるが、その場
合には、一層複雑高価な補正手段を必要とし、更に一層
地磁気方位計の構造が複雑となり、価格の上昇を招来す
る。
The conventional geomagnetic compass as described above has the following drawbacks. Geomagnetic direction sensor 15
If the characteristics of a pair of sensors that detect the earth's magnetism in a certain direction and a direction different from this by 90 ° are not uniform, the detection output voltage of the pair of sensors is generally A 1 sin θ + B 1 ,
Assuming A 2 cos θ + B 2 , these coefficients A 1 , A 2 , B
Between 1 and B 2 , A 1 ≠ A 2 or B 1 due to noise generation in the processing circuit, temperature drift, etc.
Since ≠ B 2 or A 1 ≠ A 2 and B 1 ≠ B 2 , the geomagnetic azimuth cannot be accurately measured. An A / D converter and a computer are required to perform the calculation of the above-described mathematical expression 1, the configuration of the geomagnetic compass is complicated, and the price is increased. When the characteristics of the pair of sensors of the geomagnetic direction sensor 15 are not uniform as described above, the coefficient A
Since correction means for A 1 = A 2 and / or B 1 = B 2 between 1 , A 2 , B 1 , and B 2 is required,
The structure of the geomagnetic compass will become more complicated, leading to higher prices. In order to further improve the detection accuracy of the geomagnetic direction, it is necessary to dynamically correct the detection output voltage from the pair of sensors of the geomagnetic direction sensor 15, but in that case, more complicated and expensive correction means is required, Furthermore, the structure of the geomagnetic compass becomes more complicated, leading to an increase in price.

【0006】かかる点に鑑み、本発明は、構成が簡単
で、処理回路におけるノイズの発生や温度ドリフトの影
響を受けることなく、測定精度が高く、信頼性の高い地
磁気方位計を提案しようとするものである。
In view of the above point, the present invention intends to propose a geomagnetic compass with a simple structure, high measurement accuracy and high reliability without being affected by noise and temperature drift in the processing circuit. It is a thing.

【0007】[0007]

【課題を解決するための手段】本発明は、回転磁界発生
手段と、その回転磁界発生手段の中心に配された任意の
1方向の磁界強度を検知する磁界強度センサとを有し、
その磁界強度センサによって、回転磁界発生手段による
回転磁界及び地磁気の合成磁界の磁界強度を検知し、そ
の検知された合成磁界の磁界強度の絶対値が極大値又は
極小値になったときの回転磁界の位相角から、任意の1
方向に対する地磁気方位角を検知するようにしたことを
特徴とする地磁気方位計である。
The present invention has a rotating magnetic field generating means and a magnetic field strength sensor arranged at the center of the rotating magnetic field generating means for detecting magnetic field strength in any one direction.
The magnetic field strength sensor detects the magnetic field strength of the combined magnetic field of the rotating magnetic field and the geomagnetism by the rotating magnetic field generating means, and the rotating magnetic field when the absolute value of the detected magnetic field strength of the combined magnetic field reaches the maximum value or the minimum value. Any 1 from the phase angle of
A geomagnetic azimuth meter characterized by detecting a geomagnetic azimuth angle with respect to a direction.

【0008】[0008]

【作用】かかる本発明によれば、磁界強度センサによっ
て、回転磁界発生手段による回転磁界及び地磁気の合成
磁界の磁界強度を検知し、その検知された合成磁界の磁
界強度の絶対値が極大値又は極小値になったときの回転
磁界の位相角から、任意の1方向に対する地磁気方位角
を検知する。
According to the present invention, the magnetic field strength sensor detects the magnetic field strength of the combined magnetic field of the rotating magnetic field and the earth magnetism by the rotating magnetic field generation means, and the absolute value of the detected magnetic field strength of the combined magnetic field is the maximum value or The geomagnetic azimuth angle with respect to any one direction is detected from the phase angle of the rotating magnetic field when it reaches the minimum value.

【0009】[0009]

【実施例】以下に、図3を参照して、本発明の実施例を
詳細に説明する。紙面内にX、Y軸を有し、紙面に垂直
な方向にZ軸を有する直交座標系を仮定する。そして、
YZ平面に対し面対称に配され、中心軸がX軸と一致す
る円筒状、正方形筒状等のX軸コイル3、4と、XZ平
面に対し面対称に配され、中心軸がY軸と一致する円筒
状、正方形筒状等のY軸コイル1、2とを設ける。そし
て、XY平面上への投影像において、コイル1、2、
3、4が正方形の各辺を略構成するように配される。
Embodiments of the present invention will be described in detail below with reference to FIG. Assume an orthogonal coordinate system having X and Y axes in the plane of the paper and Z axis in the direction perpendicular to the plane of the paper. And
Cylindrical, square tubular, etc. X-axis coils 3 and 4 which are arranged plane-symmetrically with respect to the YZ plane and whose central axis coincides with the X-axis, and are arranged symmetrically with respect to the XZ plane, and whose central axis is the Y-axis. The corresponding Y-axis coils 1 and 2 having a cylindrical shape, a square cylindrical shape, or the like are provided. Then, in the projected image on the XY plane, the coils 1, 2,
3, 4 are arranged so as to substantially form each side of the square.

【0010】そして、X軸コイル3、4を直列接続し
て、その直列回路に交流電流源10を接続して交流電流
X = sinφを流して、その交流電流IX に比例したX
軸方向に一様な磁界HX を発生させる。又、Y軸コイル
1、2を直列接続して、その直列回路に交流電流源9を
接続して交流電流IY = cosφを流して、その直流電流
Y に比例したY軸方向に一様な磁界HY を発生させ
る。Hrotateは、磁界HX及びHY の合成磁界(回転磁
界)を示す。6、7及び8は、それぞれ磁界HX 、HY
及びの合成磁界Hrotateのベクトルを示す。かくする
と、磁界HX 、HY はそれぞれ次式のように表される。
Then, the X-axis coils 3 and 4 are connected in series, an AC current source 10 is connected to the series circuit, an AC current I X = sinφ is passed, and an X proportional to the AC current I X is applied.
Generating a uniform magnetic field H X in the axial direction. Further, the Y-axis coils 1 and 2 are connected in series, an AC current source 9 is connected to the series circuit, an AC current I Y = cos φ is passed, and it is uniform in the Y-axis direction proportional to the DC current I Y. A strong magnetic field H Y. H rotate indicates a composite magnetic field (rotating magnetic field) of the magnetic fields H X and H Y. 6, 7 and 8 are the magnetic fields H X and H Y , respectively.
The vector of the combined magnetic field H rotate of and is shown. Thus, the magnetic fields H X and H Y are respectively expressed by the following equations.

【0011】[0011]

【数2】 [Equation 2]

【0012】[0012]

【数3】 (Equation 3)

【0013】XYZ直交座標系の原点の磁界H
rotateは、磁界HX 、HY がベクトル合成されたもの
で、次式にように表される。
Magnetic field H at the origin of the XYZ rectangular coordinate system
The rotate is a vector combination of the magnetic fields H X and H Y, and is expressed by the following equation.

【0014】[0014]

【数4】 [Equation 4]

【0015】この磁界Hrotateは、これはHX 、HY
関数であり、磁界の強度が一定で位相角が0°〜360
°の範囲で連続的に変化する回転磁界である。
This magnetic field H rotate is a function of H X and H Y , and the magnetic field strength is constant and the phase angle is 0 ° to 360 °.
It is a rotating magnetic field that continuously changes in the range of °.

【0016】図3におけるXYZ直交座標系のXY平面
を水平面に一致させ、地磁気の水平分力の影響を考え
る。即ち、図2に示すように、XY平面内において、地
磁気の水平分力をHE にて示す。12はその磁界HE
ベクトルを示す。この地磁気の水平分力HE を水平及び
垂直成分HEX、HEYにベクトル分解すると、次式のよう
に表される。
Consider the influence of the horizontal component force of the earth's magnetism by matching the XY plane of the XYZ orthogonal coordinate system in FIG. 3 with the horizontal plane. That is, as shown in FIG. 2, the horizontal component force of geomagnetism is indicated by H E in the XY plane. 12 indicates the vector of the magnetic field H E. When the horizontal component force H E of this geomagnetism is vector- divided into horizontal and vertical components H EX and H EY , it is expressed by the following equation.

【0017】[0017]

【数5】 (Equation 5)

【0018】[0018]

【数6】 (Equation 6)

【0019】かくすると、XYZ直角座標の原点でのX
Y平面内における磁界Hは、回転磁界Hrotateと地磁気
の水平分力HE のベクトル合成されたものとなるので、
次式に示すように表される。
Thus, X at the origin of the XYZ rectangular coordinates
The magnetic field H in the Y plane is a vector combination of the rotating magnetic field H rotate and the horizontal component H E of the earth's magnetism.
It is expressed as shown in the following equation.

【0020】[0020]

【数7】 (Equation 7)

【0021】この合成磁界Hは回転磁界Hrotateの回転
に応じて同方向に回転する。この合成磁界Hの強度の絶
対値は次式のように表される。
The composite magnetic field H rotates in the same direction as the rotating magnetic field H rotate rotates. The absolute value of the intensity of this synthetic magnetic field H is expressed by the following equation.

【0022】[0022]

【数8】 (Equation 8)

【0023】地磁気HE の+X軸方向に対する地磁気の
水平分力の方位角をθとし、回転磁界Hrotateの位相角
φを+X軸からの角度とする。X軸コイル3、4及びY
軸コイル1、2に流れる電流IX、IYは、図1
(a)、(b)に示す如く、90°だけ位相の異なる波
形を呈する。図1(c)に回転磁界Hrotateの位相角φ
の特性を示し、この位相角φは0°〜360°の範囲で
変化する。図1(d)に合成磁界Hの絶対値|H|の特
性を示す。
The azimuth angle of the horizontal component force of the geomagnetism with respect to the + X axis direction of the geomagnetism H E is θ, and the phase angle φ of the rotating magnetic field H rotate is the angle from the + X axis. X-axis coils 3, 4 and Y
Currents IX and IY flowing through the shaft coils 1 and 2 are as shown in FIG.
As shown in (a) and (b), the waveforms exhibit different phases by 90 °. FIG. 1C shows the phase angle φ of the rotating magnetic field H rotate.
The phase angle φ changes in the range of 0 ° to 360 °. FIG. 1D shows the characteristic of the absolute value | H | of the synthetic magnetic field H.

【0024】この図1(d)のグラフから、合成磁界強
度|H|が極大値となるのは、φ=θのときであり、極
小値となるのは、φ=θ+180°のときであることが
分かる。従って、合成磁界強度|H|がそれぞれ極大値
及び極小値となったときの位相角φがそれぞれ地磁気の
方位角θ及びθ−180°であることが分かる。
From the graph of FIG. 1D, the combined magnetic field strength | H | has a maximum value when φ = θ, and a minimum value when φ = θ + 180 °. I understand. Therefore, it can be seen that the phase angles φ when the combined magnetic field strength | H | has the maximum value and the minimum value, respectively, are the azimuth angles θ and θ-180 ° of the geomagnetism.

【0025】そして、磁界強度センサ5からの出力を、
例えば、極大値検出器(又は極小値検出器)に供給し、
極大値(又は極小値)が検出されたら、そのときの位相
角φを、X軸コイル電流IX又はY軸コイル電流IYの
波形を見るか、又は、その電流の瞬時レベルをレベル検
出器によって検出し、その検出レベルをコサイン逆変換
又はサイン逆変換することによって、地磁気の方位角θ
(又はθ−180°)を検出することができる。
The output from the magnetic field strength sensor 5 is
For example, supplying the maximum value detector (or the minimum value detector),
When the maximum value (or minimum value) is detected, the phase angle φ at that time is checked by looking at the waveform of the X-axis coil current IX or the Y-axis coil current IY, or the instantaneous level of the current is detected by a level detector. Then, the azimuth angle of the geomagnetism θ
(Or θ-180 °) can be detected.

【0026】次に、回転磁界Hrotate及び地磁気HE
比Hrotate/HE をηと置き、η=0.5、1、2のと
きの、位相角φの変化に対する合成磁界強度|H|の極
小値付近のグラフを図4に示す。これによれば、η=1
のときに合成磁界強度|H|は0となり、しかも、その
0付近の特性は急峻となる。η=0.5、2のときは、
極小値は0より大となり、その極小値付近の特性は緩慢
となる。従って、回転磁界Hrotateの強度を、地磁気H
E の水平分力の強度と等しくなるように設定し、磁界強
度センサ5よりの磁界強度検出出力を、例えば、レベル
検出器に供給することにより、レベルが0になったこと
を高S/Nを以て検知することができる。そして、その
レベルが0になったことが検出されたら、そのときの位
相角φを、X軸コイル電流IX又はY軸コイル電流IY
の波形を見るか、又は、その電流の瞬時レベルをレベル
検出器によって検出し、その検出レベルをコサイン逆変
換又はサイン逆変換することによって、地磁気の方位角
θに関する角度(θ−180°)を検出することができ
る。
Next, the ratio H rotate / H E of the rotating magnetic field H rotate and the geomagnetism H E is set to η, and when η = 0.5, 1, 2 the combined magnetic field strength | H for changes in the phase angle φ A graph around the minimum value of | is shown in FIG. According to this, η = 1
At that time, the combined magnetic field strength | H | becomes 0, and the characteristics near 0 become steep. When η = 0.5 and 2,
The minimum value becomes larger than 0, and the characteristic near the minimum value becomes slow. Therefore, the strength of the rotating magnetic field H rotate is
It is set to be equal to the strength of the horizontal component force of E , and the magnetic field strength detection output from the magnetic field strength sensor 5 is supplied to, for example, a level detector so that the level becomes 0. Can be detected. Then, when it is detected that the level becomes 0, the phase angle φ at that time is set to the X-axis coil current IX or the Y-axis coil current IY.
Or the instantaneous level of the current is detected by a level detector, and the detected level is subjected to cosine inverse conversion or sine inverse conversion to determine the angle (θ-180 °) with respect to the azimuth θ of the geomagnetism. Can be detected.

【0027】[0027]

【発明の効果】上述せる本発明によれば、回転磁界発生
手段と、その回転磁界発生手段の中心に配された任意の
1方向の磁界強度を検知する磁界強度センサとを有し、
その磁界強度センサによって、回転磁界発生手段による
回転磁界及び地磁気の合成磁界の磁界強度を検知し、そ
の検知された合成磁界の磁界強度の絶対値が極大値又は
極小値のときの回転磁界の位相角から、任意の1方向に
対する地磁気方位角を検知するようにしたので、構成が
簡単で、処理回路におけるノイズの発生や温度ドリフト
の影響を受けることなく、測定精度が高く、信頼性の高
い地磁気方位計を得ることができる。
According to the present invention described above, it has a rotating magnetic field generating means and a magnetic field strength sensor arranged at the center of the rotating magnetic field generating means for detecting the magnetic field strength in any one direction.
The magnetic field strength sensor detects the magnetic field strength of the combined magnetic field of the rotating magnetic field and the geomagnetism by the rotating magnetic field generation means, and the phase of the rotating magnetic field when the absolute value of the detected magnetic field strength of the combined magnetic field is the maximum value or the minimum value. Since the geomagnetic azimuth angle with respect to any one direction is detected from the angle, the configuration is simple, and the measurement accuracy is high and the geomagnetism is highly reliable without being affected by noise or temperature drift in the processing circuit. You can get a compass.

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

【図1】実施例の動作説明に供するタイミングチャート
である。 (a) X軸コイル電流 (b) Y軸コイル電流 (c) 回転磁界位相角 (d) 合成磁界強度
FIG. 1 is a timing chart used for explaining the operation of an embodiment. (A) X-axis coil current (b) Y-axis coil current (c) Rotating magnetic field phase angle (d) Composite magnetic field strength

【図2】磁界の説明図である。FIG. 2 is an explanatory diagram of a magnetic field.

【図3】本発明の実施例の地磁気方位計を示す回路図で
ある。
FIG. 3 is a circuit diagram showing a geomagnetic compass according to an embodiment of the present invention.

【図4】合成磁界の強度の特性曲線図である。FIG. 4 is a characteristic curve diagram of the strength of a synthetic magnetic field.

【図5】従来礼のの地磁気方位計を示すブロック線図で
ある。
FIG. 5 is a block diagram showing a conventional geomagnetic compass.

【符号の説明】[Explanation of symbols]

1〜4 回転磁界発生用コイル 5 磁界強度センサ 9 励磁電流源 10 励磁電流源 1 to 4 rotating magnetic field generating coil 5 magnetic field intensity sensor 9 exciting current source 10 exciting current source

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 回転磁界発生手段と、 該回転磁界発生手段の中心に配された任意の1方向の磁
界強度を検知する磁界強度センサとを有し、 該磁界強度センサによって、上記回転磁界発生手段によ
る回転磁界及び地磁気の合成磁界の磁界強度を検知し、
該検知された合成磁界の磁界強度の絶対値が極大値又は
極小値となったときの上記回転磁界の位相角から、上記
任意の1方向に対する地磁気方位角を検知するようにし
たことを特徴とする地磁気方位計。
1. A rotating magnetic field generating means, and a magnetic field strength sensor arranged at the center of the rotating magnetic field generating means for detecting magnetic field strength in any one direction. Detects the magnetic field strength of the combined magnetic field of rotating magnetic field and geomagnetism by means,
The geomagnetic azimuth angle with respect to the arbitrary one direction is detected from the phase angle of the rotating magnetic field when the absolute value of the detected magnetic field strength of the synthesized magnetic field has a maximum value or a minimum value. A geomagnetic compass.
JP1009795A 1995-01-25 1995-01-25 Geomagnetic azimuth meter Pending JPH08201060A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1009795A JPH08201060A (en) 1995-01-25 1995-01-25 Geomagnetic azimuth meter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1009795A JPH08201060A (en) 1995-01-25 1995-01-25 Geomagnetic azimuth meter

Publications (1)

Publication Number Publication Date
JPH08201060A true JPH08201060A (en) 1996-08-09

Family

ID=11740829

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1009795A Pending JPH08201060A (en) 1995-01-25 1995-01-25 Geomagnetic azimuth meter

Country Status (1)

Country Link
JP (1) JPH08201060A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100477511B1 (en) * 2001-11-22 2005-03-17 야마하 가부시키가이샤 Electronic apparatus
CN105510849A (en) * 2015-11-26 2016-04-20 哈尔滨工业大学 Aeromagnetic interference compensation method

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100477511B1 (en) * 2001-11-22 2005-03-17 야마하 가부시키가이샤 Electronic apparatus
CN105510849A (en) * 2015-11-26 2016-04-20 哈尔滨工业大学 Aeromagnetic interference compensation method

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