JP3441006B2 - Correction method of position and attitude angle of thruster - Google Patents

Correction method of position and attitude angle of thruster

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Publication number
JP3441006B2
JP3441006B2 JP12494793A JP12494793A JP3441006B2 JP 3441006 B2 JP3441006 B2 JP 3441006B2 JP 12494793 A JP12494793 A JP 12494793A JP 12494793 A JP12494793 A JP 12494793A JP 3441006 B2 JP3441006 B2 JP 3441006B2
Authority
JP
Japan
Prior art keywords
underground
thruster
attitude angle
propulsion
attitude
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.)
Expired - Lifetime
Application number
JP12494793A
Other languages
Japanese (ja)
Other versions
JPH06307184A (en
Inventor
一嘉 川端
友博 黒沢
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.)
Nippon Telegraph and Telephone Corp
Original Assignee
Nippon Telegraph and Telephone 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 Nippon Telegraph and Telephone Corp filed Critical Nippon Telegraph and Telephone Corp
Priority to JP12494793A priority Critical patent/JP3441006B2/en
Publication of JPH06307184A publication Critical patent/JPH06307184A/en
Application granted granted Critical
Publication of JP3441006B2 publication Critical patent/JP3441006B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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  • Excavating Of Shafts Or Tunnels (AREA)

Description

【発明の詳細な説明】 【0001】 【産業上の利用分野】本発明は、計画位置にトンネルを
築造するために、地中推進機の位置及び(方位角)を計
測する地中推進機の位置と姿勢角度の補正方法に関する
ものである。 【0002】 【従来の技術】計画位置に正確にトンネルを築造する目
的で、地中推進機を制御しながら推進計画線に沿って推
進させるためには、常時、地中推進機の位置及び姿勢角
を把握していなければならない。 【0003】従来、地中推進機の位置は、地中推進距離
計測用ストローク計で、検出した信号を基に計算して求
めてきた。また、その姿勢角(方位角)は、本発明の図
1に示す地中推進機を参照にして説明する。地中推進機
に設置された、ヨーイングを検出する角速度センサ2、
ピッチングを検出する仰角計測用加速度計3、ローリン
グを検出する回転角計測用加速度計4の3つの検出器の
信号を基に計算して求めてきた。 【0004】 【発明が解決しようとする課題】従来の方法においては
地中推進機に設置した角速度センサは長時間計測してい
るあいだに計測角度にドリフト量を含むようになる。こ
の角速度センサは、地中推進機の姿勢及び位置計測誤差
の原因となっている。 【0005】本発明は、従来の地中推進機にジャイロコ
ンパス、発信コイルおよび後部にターゲット板を設け、
前記ジャイロコンパスから得られる姿勢角度により、角
速度センサによって計測した誤差を含む姿勢角度を、あ
る推進距離毎に補正し、姿勢角度計測における誤差累積
を防止すると共に推進計画線に沿うトンネルの地上の受
信コイルにより前記発信コイルからの電磁界を検知して
推進機の位置を、更にトンネル口にレーザー光線発生装
置を設けレーザー光線を発射し、推進機に設けたターゲ
ット板上に結ぶ像の位置とを用いて誤差を含む姿勢角度
から算出した推進機の位置を、ある推進距離毎に補正す
る方法である。 【0006】 【実施例】図1は本発明の計測器を搭載した地中推進
機、図2は本発明の地中推進機を使用し地中推進機の位
置を求める方法の説明図、である。図1において、符号
1、2、3、4は従来例で説明した計器である。6はジ
ャイロコンパス、10は発信コイル、12はターゲット
板である。図2において、7は立杭、8は元押装置、9
は演算装置、11は受信コイル、13はレーザー発信
機、14は電力・信号ケーブル、15は操作卓、Tは管
体である。 【0007】地中推進機1に搭載した各計器の作用を説
明する。角速度センサ2は、角速度センサ2が設置され
ている面上の左右方向の針路ずれ(yawing)の変
化角速度を計測する。また、仰角計測用加速度計3は、
ピッチングの変化角度を、回転角計測用加速度4は、ロ
ーリングの変化角度を計測する。 【0008】図2に示すように、この値と立杭7内の元
押装置8に設置された地中推進距離計測用ストローク計
5より得られる距離信号とから演算装置9で地中推進機
1の水平位置を演算する。角速度センサ2を長時間使用
する場合、検出される変化角速度にドリフト量が含まれ
るようになる。即ち、地中推進機1の姿勢角及び位置測
定に誤差が生じることになる。そこで、地中推進機1の
姿勢角及び位置測定誤差を補正するため、角速度センサ
2のドリフト量が大きくならないうちに地中推進機1に
設置されたジャイロコンパス6により、地中推進機1の
より正確な姿勢角を測定し、この値を角速度センサ2に
よって測定された地中推進機1の姿勢角に代えて地中推
進機1の姿勢角とする。元押装置8は地中推進機1の堀
削した穴に管体Tを順に挿入する装置である。 【0009】図2は電磁コイル又はレーザー光線で地中
推進機の位置を求める方法を説明する断面図である。地
中推進機1に設置された発信コイル10によって発生し
た電磁界を地上の2つの受信コイルで感知することによ
り位置を検知する方法又は地中推進機1に設置されたタ
ーゲット板12に立杭7内のレーザー発信機13よりレ
ーザー光線を照射し、その位置を立杭7内より確認する
ことにより位置を検知する方法により地中推進機1の位
置を検知し、地中推進機1の位置とする。この方法によ
って、地中推進機1の姿勢角及び位置測定誤差をなくす
ことができるので、地中推進機の姿勢角及び位置を高精
度に計測することが可能となる。発信コイル10と受信
コイル11により地中推進機1の位置を検出する場合、
地中には磁性を有する埋設材があり、発信コイル10よ
りの磁界がみだされることもあるので、これを補正する
目的でレーザー発信機13を設けている。一方、彎曲す
る堀削路では直進するレーザー光線だけでは位置を正確
に検出できないので発信コイル10を設けたものであ
る。上記コイル10、11あるいはレーザ発信機13を
用いて、地中推進機1の正確な位置を確認できるので、
誤差を含む姿勢角度から算出してきた地下推進機1の位
置に対して必要により、地中推進機1の位置をある推進
距離ごとに補正できる。 【0010】 【発明の効果】本発明は以上の方法であるため、以下に
記載されるような効果を奏する。地中推進機の位置・姿
勢角を高精度に計測することが可能となるので、計画位
置にトンネルを正確に築造することに非常に大きく寄与
する。
Description: BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an underground thruster for measuring the position and (azimuth) of an underground thruster in order to construct a tunnel at a planned position. The present invention relates to a method for correcting a position and a posture angle. 2. Description of the Related Art In order to build a tunnel at a planned position accurately and to propel the underground thruster along a propulsion plan line while controlling the underground thruster, the position and attitude of the underground thruster are always required. You must know the corner. Conventionally, the position of an underground thruster has been obtained by a stroke meter for measuring an underground thrust distance based on a detected signal. The attitude angle (azimuth angle) will be described with reference to the underground propulsion device shown in FIG. 1 of the present invention. An angular velocity sensor 2 installed in the underground thruster to detect yawing,
It has been obtained by calculation based on the signals of three detectors, an accelerometer for elevation angle measurement 3 for detecting pitching and an accelerometer 4 for rotation angle measurement for detecting rolling. [0004] In the conventional method, the angular velocity sensor installed in the underground propulsion device includes a drift amount in the measurement angle during long-time measurement. This angular velocity sensor causes a measurement error of the attitude and position of the underground propulsion device. According to the present invention, a gyrocompass, a transmitting coil, and a target plate are provided at a rear portion of a conventional underground propulsion device,
Based on the attitude angle obtained from the gyro compass, the attitude angle including the error measured by the angular velocity sensor is corrected for each certain propulsion distance to prevent accumulation of errors in the attitude angle measurement and to receive the ground on the tunnel along the propulsion plan line. Using a coil to detect the electromagnetic field from the transmitting coil and determine the position of the propulsion device, further using a laser beam generator provided at the tunnel entrance to emit a laser beam, and using the position of the image formed on the target plate provided in the propulsion device In this method, the position of the propulsion device calculated from the attitude angle including the error is corrected for each certain propulsion distance. FIG. 1 is an underground thruster equipped with a measuring instrument according to the present invention, and FIG. 2 is an explanatory diagram of a method for determining the position of the underground thruster using the underground thruster according to the present invention. is there. In FIG. 1, reference numerals 1, 2, 3, and 4 denote instruments described in the conventional example. 6 is a gyrocompass, 10 is a transmitting coil, and 12 is a target plate. In FIG. 2, 7 is a standing pile, 8 is a main pushing device, 9
Denotes an arithmetic unit, 11 denotes a receiving coil, 13 denotes a laser transmitter, 14 denotes a power / signal cable, 15 denotes a console, and T denotes a tube. The operation of each instrument mounted on the underground propulsion device 1 will be described. The angular velocity sensor 2 measures a change angular velocity of a course deviation (yawing) in a left-right direction on a surface on which the angular velocity sensor 2 is installed. In addition, the accelerometer 3 for measuring the elevation angle is
The pitching change angle is determined by the rotation angle measurement acceleration 4 .
The angle of change of the ring is measured. As shown in FIG. 2, the arithmetic unit 9 calculates the underground thruster from this value and the distance signal obtained from the underground thrust distance measuring stroke meter 5 installed in the main pushing device 8 in the standing pile 7. 1 is calculated. When the angular velocity sensor 2 is used for a long time, the detected change angular velocity includes the drift amount. That is, an error occurs in the measurement of the attitude angle and the position of the underground propulsion device 1. Therefore, in order to correct the measurement error of the attitude angle and the position of the underground thruster 1, the gyro compass 6 installed in the underground thruster 1 before the amount of drift of the angular velocity sensor 2 increases does not cause the underground thruster 1 to move. A more accurate attitude angle is measured, and this value is used as the attitude angle of the underground thruster 1 instead of the attitude angle of the underground thruster 1 measured by the angular velocity sensor 2. The main pushing device 8 is a device for sequentially inserting the pipe T into the excavated hole of the underground propulsion device 1. FIG. 2 is a sectional view for explaining a method for determining the position of the underground thruster using an electromagnetic coil or a laser beam. A method of detecting the position by sensing the electromagnetic field generated by the transmitting coil 10 installed in the underground thruster 1 with two receiving coils on the ground, or a standing pile on the target plate 12 installed in the underground thruster 1 7, a laser beam is emitted from a laser transmitter 13, and the position of the underground propulsion device 1 is detected by a method of detecting the position by confirming the position from within the standing pile 7. I do. With this method, it is possible to eliminate the measurement error of the attitude angle and the position of the underground thruster 1, so that the attitude angle and the position of the underground thruster 1 can be measured with high accuracy. When the position of the underground thruster 1 is detected by the transmitting coil 10 and the receiving coil 11,
Since there is an underground material having magnetism in the ground and a magnetic field from the transmitting coil 10 may be generated, a laser transmitter 13 is provided for the purpose of correcting the magnetic field. On the other hand, the transmitting coil 10 is provided on a curved excavation road because the position cannot be accurately detected only by a laser beam traveling straight. Since the exact position of the underground propulsion machine 1 can be confirmed using the coils 10 and 11 or the laser transmitter 13,
If necessary for the position of the underground propulsion device 1 calculated from the attitude angle including the error, the position of the underground propulsion device 1 can be corrected for each certain propulsion distance. Since the present invention is based on the above method, the following effects can be obtained. Since the position and attitude angle of the underground thruster can be measured with high accuracy, it greatly contributes to accurately constructing a tunnel at a planned position.

【図面の簡単な説明】 【図1】本発明の地中推進機の構成図、である。 【図2】本発明の地中推進機に搭載した発信コイルとタ
ーゲット板により地中推進機の位置を求める方法を説明
する断面図である。 【符号の説明】 1 地下推進機 2 角速度センサ 3 仰角計測用加速度計 4 回転角計測用加速度計 5 地中推進距離計測用ストローク計 6 ジャイロコンパス 7 立杭 8 元押装置 9 演算装置 10 発信コイル 11 受信コイル 12 ターゲット板 13 レーザー発信機 14 電力・信号ケーブル 15 操作卓 T 管体
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a configuration diagram of an underground thruster of the present invention. FIG. 2 is a cross-sectional view illustrating a method for determining the position of the underground propulsion device using a transmission coil and a target plate mounted on the underground propulsion device according to the present invention. [Description of Signs] 1 Underground Propulsion Machine 2 Angular Velocity Sensor 3 Elevation Angle Measurement Accelerometer 4 Rotation Angle Measurement Accelerometer 5 Underground Propulsion Distance Measurement Stroke Meter 6 Gyro Compass 7 Standing Pile 8 Main Pushing Device 9 Computing Device 10 Transmitting Coil Reference Signs List 11 Receiving coil 12 Target plate 13 Laser transmitter 14 Power / signal cable 15 Console T tube

───────────────────────────────────────────────────── フロントページの続き (56)参考文献 特開 平4−12219(JP,A) 特開 平2−40581(JP,A) 特開 平5−65795(JP,A) 特開 平5−5396(JP,A) 特開 平4−68184(JP,A)   ────────────────────────────────────────────────── ─── Continuation of front page       (56) References JP-A-4-12219 (JP, A)                 JP-A-2-40581 (JP, A)                 JP-A-5-65795 (JP, A)                 JP-A-5-5396 (JP, A)                 JP-A-4-68184 (JP, A)

Claims (1)

(57)【特許請求の範囲】 【請求項1】地中推進機の位置は、地中推進距離計測用
ストローク計で検出した信号を基に計測し、地中推進機
の姿勢角は、ヨーイングを検出する角速度センサとピッ
チングを検出する仰角計測用加速度計とローリングを検
出する回転角計測用加速度計の3つの検出器の信号を基
に計測する地中推進機の位置・姿勢計測方法において、 地中推進機にジャイロコンパス、発信コイルおよび後部
にターゲット板を設け、前記ジャイロコンパスから得ら
れる姿勢角度により、角速度センサによって計測した累
積誤差を含む姿勢角度をある推進距離毎に補正し、姿勢
角度計測における誤差の累積を防止すると共に推進計画
線に沿うトンネルの地上の受信コイルにより前記発信コ
イルからの電磁界を検知して推進機の位置を、更にトン
ネル口にレーザー光線発生装置を設けてレーザー光線を
発射し、推進機に設けたターゲット板上に結ぶ像の位置
を用いて累積誤差を含む姿勢角度から算出した推進機の
位置を、ある推進距離毎に補正し、位置計測における誤
差の累積を防止することを特徴とする推進機の位置と姿
勢角度の累積誤差の補正方法。
(57) [Claims] [Claim 1] The position of the underground thruster is for measuring the underground thrust distance.
Measures based on the signal detected by the stroke meter, and
The attitude angle of the motor is controlled by the angular velocity sensor that detects yawing and the pitch.
Elevation angle measurement accelerometer that detects
Based on the three detector signals of the accelerometer for measuring the rotation angle
In the method of measuring the position and attitude of the underground thruster, the underground thruster is provided with a gyro compass, a transmitting coil and a target plate at the rear, and a cumulative error measured by an angular velocity sensor by an attitude angle obtained from the gyro compass. Is corrected for each propulsion distance, preventing the accumulation of errors in the attitude angle measurement, and detecting the electromagnetic field from the transmitting coil by the receiving coil on the ground of the tunnel along the propulsion planning line, The position, the position of the propulsion device calculated from the attitude angle including the accumulated error using the position of the image formed on the target plate provided in the propulsion device, further providing a laser beam generator at the tunnel entrance and emitting the laser beam, Accumulated error in the position and attitude angle of the propulsion unit, which is corrected for each propulsion distance to prevent accumulation of errors in position measurement Correction method.
JP12494793A 1993-04-28 1993-04-28 Correction method of position and attitude angle of thruster Expired - Lifetime JP3441006B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP12494793A JP3441006B2 (en) 1993-04-28 1993-04-28 Correction method of position and attitude angle of thruster

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP12494793A JP3441006B2 (en) 1993-04-28 1993-04-28 Correction method of position and attitude angle of thruster

Publications (2)

Publication Number Publication Date
JPH06307184A JPH06307184A (en) 1994-11-01
JP3441006B2 true JP3441006B2 (en) 2003-08-25

Family

ID=14898145

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12494793A Expired - Lifetime JP3441006B2 (en) 1993-04-28 1993-04-28 Correction method of position and attitude angle of thruster

Country Status (1)

Country Link
JP (1) JP3441006B2 (en)

Also Published As

Publication number Publication date
JPH06307184A (en) 1994-11-01

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