CN106774154B - A kind of space curve interpolating method based on osculating plane theory - Google Patents

A kind of space curve interpolating method based on osculating plane theory Download PDF

Info

Publication number
CN106774154B
CN106774154B CN201611258996.1A CN201611258996A CN106774154B CN 106774154 B CN106774154 B CN 106774154B CN 201611258996 A CN201611258996 A CN 201611258996A CN 106774154 B CN106774154 B CN 106774154B
Authority
CN
China
Prior art keywords
point
high error
space curve
bow
section
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
CN201611258996.1A
Other languages
Chinese (zh)
Other versions
CN106774154A (en
Inventor
智红英
闫献国
杜娟
张唐圣
陈峙
郭宏
陈高华
曹启超
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.)
Taiyuan University of Science and Technology
Original Assignee
Taiyuan University of Science and Technology
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 Taiyuan University of Science and Technology filed Critical Taiyuan University of Science and Technology
Priority to CN201611258996.1A priority Critical patent/CN106774154B/en
Publication of CN106774154A publication Critical patent/CN106774154A/en
Application granted granted Critical
Publication of CN106774154B publication Critical patent/CN106774154B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05BCONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B19/00Programme-control systems
    • G05B19/02Programme-control systems electric
    • G05B19/18Numerical control [NC], i.e. automatically operating machines, in particular machine tools, e.g. in a manufacturing environment, so as to execute positioning, movement or co-ordinated operations by means of programme data in numerical form
    • G05B19/404Numerical control [NC], i.e. automatically operating machines, in particular machine tools, e.g. in a manufacturing environment, so as to execute positioning, movement or co-ordinated operations by means of programme data in numerical form characterised by control arrangements for compensation, e.g. for backlash, overshoot, tool offset, tool wear, temperature, machine construction errors, load, inertia
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05BCONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B2219/00Program-control systems
    • G05B2219/30Nc systems
    • G05B2219/35Nc in input of data, input till input file format
    • G05B2219/35408Calculate new position data from actual data to compensate for contour error

Landscapes

  • Engineering & Computer Science (AREA)
  • Human Computer Interaction (AREA)
  • Manufacturing & Machinery (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Image Generation (AREA)
  • Complex Calculations (AREA)
  • Numerical Control (AREA)

Abstract

The invention belongs to Computerized Numerical Control processing technology fields, it is proposed that a kind of space curve interpolating method based on osculating plane theory is mainly used for tool-path planning operation in Multi-axis Machining.According to the local geometric shape on space curve at interpolated point, the interpolated point of the high error of the bow such as equidistant surface construction satisfaction is utilized on the principal normal direction from section of each interpolated point.But the high error of bow of the high error of bow that this side up not necessarily truly, establishes apart from meaning followed by analytic geometry midpoint to straight line and bends high error functionThe high error of most longbow calculated between two adjacent discrete points is verified.Cutting step can adaptively be adjusted using new method, realize the high error of bow truly, be evenly distributed respectively approaching the high error of the bow in straightway, high precision machining, surface quality is good.

Description

A kind of space curve interpolating method based on osculating plane theory
Technical field:
The invention belongs to Computerized Numerical Control processing technology field more particularly to a kind of space curve interpolation sides based on osculating plane theory Method is mainly used for tool-path planning operation in Machining of Curved Surface.
Background technology:
In the process industries such as aviation, aerospace industry, automobile and mold, there is largely have complex-curved part, These parts not only complex geometry, and the accuracy of manufacture and surface quality requirements are very high.With computer technology and certainly The development of dynamic control technology, has application of the complex-curved part in industrial products more and more extensive.Currently, complex-curved The processing of part is mostly realized by numerically-controlled machine tool.Tool-path planning is the important composition of design for NC Part, designing quality directly affect the machining accuracy and processing efficiency of part.The cutter path of Machining of Curved Surface is by one Cutter-contact point trace curve composition, from geometrically saying, each cutter-contact point trace curve is essentially all a space curve, because This tool-path planning is converted to the interpolated point computational problem of a rule space curve.Different interpolation point calculating methods are with regard to shape At different interpolating methods.
Currently, the wider interpolation point calculating method of application range mainly has equal parameter step lengths method, equidistant step length, step-length Screening method etc..
Equal parameter step lengths method and equidistant step length are divided to parameter and curve equidistant, although both methods is simple, However in order to enable the approximate error of every section of straight line is met the requirements, step-length or parameter increase can only be selected using adverse conditions the most It takes, to cause remaining processing sequences huge, the actual high error of bow is unevenly distributed.
Based on step-length screening method uses equal steps, smaller equidistance or parameter discrete cutter rail are used before this Then mark checks the practical approximate error of every section of straight line, finally need to delete extra discrete point, so that remaining trajectory error More uniformly.The shortcomings that parameter step lengths methods such as although step-length screening method overcomes and equidistant step length, but checking every section directly All it is approximately to bend high error when the high error of bow in line, to influence the surface quality of curved surface, reduces the processing essence of workpiece Degree.
Invention content:
In order to solve the problems, such as that conventional method exists in terms of Multi-axis Machining tool-path planning step size computation, the present invention carries A kind of space curve interpolating method of the satisfaction bow high franchise theoretical based on osculating plane is gone out.It can be according to P on space curve0Point The local geometric shape at place, is adaptively adjusted cutting step, and the practical bow in every section of straight line is calculated using high error function is bent High error so that be evenly distributed respectively approaching the high error of the bow in straightway, high precision machining, surface quality is good.
According to the relevant knowledge of Differential Geometry, at any on space curve, three orthogonal tangent lines, principal normals The fundamental three-vector form that curve is constituted with binormal, is generated the osculating plane of this point by them, normal plane and from section.? In these three planes, the plane that osculating plane is " most close to curve " was tangent line and perpendicular to osculating plane from section.It is based on This conclusion, the high error requirements of the bow such as satisfaction obtain discrete interpolated point on the principal normal direction from section, due at each point Bent curvature of a curve and torsion difference, the high error of the bow of error not necessarily truly at this time, so also needing to utilize Bend the high error of most longbow that high error function calculates between two-phase neighbor interpolation point to be verified.
According to being described above, it includes following step to bend the space curve interpolating method of high franchise based on the theoretical satisfaction of osculating plane Suddenly:
Step (1) assumes parametric equation r=r (t)={ x (t), y (t), z (t) } t ∈ [a, b] of a space curve Γ, When interpolation starts, the 0th interpolated point P0Parameter be t0=a, bends high franchise ε, and the high franchise size of bow influences free curve Surface quality and machining accuracy, it is better to bend the smaller surface quality of high franchise, and the high franchise of bow is by manufacturer according to being processed Surface set, be known quantity;
Step (2) is in P0At point, r (t are calculated0),r′(t0),r″(t0), acquire equation the r " (t from section π0)·[ρ-r (t0)]=0, ρ be from section any point vector, on principal normal direction with bend high franchise ε be distance construction from section π's Equidistant surface π1
Step (3) simultaneous equidistant surface π1The equation of equation and space curve Γ solves equidistant surface π1With the friendship of space curve Γ The parameter t of point1
Step (4) calculates t0And t1Two corresponding interpolated point P0And P1Between the high error max δ of most longbow.Solve most longbow High error has mid-point method, dichotomy and Fibonacci method, but is not the high error of most longbow truly, error degree ratio Higher, the present invention establishes P by using the knowledge of the distance at analytic geometry midpoint to straight line0And P1Any point between 2 points The high error function of bowThe method being most worth is asked to acquire max δ using function;
Step (5) is if max δ<ε, then P1As next interpolated point, satisfaction bow Gao Yun is otherwise found using line search method The point that difference requires is as next interpolated point;
Step (6) return to step (2);Until the operation of a space curve terminates.
Description of the drawings
Fig. 1 is equidistant surface schematic diagram.
Fig. 2 is flow chart of the method for the present invention.
Fig. 3 is the interpolated point schematic diagram of space curve Γ.
Fig. 4 is the high error curve diagram of most longbow between space curve Γ interpolated points.
Specific implementation mode
In order to make the purpose , technical scheme and advantage of the present invention be clearer, below in conjunction with attached drawing 1-4 and embodiment The present invention is further described in detail in son.Specific embodiment described herein is only used for explaining the present invention, not For limiting the present invention.
1. assuming that the parametric equation of a space curve Γ is r=r (t)={ t, t2,t3T ∈ [0,100], the 0th interpolation Point P0Parameter be t0=0, bend high franchise ε=0.001.
2. in P0At point, r (t are calculated0),r′(t0),r″(t0),
Then r (t0)={ t0,t0 2,t0 3, r, ' (t0)={ 1,2t0,3t0 2, r " (t0)={ 0,2,6t0,
It obtains from section π equations and is:r″(t0)·[ρ-r(t0)]=0, i.e. y+3t0z-t0 2-3t0 4=0, ρ are to take up an official post from section The vector of a bit.
To bend equidistant surface πs of the high franchise ε for distance construction from section π on the principal normal direction from section π1
3. simultaneous equidistant surface π1The equation of equation and space curve Γ obtains intersection point P1Parameter t1It is equationRoot, utilize matlab softwares solve.
4. calculating P0And P1The high error max δ of most longbow between two-phase neighbor interpolation.Utilize distance between beeline and dot in analytic geometry Meaning, establish P0And P1The high error function of bow of any point between 2 pointsProfit The method being most worth is asked to acquire max δ with function;
5. if max δ<ε, then P1As next interpolated point, section is gradually otherwise reduced using line search method and is found completely The point of the high tolerance requirements of arch of foot is as next interpolated point;
6. return to step (2);Until all interpolated points on a space curve have determined.
Space curve Γ interpolated points schematic diagram and the high error curve diagram of most longbow are as shown in figs. 34.

Claims (2)

1. a kind of space curve interpolating method based on osculating plane theory, which is characterized in that be as follows:
Step (1) assumes that the parametric equation of a space curve Γ is r=r (t) t ∈ [a, b], when interpolation starts, the 0th interpolation Point P0Parameter be t0=a bends high franchise ε;
Step (2) is in P0At point, r (t are calculated0),r′(t0),r″(t0), acquire equation the r " (t from section π0)·[ρ-r(t0)] =0, ρ are the vector of any point from section, are constructed from the equidistant of section π for distance on principal normal direction with bending high franchise ε Face π1
Step (3) simultaneous equidistant surface π1The equation of equation and space curve Γ solves equidistant surface π1With the intersection point of space curve Γ Parameter t1
Step (4) calculates t0And t1Two corresponding interpolated point P0And P1Between the high error max δ of most longbow;
Step (5) is if max δ < ε, P1As next interpolated point, [t is gradually otherwise reduced using line search method0,t1] area Between find and meet the point for bending high tolerance requirements as next interpolated point;
Step (6) return to step (2);Until the operation of a space curve terminates.
2. the space curve interpolating method according to claim 1 based on osculating plane theory, which is characterized in that
Step (4) establishes P0And P1The high error function of bow of any point between 2 points The method being most worth is asked to acquire max δ using function.
CN201611258996.1A 2016-12-30 2016-12-30 A kind of space curve interpolating method based on osculating plane theory Expired - Fee Related CN106774154B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201611258996.1A CN106774154B (en) 2016-12-30 2016-12-30 A kind of space curve interpolating method based on osculating plane theory

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201611258996.1A CN106774154B (en) 2016-12-30 2016-12-30 A kind of space curve interpolating method based on osculating plane theory

Publications (2)

Publication Number Publication Date
CN106774154A CN106774154A (en) 2017-05-31
CN106774154B true CN106774154B (en) 2018-11-13

Family

ID=58953769

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201611258996.1A Expired - Fee Related CN106774154B (en) 2016-12-30 2016-12-30 A kind of space curve interpolating method based on osculating plane theory

Country Status (1)

Country Link
CN (1) CN106774154B (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107145126B (en) * 2017-06-29 2018-01-16 南京航空航天大学 Consider the numerical control machining knife rail subregion mapping method of error band distribution
CN110116353B (en) * 2019-06-03 2021-01-15 武汉理工大学 Abrasive belt grinding and polishing step length optimization method for blade front and rear edge robot
CN111983975B (en) * 2020-07-23 2023-04-18 江苏威泽智能科技股份有限公司 Spline curve interpolation method for parameter increment compensation
CN112987647B (en) * 2021-01-04 2022-03-29 苏州科技大学 Equal-error tool path generation method for five-axis machining of parametric curved surface flat-bottom tool
CN114563979B (en) * 2022-02-25 2023-10-13 苏州谷夫道自动化科技有限公司 Compensation method and system for single-channel semi-closed-loop multi-spindle multi-station processing
CN114879606B (en) * 2022-04-29 2024-08-06 燕山大学 Adaptive control interpolation method for micromachining precision of arbitrary parameter curve

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6225771B1 (en) * 1999-12-01 2001-05-01 General Electric Company Probe chord error compensation
CN105045211A (en) * 2015-07-13 2015-11-11 太原科技大学 Equal-chord-error variable-step tangent interpolation method
CN105676787A (en) * 2015-12-28 2016-06-15 龙兵 Elliptic arc interpolation algorithm
CN105759725A (en) * 2016-03-22 2016-07-13 大连理工大学 Speed-sensitive section constant-speed curve interpolation speed planning method

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6225771B1 (en) * 1999-12-01 2001-05-01 General Electric Company Probe chord error compensation
CN105045211A (en) * 2015-07-13 2015-11-11 太原科技大学 Equal-chord-error variable-step tangent interpolation method
CN105676787A (en) * 2015-12-28 2016-06-15 龙兵 Elliptic arc interpolation algorithm
CN105759725A (en) * 2016-03-22 2016-07-13 大连理工大学 Speed-sensitive section constant-speed curve interpolation speed planning method

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
等弓高误差变步长的插补点求取方法优化;杨振玲,等;《工具技术》;20160831;42-46 *

Also Published As

Publication number Publication date
CN106774154A (en) 2017-05-31

Similar Documents

Publication Publication Date Title
CN106774154B (en) A kind of space curve interpolating method based on osculating plane theory
Lartigue et al. CNC tool path in terms of B-spline curves
CN102637216B (en) Method for generating numerical-control side milling machining tool path for complicated curved surfaces
Pateloup et al. Bspline approximation of circle arc and straight line for pocket machining
Chiou Accurate tool position for five-axis ruled surface machining by swept envelope approach
CN104615083B (en) Curved surface tool path contour error compensation method based tool location point correction
KR101928419B1 (en) Tool Path Generation Method and Machine Tool
US20120215334A1 (en) Tool path generation method and device
CN102289534A (en) Method for modeling involute helical gear accurately
CN102581705B (en) Division compensation method for machining error during milling of workpiece
Gong et al. Optimize tool paths of flank milling with generic cutters based on approximation using the tool envelope surface
CN103809521B (en) SPL interpolating method based on Secant Method
CN110069041A (en) A kind of Work piece processing method and system based on on-machine measurement
Lai Tool-path generation of planar NURBS curves
CN108062071B (en) Real-time measuring method for parameter curve track servo contour error
CN107037779A (en) Free form surface NC process tool track optimizing methods under non-homogeneous tolerance
CN104317251A (en) Three-order NURBS curve real-time interpolation method based on Obrechkoff algorithm
CN104035379B (en) Compensation method for perpendicularity error between feed shafts
JP2007279937A (en) Method for machining contour surface and solid by numerical control single cutting tool
Min et al. An improved b-spline fitting method with arc-length parameterization, g 2-continuous blending, and quality refinement
Li et al. Tool path optimization in postprocessor of five-axis machine tools
Du et al. The avoidance of cutter gouging in five-axis machining with a fillet-end milling cutter
Lo et al. An improved method for scheduling the tool paths for three-axis surface machining
CN105116840A (en) Compensation method for slowly varying error of primary interpolation of space curve
CN109725595A (en) Compensation method, processing method and the workpiece of the machining path of workpiece

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: 20181113

Termination date: 20201230