Dynamic correction of servo following errors in a computer-numerically controlled system and fixed cycle utilizing same

• US 5,005,135 A
• Filed: 03/22/1989
• Issued: 04/02/1991
• Est. Priority Date: 03/22/1989
• Status: Expired due to Term

• Current Assignee: Siemens Energy & Automation Incorporated (Siemens AG)
• Original Assignee: Cincinnati Machines Incorporated (Fives SA)
• Inventors: Gildemeister, Walter M., Farmer, David M., Morser, Alfred H.
• Primary Examiner(s): Smith, Jerry
• Assistant Examiner(s): GORDON, PAUL P
• Application Number:
  US07/327,324
• Time in Patent Office: 741 Days
• Field of Search: 364/474.29, 364/474.30, 364/474.31, 364/167.01, 364/172, 364/474.28, 364/474.35, 408/12, 408/13, 318/571-573
• US Class Current: 700/193
• CPC Class Codes: G05B 19/373 with speed feedback only
• CPC Class Codes: G05B 2219/33119 Servo parameters in memory, configuration of control parameters
• CPC Class Codes: G05B 2219/33338 DNC distributed, decentralised nc, concurrent, multiprocessing
• CPC Class Codes: G05B 2219/34206 Motion controller independent from nc, lmc local motor controller
• CPC Class Codes: G05B 2219/34419 Structure of control system
• CPC Class Codes: G05B 2219/35245 Expansion of control words, code of standard language to increase functionality
• CPC Class Codes: G05B 2219/35263 Using variables, parameters in program, macro, parametrized instruction
• CPC Class Codes: G05B 2219/35279 Ignoring invalid program
• CPC Class Codes: G05B 2219/35287 Verify, check program by drawing, display part, testpiece
• CPC Class Codes: G05B 2219/35294 Display concentric circles
• CPC Class Codes: G05B 2219/35373 Data storage, buffer
• CPC Class Codes: G05B 2219/35394 A separate processor for block, span
• CPC Class Codes: G05B 2219/36168 Touchscreen
• CPC Class Codes: G05B 2219/36395 Load local computer program from host, data transfer ram to rom, BTR
• CPC Class Codes: G05B 2219/37619 Characteristics of machine, deviation of movement, gauge,
• CPC Class Codes: G05B 2219/41113 Compensation for path radius
• CPC Class Codes: G05B 2219/41192 Compensation for different response times, delay of axis
• CPC Class Codes: G05B 2219/41219 To compensate path, track error, calculate, use compensated reference
• CPC Class Codes: G05B 2219/42062 Position and speed and current
• CPC Class Codes: G05B 2219/42152 Learn, self, auto tuning, calibrating, environment adaptation, repetition
• CPC Class Codes: G05B 2219/43199 : Safety, limitation of feedrate
• CPC Class Codes: G05B 2219/45215 : Thread cutting
• CPC Class Codes: G05B 2219/45216 : Tapping
• CPC Class Codes: G05B 2219/49376 : Select two machining types, milling or turning, complete machining with one tool
• CPC Class Codes: G05B 2219/50109 : Soft approach, engage, retract, escape, withdraw path for tool to workpiece
• CPC Class Codes: G05B 2219/50113 : Short stroke, retract tool, safe distance from workpiece surface, hover height
• CPC Class Codes: G05B 2219/50208 : Retrace, remachine portion of path, locus to remove start discontinuities
• CPC Class Codes: Y10T 409/30056 : with planetary cutter

Abstract

The invention relates to servo-driven computer-numerically-controlled systems of the type adapted to receive part program instructions defining a desired path of relative movement between a tool and a workpiece, wherein the path may include an interior or exterior curved portion to be effected by coordinated linear movement of machine members along at least two orthogonal linear axes. The invention provides apparati and methods for correcting path radius errors to facilitate rapid and accurate movement along the curve. In a preferred embodiment, such path radius correction is applied to a fixed cycle for machining inside circles preferably incorporating such path radius correction and providing substantially tangential engagement between the tool and a machining locus orbited by the tool to avoid abrupt accelerations or decelerations while the tool is in contact with the workpiece. In addition to avoiding surface blemishes, this facilitates machining a broader range of hole sizes with a given sized tool thereby reducing the need for frequent tool changes. The invention carries out path radius correction by generating position commands received by the servo using corrected radius data, the difference between which and the desired radius to be machined compensates for at least a portion of the path radius error that would otherwise be generated by the servo. Apparatus and methods for threading holes using a non-helical threading tools with or without path radius correction are also disclosed.

Claims

1. A method of correcting path radius errors in a computer numerically controlled system of the type adapted to receive program instructions defining a desired path of relative movement to be effected between a workpiece and a tool by motion of machine members along at least two orthogonal linear axes at a feedrate, (F) under control of a servo which receives position commands based on said instructions, said servo having at least one of, a position loop gain, (K_v) and a velocity loop integral time, (T_i), said path including a curved portion to be executed by effecting coordinated linear movement along said axes, said method comprising the steps of:

(a) receiving an instruction defining a desired radius, (R) of said curved portion;

(b) generating corrected radius data, (R2) to compensate for servo following errors appearing as path radius errors along said curved portion of said path such that the difference between the desired radius, (R) and said corrected radius data, (R2) compensates for at least a portion of the path radius error that would otherwise be induced in the movement by the servo, and

(c) generating the position commands in response to said corrected radius data whereby the actual relative movement between the workpiece and the tool more closely follows said curved portion of said desired path.

2. The method of claim 1 wherein said corrected radius data, (R2) is generated substantially in accordance with the expression:

space="preserve" listing-type="equation">R2=R+Q-S

where;

space="preserve" listing-type="equation">Q=F.sup.2 /2R K.sub.v.sup.2, and

space="preserve" listing-type="equation">S=2Q T.sub.i K.sub.v.

3. The method of claim 1 wherein said corrected radius data, (R2) is generated substantially in accordance with the expression:

space="preserve" listing-type="equation">R2=R+Q-S+U

where;

space="preserve" listing-type="equation">Q=F.sup.2 /2R K.sub.v.sup.2

space="preserve" listing-type="equation">S=2Q T.sub.i K.sub.v, and

space="preserve" listing-type="equation">U=Q(T.sub.i F/R).sup.2.

4. The method of claim 1 further comprising the step of carrying out the steps of said method by means of a fixed cycle, the execution of which is invoked by a single, parameterized program instruction.

5. The method of claim 1 further comprising the step of adjusting the value of T_i for at least one of said axes such that said servo will execute said relative movement along a curve substantially parallel to said curved portion of said path.

6. The method of claim 5 wherein said adjusting step includes the steps of:

(a) using said system to run a first program commanding execution of a first circular path of a first commanded radius at a first commanded feedrate and centered at a given point to determine a first actual curve;

(b) using said system to run a second program commanding execution at a second commanded feedrate of a second circular path of said first commanded radius centered at said point to determine a second actual path, second commanded feedrate differing from said first commanded feedrate, and

(c) determining whether said first actual curve and said second actual paths lie substantially concentric with one another and, if not, adjusting the value of T_i for at least one of said axes.

7. The method of claim 6 further comprising the steps of repeating steps (a), (b) and (c) until said first actual curve and said second actual curve lie substantially concentric with one another.

8. The method of claim 6 further comprising the steps of forming a graphical representation of said first and second actual curves and/or the difference, if any, between said first and second curves at angularly corresponding points.

9. The method of claim 8 wherein said graphical representation is formed using a roundness measuring instrument.

10. The method of claim 8 wherein said graphical representation is formed by electronically generating display data correlated to said first and second actual curves, respectively.

11. The method of claim 2 further comprising the step of determining said integral time factor, (T_i) of a servo in a computer numerically controlled system of the type adapted to receive program instruction specifying a desired curved path of relative movement to be effected between a workpiece and a tool by coordinated linear motion of machine members along at least two orthogonal axes at a feedrate, (F) under control of the servo in response to position commands based on said instructions, said servo having in addition to said integral time factor, (T_i) a position loop gain, (K_v), said method comprising the steps of:

(a) setting the values of K₄ for each of said axes to equal, known values;

(b) adjusting the value of T_i for at least one of said axes such that said servo will execute said relative movement along a substantially time circular arc concentric with said desired curved path;

(c) determining a path radius error, (e) due to said integral term, (T_i), and

(d) determining the value of T_i substantially in accordance with the expression;

space="preserve" listing-type="equation">T.sub.i =K.sub.v /2=(E*K.sub.v *R/F.sup.1/2)

where;

R represents the radius of said desired curved path.

12. A method of determining the integral time factor, (T_i) of a servo in a computer numerically controlled system of the type adapted to receive program instructions specifying a desired curved path of relative movement to be effected between a workpiece and a tool by coordinated linear motion of machine members along at least two orthogonal axes at a feedrate, (F) under control of the servo in response to position commands based on said instructions, said servo having in addition to said integral time factor, (T_i), a position loop gain, (K_v), said method comprising the steps of:

(a) setting he values of K_v for each of said axes to equal, known values;

(b) adjusting the value of T_i for at least one of said axes such that said servo will execute said relative movement along a substantially true circular arc concentric with said desired curved path;

(c) determining a path radius error, (E) due to said integral term, (T_i), and

(d) determining the value of T_i substantially in accordance with the expression;

space="preserve" listing-type="equation">T.sub.i =K.sub.v /2-(E*K.sub.v *R/VF.sup.1/2)

where;

R represents the radius of said desired curved path.

13. A method of correcting path radius errors in a computer numerically controlled system of the type adapted to receive program instructions defining a desired path of relative movement between a workpiece and a tool to be effected by motion of machine members along at least two orthogonal linear axes at a desired feedrate, (F) under control of a servo which receives position commands based on said instruction, said path including a curved portion to be executed by effecting coordinated linear movement along said axes, said servo having at least one of, a position loop gain, (K_v) and a velocity loop integral time, (T_i), said method comprising the steps of:

(a) receiving an instruction defining a desired radius, (R) of said curved portion;

(b) determining a feedrate limit, (F_L);

(c) generating corrected radius data, (R2) to compensate for servo following error along said curved portion, said corrected radius data (R2) being generated based on a limited feedrate, (F_active), whose magnitude does not significantly exceed said feedrate limit, (F_L), and

(d) generating the position commands in responses to said corrected radius data whereby the actual relative movement between the workpiece and the tool more closely follows said curved portion of said desired path.

14. The method of claim 13 wherein said corrected radius data, (R2) is generated substantially in accordance with the expression:

space="preserve" listing-type="equation">R2=R+Q.sub.L -S.sub.L

where;

space="preserve" listing-type="equation">Q.sub.al =F.sub.active.sup.2 /2R K.sub.v.sup.2, and

space="preserve" listing-type="equation">S.sub.L =2Q.sub.L T.sub.i K.sub.v.

15. The method of claim 13 wherein said corrected radius data, (R2) is generated substantially in accordance with the expression:

space="preserve" listing-type="equation">R2=R+Q.sub.L -S.sub.L +U.sub.L

where;

space="preserve" listing-type="equation">Q.sub.L =F.sub.active.sup.2 /2R K.sub.v.sup.2

space="preserve" listing-type="equation">S.sub.L =2Q.sub.L T.sub.i K.sub.v, and

space="preserve" listing-type="equation">U.sub.L =Q.sub.L (T.sub.i F.sub.active /R).sup.2.

16. The method of claim 13 wherein said limited feedrate, (F_active) is selected to substantially equal the lesser of:

(a) said feedrate limit, (F_L), and

(b) the desired feedrate, (F).

17. The method of claim 13 wherein said feedrate limit, (F_L) is determined substantially in accordance with the expression:

space="preserve" listing-type="equation">F.sub.L =0.10K.sub.v R.sup.1/2.

18. A method of machining holes in a workpiece using a tool, said method comprising the steps of:

(a) positioning the tool interiorly of a bore previously formed in the workpiece;

(b) moving the tool to substantially tangentially engage a closed locus of points defining a desired path to be machined;

(c) orbiting the tool at least 360 degrees around said locus to machine a hole of a desired size from said bore, and

(d) moving the tool to substantially tangentially disengage said tool from substantial coincidence with said locus.

19. The method of claim 18 further comprising the step of accelerating said tool to a desired orbital feedrate as it is moved from the interior of bore into said tangential engagement.

20. The method of claim 18 further comprising the step of decelerating said tool from a desired orbital feedrate after said tool is moved to substantially tangentially disengage said locus.

21. The method of claim 18 further comprising the step of continuing said orbiting step beyond said 360 degrees prior to execution of said disengaging step to facilitate removal of any significant discontinuity in the machined surface of the workpiece.

22. The method of claim 18 wherein said closed locus of points is a circle.

23. The method of claim 18 further comprising the step of carrying out the steps of said method by means of a fixed cycle in a computer numerically controlled system, the execution of said fixed cycle being invoked by a single parameterized program instruction.

24. A method of machining holes in a workpiece with correction of path radius errors for use in a computer numerically controlled system of the type adapted to receive program instructions defining a desired path of relative movement to be effected by motion of machine members along at least two orthogonal linear axes between a workpiece and a tool at a feedrate, (F) under control of a servo which receives position commands based on said instructions, said path including a curved portion to be executed by effecting coordinated linear movement along said axes, said servo having at least one of, a position loop said method comprising the steps of:

(a) receiving data defining at least X and Y coordinates of an interior location of a hole to be machined, a desired feedrate, (F), and the radius, (R) of a desired path to be traversed by the tool in order to machine a hole of a given size;

(b) generating corrected radius data (R2) to compensate for servo following errors appearing as path radius errors along said curved portion of said path so that the difference between the desired radius, (R) and the corrected radius data, (R2) compensates for at least a portion of the path radius error that would otherwise be induced in the movement by the servo;

(c) generating tangential engagement data for defining a second path for moving said tool to substantially tangentially engage said desired path;

(d) generating tangential disengagement data for defining a third path for moving said tool to substantially tangentially disengage said desired path;

(e) moving said tool to a particular location interiorly of a bore in accordance with at least said coordinates;

(f) moving said tool in accordance with . said tangential engagement data along said second path into substantially tangential coincidence with said desired path;

(g) orbiting said tool at least about 360 degrees around said desired path in accordance with said corrected radius data to machine said hole to said given size, and

(h) moving said tool in accordance with said tangential disengagement data along said third path to substantially tangentially disengage said tool from the surface of the workpiece.

25. The method of claim 24 wherein said corrected radius data, (R2) is generated substantially in accordance with the expression:

space="preserve" listing-type="equation">R2=R+Q.sub.L -S.sub.L

where;

space="preserve" listing-type="equation">Q.sub.L =F.sub.active /2R K.sub.v.sup.2

space="preserve" listing-type="equation">S.sub.L =2Q.sub.L T.sub.i K.sub.v, and

F_active is a limited feedrate which does not significantly exceed said desired feedrate, F.

26. The method of claim 25 wherein at least one of said tangential engagement data in said tangential disengagement data define an arc whose radius, R1 is determined substantially in accordance with the expression:

space="preserve" listing-type="equation">R1=R/2+2Q.sub.L -2S.sub.L.

27. The method of claim 24 wherein said corrected radius data, (R2) is generated substantially in accordance with the expression:

space="preserve" listing-type="equation">R2=R+Q.sub.L -S.sub.L +U.sub.L

where;

space="preserve" listing-type="equation">Q.sub.L =F.sub.active /2R K.sub.v.sup.2

space="preserve" listing-type="equation">S.sub.L =2Q.sub.L T.sub.i K.sub.v

space="preserve" listing-type="equation">U.sub.L =Q.sub.L (T.sub.i F/R).sup.2, and

F_active is a limited feedrate which does not significantly exceed said desired feedrate, F.

28. The method of claim 27 wherein said coordinates define the center of the hole and wherein in step (e) of said method, said particular interior location is offset from said center by a distance, (D) determined substantially in accordance with the expression:

space="preserve" listing-type="equation">D=ABS

D =ABS [R2-Rl]

wherein R1 is determined substantially in accordance with the expression;

space="preserve" listing-type="equation">R1=R/2+2Q.sub.L -2S.sub.L.

29. The method of claim 24 wherein at least said orbiting step is substantially carried out at substantially the desired feedrate, (F).

30. The method of claim 24 wherein at least said orbiting step is substantially carried out at a limited feedrate, (F_active) which does not substantially exceed the desired feedrate, (F).

31. The method of claim 30 wherein said limited feedrate, (F_active) is selected to substantially equal the lesser of:

(a) a feedrate limit, (F_L), and

(b) the desired feedrate, (F).

32. The method of claim 31 wherein said feedrate limit, (F_L) is determined substantially in accordance with the expression:

space="preserve" listing-type="equation">F.sub.L =0.10K.sub.v R.sup.1/2.

33. The method of claim 24 further comprising the steps of carrying out the steps of said method by means of a fixed cycle, the execution of which is invoked by a single, parameterized program instruction.

34. The method of claim 24 further comprising the steps of repeating the steps of said method to machine a second hole and wherein the tool used to machine both said hole and said second hole is the same tool, said hole and said second hole being of substantially different sizes whereby a plurality of holes of different sizes may be machined using a tool of a given size.

35. A method of machining holes in a workpiece using a non-helical threading tool, said method comprising the steps of:

(a) positioning the tool interiorly of a bore previously formed in the workpiece;

(b) moving the tool into substantially tangential coincidence with a locus of points defining a desired circular path to be machined;

(c) orbiting the tool around said locus while simultaneously moving the tool in a direction parallel to the longitudinal axis of said bore at a rate appropriate to form threads of a desired pitch int he hole, and

(d) moving the tool to substantially tangentially disengage said tool from the surface of the workpiece.

36. A method of forming threaded holes in a workpiece with correction of path radius errors for use in a computer numerically controlled system of the type adapted to receive program instructions defining a desired path of relative movement between a workpiece and a rotating non-helical threading tool to be effected by motion of machine members along at least three orthogonal axes at a feedrate, (F) under control of a servo which receives position commands based on said instructions, said path including a curved portion to be executed by carrying out coordinated linear movement along at least two of said axes, said servo having at least one of, a position loop gain, (K_v) and an integral time, (T_i), said method comprising the steps of:

(a) receiving data defining at least X and Y interior coordinates of a hole to be threaded, a desired feedrate, (F), and the radius, (R) of a desired path to be traversed by the tool in order to thread the hole;

(b) generating corrected radius data (R2) for driving said servo to compensate for servo following errors appearing as path radius errors along said curved portion of said path so that the difference between the desired radius, (R) and the corrected radius data, (R2) compensates for at least a portion of the path radius error that would otherwise be induced in the movement by the servo;

(c) generating tangential engagement data for defining a second path for moving said tool to substantially tangentially engage with said desired path;

(d) generating tangential disengagement data for defining a third path for moving said tool to substantially tangentially disengage said desired path;

(e) moving said tool to a location interiorly of the hole in accordance with at least said X and Y coordinates;

(f) moving said tool in accordance with said tangential engagement along said second path into substantially tangential coincidence with said desired path;

(g) orbiting the tool around said desired path in accordance with said corrected radius data while simultaneously moving the tool in a direction parallel to the longitudinal axis of the hole at a rate appropriate to form threads of a desired pitch in the hole, and

(h) moving said tool in accordance with said tangential disengagement data along said third path to substantially tangentially disengage said tool from the surface of the workpiece.

37. The method of claim 36 wherein at least said orbiting step is substantially carried out at substantially the desired feedrate, (F).

38. The method of claim 36 wherein at least said orbiting step is substantially carried out at a limited feedrate, (F_active) which does not substantially exceed the desired feedrate, (F).

39. The method of claim 38 wherein said limited feedrate, (F_active) is selected to substantially equal the lesser of:

(a) a feedrate limit, (F_L), and

(b) the desired feedrate, (F).

40. The method of claim 39 wherein said corrected radius data, (R2) is generated substantially in accordance with the expression:

space="preserve" listing-type="equation">R2=R+Q-S

where;

space="preserve" listing-type="equation">Q=F.sup.2 /2R K.sub.v.sup.2, and

space="preserve" listing-type="equation">S=2Q T.sub.i K.sub.v.

41. The method of claim 39 wherein said corrected radius data, (R2) is generated substantially in accordance with the expression:

space="preserve" listing-type="equation">R2=R+Q-S+U

where;

space="preserve" listing-type="equation">Q=F.sup.2 /2R K.sub.v.sup.2

space="preserve" listing-type="equation">S=2Q T.sub.i K.sub.v, and

space="preserve" listing-type="equation">U=Q(T.sub.i F/R).sup.2.

42. The method of claim 39 wherein said feedrate limit, (F_L) is determined substantially in accordance with the expression:

space="preserve" listing-type="equation">F.sub.L =0.10 K.sub.v R.sup.1/2.

43. The method of claim 36 further comprising the step of repeating the steps of said method to thread a second hole and wherein the tool used to thread both said hole and said second hole is the same tool, said hole and said second hole being of substantially different diameter whereby a plurality of holes of different diameter may be threaded using a tool of a given size.

44. The method of claim 36 further comprising the steps of carrying out the steps of said method by means of a fixed cycle, the execution of which is invoked by a single, parameterized program instruction.

45. An apparatus for correcting path radius errors in a computer numerically controlled system of the type adapted to receive program instructions defining a desired path of relative movement to be effected by motion of machine members along at least two orthogonal linear axes between a workpiece and a tool at a feedrate, (F) under control of a servo which receives position commands based on said instructions, said path including a curved portion to be executed by effecting coordinated linear movement along said axes, said servo having at least one of, a position loop gain, (K_v) and a velocity loop integral time, (T_i), said apparatus comprising:

(a) input means for receiving program instructions including an instruction defining a desired radius, (R) of said curved portion, and

(b) compensation means connected to said input means for generating corrected radius data, (R2) to compensate for servo following errors appearing as path radius errors along said curved portion of said path such that the difference between the desired radius, (R) and said corrected radius data, (R2) compensates for at least a portion of the path radius error that would otherwise be induced in the movement by the servo, said compensation means also being connected to said servo so that said servo receives position commands correlated to said corrected radius data whereby the actual relative movement between the workpiece and the tool more closely follows said curved portion of said desired path.

46. The apparatus of claim 45 wherein said corrected radius data, (R2) is generated substantially in accordance with the expression:

space="preserve" listing-type="equation">R2=R+Q-S

where;

space="preserve" listing-type="equation">Q=F.sup.2 /2R K.sub.v.sup.2, and

space="preserve" listing-type="equation">S=2Q T.sub.i K.sub.v.

47. The apparatus of claim 45 wherein said corrected radius data, (R2) is generated substantially in accordance with the expression:

space="preserve" listing-type="equation">R2=R+Q-S+U

where;

space="preserve" listing-type="equation">Q=F.sup.2 /2R K.sub.v.sup.2

space="preserve" listing-type="equation">S=2Q T.sub.i K.sub.v, and

space="preserve" listing-type="equation">U=Q(T.sub.i F/R).sup.2.

48. The apparatus of claim 45 further comprising means for carrying out said compensation by means of a fixed cycle, the execution of which system is invoked by a single, parameterized program instruction.

49. An apparatus for correcting path radius errors in a computer numerically controlled system of the type adapted to receive program instructions defining a desired path of relative movement to be effected between a workpiece and a tool by motion of machine members along at least two orthogonal linear axes at a desired feedrate, (F) under control of a servo which receives position commands based on said instructions, said path including a curved portion to be executed by effecting coordinated linear movement along said axes, said servo having at least one of, a position loop gain, (K_v) and a velocity loop integral time, (T_i), said apparatus comprising:

(a) input means for receiving an instruction defining a desired radius, (R) of said curved portion;

(b) feedrate limiting means for determining a feedrate limit, (F_L), and

(c) compensation means connected to said input means and said feedrate limiting means for generating corrected radius data, (R2) using a limited feedrate, (F_active), whose magnitude does not significantly exceed said feedrate limit, (F_L), said compensation means also being connected to said servo so that said servo receives position commands correlated to said corrected radius data whereby the actual relative movement between the workpiece and the tool more closely follows said curved portion of said desired path.

50. The apparatus of claim 49 wherein said corrected radius data, (R2) is generated substantially in accordance with the expression:

space="preserve" listing-type="equation">R2=R+Q-S

where;

space="preserve" listing-type="equation">Q=F.sub.active.sup.2 /2R K.sub.v.sup.2, and

space="preserve" listing-type="equation">S=2Q T.sub.i K.sub.v.

51. The apparatus of claim 49 wherein said corrected radius data, (R2) is generated substantially in accordance with the expression:

space="preserve" listing-type="equation">R2=R+Q-S+U

where;

space="preserve" listing-type="equation">Q=F.sub.active.sup.2 /2R K.sub.v.sup.2

space="preserve" listing-type="equation">S=2Q T.sub.i K.sub.v, and

space="preserve" listing-type="equation">U=Q(T.sub.i F.sub.active /R).sup.2.

52. An apparatus for machining holes in a workpiece using a tool, said apparatus comprising:

(a) means for positioning the tool interiorly of a bore previously formed int he workpiece;

(b) means for moving the tool to substantially tangentially engage a closed locus of points surrounding said bore, said locus defining a desired path to be machined;

(c) means for orbiting the tool at least 360 degrees around said locus to machine a hole of a desired size from said bore, and

(d) means for moving the tool to substantially tangentially disengage said tool from said locus.

53. The apparatus of claim 52 further comprising means for continuing said orbiting step beyond said 360 degrees prior to execution of said disengaging step to facilitate removal of any significant discontinuity in the machined surface of the workpiece.

54. The apparatus of claim 52 further comprising means for carrying out said positioning, engaging, orbiting and disengaging by means of a fixed cycle, the execution of which is invoked by a single parameterized program instruction.

55. An apparatus for machining holes in a workpiece with correction of path radius errors for use in a computer numerically controlled system of the type adapted to receive program instructions defining a desired path of relative movement between a workpiece and a tool to be effected by motion of machine members along at least two orthogonal linear axes at a feedrate, (F) under control of a servo which receives position commands based on said instructions, said path including a curved portion to be executed by effecting coordinated linear movement along said axes, said servo having at least one of, a position loop gain, (K_v) and a velocity loop integral time, (T_i), said apparatus comprising:

(a) input means for receiving data defining an interior location of a bore, a desired feedrate, (F), and the radius, (R) of a desired path to be traversed by the tool in order to machine said bore to a hole of a given size;

(b) processor means means for;

(i) generating corrected radius data (R2) to compensate for servo following errors appearing as path radius errors along said curved portion of said path so that the difference between the desired radius, (R) and the corrected radius data, (R2) compensates for at least a portion of the path radius error that would otherwise be induced in the movement by the servo;

(ii) generating tangential engagement data for defining a second path for moving said tool to substantially tangentially engage with said desired path;

(iii) generating tangential disengagement data for defining a third path for moving said tool to substantially tangentially disengage said desired path, and

(c) means connected to said processor means for sequentially;

(i) moving said tool interiorly of said bore in accordance with said coordinates;

(ii) moving said tool in accordance with said tangential engagement data along said second path into substantially tangential coincidence with said desired path;

(iii) orbiting said tool at least about 360 degrees around said desired path in accordance with said corrected radius data to machine said hole to said given size, and

(iv) moving said tool in accordance with said tangential disengagement data along said third path to substantially tangentially disengage said tool from the surface of the workpiece.

56. The apparatus of claim 55 wherein said corrected radius data, (R2) is generated substantially in accordance with the expression:

space="preserve" listing-type="equation">R2=R+Q-S+U

where;

space="preserve" listing-type="equation">Q=F.sup.2 /2R K.sub.v.sup.2

space="preserve" listing-type="equation">S=2Q T.sub.i K.sub.v, and

space="preserve" listing-type="equation">U=Q(T.sub.i F/R).sup.2.

57. The apparatus of claim 55 further comprising means for carrying out the said generation of said corrected radius data by means of a fixed cycle, the execution of which is invoked by a single, parameterized program instruction.