CN107192368B - A kind of rotation angle measurement method of 3 structure faces dead axle - Google Patents

A kind of rotation angle measurement method of 3 structure faces dead axle Download PDF

Info

Publication number
CN107192368B
CN107192368B CN201710384795.4A CN201710384795A CN107192368B CN 107192368 B CN107192368 B CN 107192368B CN 201710384795 A CN201710384795 A CN 201710384795A CN 107192368 B CN107192368 B CN 107192368B
Authority
CN
China
Prior art keywords
plane
rotation
angle
shaft
displacement
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 - Fee Related
Application number
CN201710384795.4A
Other languages
Chinese (zh)
Other versions
CN107192368A (en
Inventor
李凡星
田鹏
杨帆
严伟
彭伏平
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.)
Institute of Optics and Electronics of CAS
Original Assignee
Institute of Optics and Electronics of CAS
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 Institute of Optics and Electronics of CAS filed Critical Institute of Optics and Electronics of CAS
Priority to CN201710384795.4A priority Critical patent/CN107192368B/en
Publication of CN107192368A publication Critical patent/CN107192368A/en
Application granted granted Critical
Publication of CN107192368B publication Critical patent/CN107192368B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01BMEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B21/00Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant
    • G01B21/22Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant for measuring angles or tapers; for testing the alignment of axes

Abstract

The invention discloses a kind of rotation angle measurement methods of 3 structure face dead axles, in the uncertain situation of plane shaft, the mode of general measure Plane Rotation angle is difficult to directly accurately measure Plane Rotation angle, and existing unknown axis measurement method precision is not high enough, and process is relatively complicated.The present invention uses three high accuracy displacement sensors, the known points of three form right angle triangles on Plane of rotation is measured before rotation and postrotational displacement, according to geometrical relationship, calculate the angle value of Plane Rotation, without finding Plane Rotation shaft, and to shaft angle with horizontal plane, there is no limit largely reduced since institute's geodesic structure is special, shaft is difficult to accurately find brought measurement error when measuring.The displacement generated in Plane Rotation for measuring the point of the known relation of three form right angle triangles in surveyed plane acquires object rotation angle according to geometrical relationship.

Description

A kind of rotation angle measurement method of 3 structure faces dead axle
Technical field
The invention belongs to field of measuring technique, and in particular to a kind of rotation angle measurement method of 3 structure face dead axles, It does not require to be pushed away in the case where known Plane Rotation axis according to 3 points of displacements in Plane Rotation known in tested plane The true rotation angle for exporting plane removes the step of looking for rotary shaft from Plane Angle measurement, is a kind of novel angle survey Amount mode.
Background technique
Currently, many applications require to carry out the rotation angle measurement of degree of precision, but surveyed using angular transducer Amount must find the rotary shaft of Plane of rotation, and the installation of angular transducer vertical rotating shaft just can be measured accurately, and many special Mechanical devices can not accurately find rotary shaft, and measurement in this way can bring very big error.This design of the invention, without look for by Plane of rotation rotary shaft is surveyed, Plane Rotation angle can be found out according to 3 points of displacements in Plane Rotation known in plane, It is a kind of improvement new paragon of angle measurement.
Summary of the invention
The invention proposes a kind of novel angle measurement methods, and which is when measuring Plane Angle without finding rotation The rotary shaft of plane can find out plane rotation according to 3 points of displacements generated in Plane Rotation known on tested Plane of rotation The real angle turned.
In order to achieve the above object, a kind of the technical solution adopted by the present invention are as follows: rotation angle survey of 3 structure face dead axles Amount method is being revolved using the known point that three high accuracy displacement sensors measure three form right angle triangles on Plane of rotation The angle value of Plane Rotation is calculated according to geometrical relationship with postrotational displacement before turning, is turned without finding Plane Rotation Axis, and to shaft angle with horizontal plane, there is no limit largely reduced since measurement structure is special, shaft when measurement It is difficult to accurately find brought measurement error.Measure the known point of three form right angle triangles on Plane of rotation flat The displacement that face generates when rotating acquires object rotation angle according to geometrical relationship.
Further, it has to accurately find out three known points in tested plane, and these three points constitute one directly Angle triangle, three side lengths of the triangle need it is known that and the right angle of the right angled triangle that constitutes open direction towards quilt Survey the Position Approximate of plane shaft.
Further, Plane Rotation angle can be measured without finding Plane Rotation shaft in measurement, but in plane Known 3 points of displacements generated in Plane Rotation will be measured accurately, and high accuracy displacement sensor or other methods can be passed through It measures.Moreover, in the case that known 3 points of displacements generated in Plane Rotation accurately measure next in plane, to tested flat There is no limit institute is angled to be accurately measured the size of face rotation angle.
Further, three of form right angle triangle known to tested plane are measured by displacement sensor or other modes After displacement of the point in the Plane Rotation, the true angle of Plane Rotation is gone out by Similar Principle of Triangle and the chord length derivation of equation Degree.
The advantages of the present invention over the prior art are that:
(1), the present invention can be measured accurately when measuring Plane Rotation angle without known plane shaft.
(2), there is no limit to surveyed plane shaft angle with horizontal plane by the present invention.
(3), 3 points of displacements in tested Plane Rotation determined by being tested in plane can accurately measure situation about coming Under, there is no limit to institute's measuring angle size for the Plane Angle measurement method.
Detailed description of the invention
Fig. 1 is a kind of rotation angle measurement method schematic of 3 structure face dead axles of the present invention;
Fig. 2 is the letter for the rotation angle measurement method that the present invention implements 3 structure face dead axles using linear displacement transducer Figure.
Specific embodiment
For a better understanding of the technical solution of the present invention, being described in further detail below in conjunction with attached drawing.
A kind of Plane Rotation angle measurement method without looking for shaft based on displacement measurement, the specific steps are as follows:
Step 1: three known points are found in measurement plane, and these three points constitute a right angled triangle, the right angle Atria side length wants known;
Step 2: high accuracy displacement sensor or other modes are used, are measured known to three respectively in Plane Rotation And the displacement of the point of form right angle triangle;
Step 3: use three measured displacements, and in surveyed plane known right angled triangle side length, root Plane Rotation angle is calculated according to Similar Principle of Triangle and chord length formula.
Fig. 1 is the Plane Rotation angle measurement method schematic diagram without looking for shaft about a kind of based on displacement measurement, such as Shown in figure, wherein L is shaft, and 3 points of A, B, C in tested plane, and constitute known right angled triangle ABC.Use displacement sensing Device or other modes measure 3 points of displacements moved in Plane Rotation of A, B, C, are set to SA、SB、Sc
When the plane rotates θ angle around L axis, there is chord length formula:
Wherein R is radius of turn, and the distance that as point A, B, C arrives shaft L respectively is set to AA ', BB ', CC ';S is Chord length, as displacement sensor amount SA、SB、Sc.Wherein triangle ABC is right angled triangle, and AB edge lengths and BC side length Degree is it is known that BM is the side BC extended line, and BN is the side AB extended line, and AA ', BB ' and CC ' are perpendicular to shaft L.It is apparent from triangle AA ' N Similar to triangle BB ' N, triangle CC ' M is similar to triangle BB ' M, periodically revolves further according to angle, θ one is rotated in arc length formula Turn that radius R is proportional to chord length S to be had:
BN and BM length can be found out according to above two formula, and in triangle MBN, angle MBN is right angle, and BN and BM length can It asks, can be asked according to right angled triangle area formula:
Bring chord length formula intoWherein R is radius, and S is chord length, and θ is rotation angle, is had:
S in the formulaA、SB、ScFor displacement sensor value, known to the side AB and BC edge lengths, it is possible to directly find out Plane Rotation angle, θ.
By the above reasoning it is found that on known tested Plane of rotation 3 points of form right angle triangle generated in Plane Rotation Displacement, the real angle of tested Plane Rotation can be obtained further according to chord length formula and Similar Principle of Triangle.
Fig. 2 is the letter for the rotation angle measurement method that the present invention implements 3 structure face dead axles using linear displacement transducer Figure, wherein three displacement sensors are separately fixed on fixed pan, is fixed on rotation for the measurement end of three displacement sensors Turn 3 points of A, B, C in plane;Plane of rotation rotation, displacement sensor generate corresponding displacement reading;According in specific embodiment Solution mode can acquire rotation angle.But it may be noted that this kind of displacement measurement mode is the displacement of 3 points of approximate A, B, C, This kind of linear displacement transducer in the lesser situation of angle is only rotated just to use.
Generally, a kind of Plane Rotation angle measurement side without looking for shaft based on displacement measurement of the present invention Method, this kind of measurement method can reach degree of precision under the misalignment of known tested plane form right angle Atria point, It calculates simply, and without finding Plane Rotation shaft.The invention can be used for the inertial measurement system of spacecraft, mechanical arm rotation The multiple fields such as transfer to test, vehicle hull wheel measuring are particularly suitable for the rotation that shaft is difficult to determining large-scale apparatus structure Angle measurement.
The content that the present invention does not elaborate belongs to technology well known to field personnel of the present invention.

Claims (1)

1. a kind of rotation angle measurement method of 3 structure face dead axles, it is characterised in that: the measurement method uses three high-precisions Displacement sensor measures the known points of three form right angle triangles on Plane of rotation before rotation and postrotational displacement Amount, according to geometrical relationship, calculates the angle value of Plane Rotation, without finding Plane Rotation shaft, and to shaft when measurement There is no limit largely reduce since institute's geodesic structure is special, shaft is difficult to accurately find and be brought angle with horizontal plane Measurement error, measure the generation in Plane Rotation of the point of the known relation of three form right angle triangles in surveyed plane Displacement object rotation angle is acquired according to geometrical relationship;
It has to accurately find out three known points in tested plane, and these three points constitute a right angled triangle, the triangle Three side lengths of shape need it is known that and the right angle of the right angled triangle that constitutes open direction and need towards being tested the big of plane shaft Position approximate is set;
Plane Rotation angle can be measured without finding Plane Rotation shaft in measurement, but in plane known 3 points revolved in plane The displacement generated when turning will be measured accurately, can be measured by high accuracy displacement sensor;
3 points of known form right angle triangle in tested plane are measured in the Plane Rotation by high accuracy displacement sensor Displacement after, Plane Rotation real angle is gone out by Similar Principle of Triangle and the chord length derivation of equation.
CN201710384795.4A 2017-05-26 2017-05-26 A kind of rotation angle measurement method of 3 structure faces dead axle Expired - Fee Related CN107192368B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710384795.4A CN107192368B (en) 2017-05-26 2017-05-26 A kind of rotation angle measurement method of 3 structure faces dead axle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710384795.4A CN107192368B (en) 2017-05-26 2017-05-26 A kind of rotation angle measurement method of 3 structure faces dead axle

Publications (2)

Publication Number Publication Date
CN107192368A CN107192368A (en) 2017-09-22
CN107192368B true CN107192368B (en) 2019-10-08

Family

ID=59874938

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201710384795.4A Expired - Fee Related CN107192368B (en) 2017-05-26 2017-05-26 A kind of rotation angle measurement method of 3 structure faces dead axle

Country Status (1)

Country Link
CN (1) CN107192368B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113267112B (en) * 2021-03-29 2022-08-19 河北沧海核装备科技股份有限公司 Method for measuring bending angle of induction heating bent pipe

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101566470A (en) * 2009-05-08 2009-10-28 上海都峰智能科技有限公司 Method for correcting position of angle sensor
CN104006786A (en) * 2014-06-18 2014-08-27 清华大学 Curved surface normal vector measurement device
CN105444722A (en) * 2015-12-21 2016-03-30 中国科学院长春光学精密机械与物理研究所 Method for detecting changes of postures of platform

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101566470A (en) * 2009-05-08 2009-10-28 上海都峰智能科技有限公司 Method for correcting position of angle sensor
CN104006786A (en) * 2014-06-18 2014-08-27 清华大学 Curved surface normal vector measurement device
CN105444722A (en) * 2015-12-21 2016-03-30 中国科学院长春光学精密机械与物理研究所 Method for detecting changes of postures of platform

Also Published As

Publication number Publication date
CN107192368A (en) 2017-09-22

Similar Documents

Publication Publication Date Title
CN107063119B (en) Inner wall of the pipe pattern and central axis linearity measurer and method
CN105423910B (en) Deflection angle of airplane control surface degree measuring device and method
CN101813465B (en) Monocular vision measuring method of non-contact precision measuring corner
CN111366908A (en) Laser radar rotary table and measuring device and measuring method thereof
CN110134134A (en) A kind of wind detection method under unmanned plane floating state
CN106290968A (en) A kind of large space pulsatile flow field three-dimension measuring system and measuring method
CN106940195B (en) Double-shaft tilt angle sensor input shaft is misaligned error calibration method
CN104515481A (en) Device and method for measuring planeness of large-diameter torus
CN107192368B (en) A kind of rotation angle measurement method of 3 structure faces dead axle
CN102809367A (en) Space rotating angle measuring method based on double-shaft obliquity sensor
CN102207380A (en) High-precision horizontal axis tilt error compensation method
CN104390624A (en) Inclined circular cone angle horizontal rotary measuring method
AU2002223460B2 (en) Method for determining the orientation of a cylindrical body in relation to a reference direction
CN109357612A (en) One kind being used for static liquid level capacitance displacement sensor on-line calibration method
CN206020457U (en) A kind of five-hole probe based on inertial sensor
WO2018161717A1 (en) Rotation speed measuring device and method employing two sinusoidal variable density fringes
JP2006300702A (en) Revolution speed detector and rotating flying object
CN104316230A (en) Method and device for measuring vector force borne by cylindrical beam
CN109211272B (en) Method for measuring scale factor of variable speed tilting momentum wheel tilting angle sensor by adopting space rotation moment
CN111721962B (en) Flow velocity measuring method based on Magnus effect
CN202420497U (en) Auxiliary measuring device for measuring point position coordinate by using total station
CN115200487A (en) Safety measuring device and safety evaluation method for large-diameter pipeline
CN208653434U (en) A kind of indexing single-line type spatial position measuring device
CN101825448B (en) Method for determining included angle between lens plane of thermal infrared imager and plane to be measured
CN106885922A (en) A kind of wind vane calibrating installation and method for wind power generating set

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20191008

Termination date: 20210526