Adaptive control system for an internal combustion engine

• US 4,841,933 A
• Filed: 12/29/1987
• Issued: 06/27/1989
• Est. Priority Date: 01/14/1987
• Status: Expired due to Fees

• Current Assignee: Lucas Industries Public Limited Company Well Street Birmingham B19 2XF England
• Original Assignee: Lucas Industries Limited (Zeppelin - Stiftung der Stadt Friedrichshafen)
• Inventors: McHale, Anthony, Frith, Andrew P.
• Primary Examiner(s): Nelli, Raymond A.
• Application Number:
  US07/139,301
• Time in Patent Office: 546 Days
• Field of Search: 123/417, 123/419, 123/436, 123/415, 123/416, 123/418, 364/431.05, 364/431.04
• US Class Current: 477/111
• CPC Class Codes: F02D 41/0087 Selective cylinder activation, i.e. partial cylinder operation deceleration cut-off F02D41/123
• CPC Class Codes: F02D 41/1408 Dithering techniques
• CPC Class Codes: F02P 5/1455 by using a second control of the closed loop type dependent on pinking F02P5/152
• CPC Class Codes: F02P 5/1504 with particular means during a transient phase, e.g. acceleration, deceleration, gear change during starting F02P5/1506
• CPC Class Codes: F02P 5/151 with means for compensating the variation of the characteristics of the engine or of a sensor, e.g. by ageing
• CPC Class Codes: Y02T 10/40 Engine management systems

Abstract

An adaptive control system and method for a multi-cylinder internal combustion engine is provided wherein a perturbation generator perturbs an engine control parameter of a cylinder about a base-line value, and a measuring means measures the slope of an engine output with respect to perturbations in the engine control parameter caused by the perturbation generator. A correction unit employs the measured slope to correct at least one engine control parameter of the engine so as to obtain a desired value of the slope measured by the measuring means. The corrected control parameter can be the same or different from the perturbed control parameter. The perturbation generator operates in a first perturbation mode in an upper speed range of the engine and in a second perturbation mode in a lower speed range of the engine. The slope measuring unit operates in different measurement modes corresponding to these perturbation modes.

Claims

1. An adaptive control system for a power producing engine having at least one engine control parameter affecting an engine output, said engine having a drive train combination having at least one resonant frequency, said control system comprising:

(a) a perturbation generator for perturbing intermittently a particular said engine control parameter about a base line value in at least one perturbation mode in a given operating mode of said engine which includes said at least one resonant frequency;

(b) measuring means for measuring a slope of said engine output with respect to said particular control parameter caused by said perturbation generator; and

(c) control means, responsive to said slope, for controlling one said engine control parameter so as to obtain a desired value of said slope, wherein said perturbation generator operates in another perturbation mode in another operating mode of said engine to perturb said particular control parameter at a frequency greater than said at least one resonant frequency.

2. The system as in claim 1, wherein said engine is an internal combustion engine and said perturbation generator in said at least one perturbation mode (a) perturbs said particular control parameter with a first perturbation, (b) permits a predetermined period to elapse without perturbing said particular control parameter, (c) perturbs said particular control parameter with a second perturbation of opposite polarity to that of said first perturbation, and (d) permits another predetermined period to elapse without perturbing said particular engine control parameter.

3. The system as in claim 2, wherein said another operating mode is an upper speed range of said engine and said given operating mode is a lower speed range of said engine.

4. The system as in claim 1, wherein said particular control parameter and said one control parameter are the same.

6. The system as in claim 2, wherein said measuring means in a measurement mode corresponding to said at least one perturbation mode creates a series of measurement windows following each perturbation of said particular control parameter, each of said series of measurement windows occupying part of an interval between successive perturbations of said particular control parameter, said measuring means calculating said slope in accordance with a change in engine output between adjacent ones of said series of measurement windows.

7. The system as in claim 2, wherein said perturbation generator in said another perturbation mode generates a periodic perturbation waveform having said frequency greater than said resonant frequency and applies a first perturbation to said particular control parameter during a first part of each period of said waveform and a second perturbation of opposite polarity to that of said first perturbation to said particular control parameter during a second part of each period of said waveform.

8. The system as in claim 7, wherein said measuring means in a measurement mode corresponding to said another perturbation mode creates a series of contiguous first and second measurement windows associated respectively with said first part and said second part of said period of said perturbation waveform, each of said measurement windows in said series lagging its associated part of said period of said perturbation waveform by a predetermined phase shift.

9. The system as in claim 2, further comprising cylinder combination selection means for establishing a plurality of cylinder combinations of said engine and for selecting each combination in turn, each of said cylinder combinations comprising at least one cylinder, said perturbation generator perturbing in both said at least one perturbation mode and said another perturbation mode each of said cylinder combinations in turn at the time it is selected by said selection means, said measuring means measures said slope for each of said cylinder combinations in turn, and said correction means corrects at least one said control parameter for each cylinder combination in turn.

5. An adaptive control system for a power producing engine having at least one engine control parameter affecting an engine output, said engine having a drive train combination having at least one resonant frequency, said control system comprising:

(a) a perturbation generator for perturbing intermittently a particular said engine control parameter about a base line value in at least one perturbation mode in a given operating mode of said engine which includes said at least one resonant frequency;

(b) measuring means for measuring a slope of said engine output with respect to said particular control parameter caused by said perturbation generator; and

(c) control means, responsive to said slope, for controlling one said engine control parameter so as to obtain a desired value of said slope, wherein said particular control parameter and said one control parameter are different.

10. An adaptive control system for a multi-cylinder internal combustion engine having at least one engine control parameter affecting an engine output, said control system comprising:

(a) cylinder combination selection means for establishing a plurality of combinations of cylinders of said engine and for selecting each combination in turn, each of said combinations of cylinders including at least one cylinder;

(b) a perturbation generator for perturbing a particular said engine control parameter of each of said combinations of cylinders at the time it is selected by said cylinder combination selection means, said perturbation generator operating in a first perturbation mode in an upper speed range of said engine and in a second perturbation mode in a lower speed range of said engine;

(c) measuring means for measuring a slope or differential of said engine output with respect to perturbations in said particular engine control parameter caused by said perturbation generator for each of said combinations in turn, said measuring means operating in a first measurement mode corresponding to said first perturbation mode and a second measurement mode corresponding to said second perturbation mode; and

(d) correction means, responsive to said slope, for correcting at least one said control parameter for each of said combinations of cylinders of said engine so as to obtain a desired value of said slope.

11. The system as in claim 10, wherein (i) said perturbation generator in said first perturbation mode generates a periodic perturbation waveform and applies a first perturbation to said particular control parameter during a first part of each period of said perturbation waveform and a second perturbation of opposite polarity to that of said first perturbation to said particular control parameter during a second part of each period of said perturbation waveform, (ii) said perturbation generator in said second perturbation mode applies a third perturbation to said particular control parameter, permits a predetermined period to elapse without perturbing said particular control parameter, applies a fourth perturbation of opposite polarity to that of said third perturbation to said particular control parameter, and permits another predetermined period to elapse without perturbing said particular control parameter, (iii) said measuring means in said first measurement mode creates a first series of contiguous first and second measurement windows associated respectively with said first part and said second part of said period of said perturbation waveform, each of said measurement windows in said first series lagging its associated part of said period of said perturbation waveform by a predetermined phase shift, said measuring means calculating said slope in accordance with a change in engine output between contiguous ones of said measurement windows in said first series, and (iv) said measuring means in said second measurement mode creates a second series of measurement windows following each perturbation of said particular control parameter, each of said second series of measurement windows occupying part of an interval between successive perturbations of said particular control parameter, said measuring means calculating said slope in accordance with a change in engine output between adjacent ones of said second series of measurement windows.

12. The system as in claim 11, wherein said internal combustion engine includes a flywheel, a resilient shaft means connected to said flywheel, and a gear means connected to said shaft means;

said flywheel, said shaft means and said gear means forming a resonant system having a particular resonant frequency for each gear ratio of said gear means, and wherein said periodic perturbation waveform is caused to have a frequency greater than a highest resonant frequency of said resonant system when said engine is in said upper speed range and each measurement window in said second series of measurement windows is equal to a whole number of quarters of said resonant frequency of said resonant system corresponding to a current gear ratio of said gear means.

13. The system as in claim 11, wherein in both said first measurement mode and said second measurement mode said measuring means accumulates respectively during each window of said first series of measurement windows and said second series of measurement windows the fire periods having central points which fall within each window to produce a total fire period for each window, said measuring means calculating said slope in accordance with said total fire period for each window.

14. The system as in claim 10 or 11, wherein said perturbation generator operates in a third perturbation mode when one of (i) said engine is in neutral and (ii) a clutch associated with said engine is disengaged, and said measuring means operates in a third measurement mode corresponding to said third perturbation mode.

15. The system as in claim 10 or 11, wherein each of said combinations comprises a single cylinder.

16. The system as in claim 10 or 11, wherein each of said cylinder combinations comprises all cylinders of said engine except one.

17. The system as in claim 10 or 11, further comprising means for establishing a value of said at least one control parameter prior to correction by said correction means as a function of engine output and load on said engine.

18. The system as in claim 10 or 11, wherein said particular control parameter perturbed by said perturbation means is an ignition timing parameter.

19. The system as in claim 10 or 11, wherein a single control parameter is corrected by said correction means and both said particular control parameter perturbed by said perturbation means and said control parameter corrected by said correction means are an ignition timing parameter.

20. The system as in claim 10 or 11, wherein said particular control parameter perturbed by said perturbation means is an ignition timing parameter and said control parameter corrected by said correction means is a single engine fuel control parameter.

21. The system as in claim 10 or 11, wherein said particular control parameter perturbed by said perturbation means is an ignition timing parameter and said correction means corrects two said control parameters comprising an ignition timing parameter and an engine fuel control parameter.

22. An adaptive control system for a multi-cylinder, fuel injected, spark ignition, internal combustion engine comprising a flywheel, a resilient shaft connected to said flywheel, a gear means connected to said resilient shaft and a crankshaft, said engine having an engine output affected by at least one control input, said control system comprising:

(a) a position transducer for producing a series of reference pulses representing rotational positions of said crankshaft;

(b) a control means, responsive to said position transducer, for providing output signals for controlling at least one said control input;

(c) an engine speed calculation means, responsive to said position transducer, for providing an output signal indicating engine speed to said control means;

(d) cylinder synchronization means, responsive to said position transducer, for determining which cylinder is undergoing a combustion stroke;

(e) gear indication means for indicating which gear of said engine is presently engaged;

(f) load demand transducer means for sensing a load demand parameter of said engine;

(g) fire period calculation means, responsive to said position transducer, for calculating a period which elapses between pistons in consecutive cylinders of said engine being at a given angular position after top dead center;

(h) a first memory means storing data representing a particular control input of said engine as a function of engine speed and load demand;

(i) a first calculation means, responsive to (i) said engine speed calculation means, (ii) said load demand transducer and (iii) said first memory means, for calculating a basic value for said particular control input corresponding to prevailing engine speed and load demand;

(j) a second memory means storing data representing a second control input of said engine as a function of engine speed and load demand;

(k) a second calculation means, responsive (i) said engine speed calculation device, (ii) said load demand transducer, and (iii) said second memory means, for calculating a basic value for said second control input corresponding to prevailing engine speed and load demand;

(l) perturbation means, responsive to (i) said gear indication means, (ii) said fire period calculation means, and (iii) said cylinder synchronization means, for operating in at least one perturbation mode in a given operating mode of said engine including a highest resonant frequency of a resonant system comprising said flywheel, said resilient shaft means and said gear means in an lower speed range of said engine perturbing said particular control input to each cylinder of said engine in synchronization with the time it is undergoing a combustion stroke at an intermittent frequency which is a function of outputs from said gear determination means and said fire period calculation means;

(m) measuring means for sensing a slope in said engine output with respect to said particular control input resulting from perturbations caused by said perturbation means;

(n) third memory means comprising individual correction memories for each individual cylinder;

(o) selector means, responsive to said cylinder synchronization means, for selective connection to said individual correction memories;

(p) third calculation means, responsive to said load demand transducer and said engine speed calculation device and connected to said selector means so as to selectively receive said correction values from said individual correction memories through said selector means, for calculating a correction value for said second control input for each individual cylinder immediately prior to its firing; and

(q) a first summer means for summing said basic value for said second control input and said correction value for said second control input relating to each individual cylinder immediately prior to its firing to provide an output to said control device.

23. The system as in claim 22, wherein said perturbation generator operates in another perturbation mode in another operating mode of said engine to perturb said particular control input at a frequency greater than said highest resonant frequency.

24. The system as in claim 22, wherein said particular control input and said second control input are the same control input, and further comprising a second summer receiving said output of said first summer means prior to its being provided to said control means and summing it with said output of said perturbation generator to provide an output to said control means.

25. The system as in claim 22, wherein said particular control input and said second control input are not the same control input.

26. The system as in claim 23, wherein (i) said perturbation generator in said another perturbation mode generates a periodic perturbation waveform having said frequency greater than said highest resonant frequency and applies a first perturbation to said particular control parameter during a first part of each period of said perturbation waveform and a second perturbation of opposite polarity to that of said first perturbation to said particular control parameter during a second part of each period of said perturbation waveform, (ii) said perturbation generator in said at least one perturbation mode applies a third perturbation to said particular control parameter, permits a predetermined period to elapse without perturbing said particular control parameter, applies a fourth perturbation of opposite polarity to that of said perturbation to said particular engine control parameter, and permits another predetermined period to elapse without perturbing said particular control parameter, (iii) said measuring means in a first measurement mode corresponding to said another perturbation mode creates a first series of contiguous first and second measurement windows associated respectively with said first part and said second part of said period of said perturbation waveform, each of said measurement windows in said first series lagging its associated part of said period of said perturbation waveform by a predetermined phase shaft, said measuring means calculating said slope in accordance with a change in engine output between contiguous ones of said measurement windows in said first series, and (iv) said measuring means in a second measurement mode corresponding to said second perturbation mode creates a at least one series of measurement windows following each perturbation of said particular control parameter, each of said a at least one series of measurement windows occupying part of an interval between successive perturbations of said particular control parameter, said measuring means calculating said slope in accordance with a change in engine output between adjacent ones of said a at least one series of measurement windows.

27. The system as in claim 26, wherein in both said first measurement code and said second measurement mode said measuring means accumulates respectively during each window of said first series of measurement windows and said second series of measurement windows the fire periods whose central points fall within each window to produce a total fire period for each window, said measuring means calculating said slope in accordance with said total fire period for each window.

28. A method of controlling a power producing engine having at least one engine control parameter affecting an engine output, said engine having a drive train combination having at least one resonant frequency, said method comprising:

(a) perturbing intermittently a particular said control parameter about a base line value in at least one perturbation mode in a given operating mode of said engine which includes said resonant frequency;

(b) measuring a slope of said engine output with respect to said particular control parameter; and

(c) controlling one said control parameter so as to obtain a desired value of said slope, wherein step (a) includes perturbing said particular control parameter in another perturbation mode in another operating mode of said engine at a frequency greater than said resonant frequency.

29. The method as in claim 28, wherein said engine is an internal combustion engine and step (a) includes in the at least one perturbation mode (i) perturbing said particular control parameter with a first perturbation, (ii) permitting a predetermined period to elapse without perturbing said particular control parameter, (iii) perturbing said particular control parameter with a second perturbation having a polarity opposite that of said first perturbation, and (iv) permitting another predetermined period to elapse without perturbing said particular control parameter.

30. The method as in claim 29, wherein step (b) includes in a measurement mode corresponding to said at least one perturbation mode creating a series of measurement windows following each perturbation of said particular control parameter, each of said series of measurement windows occupying part of an interval between successive perturbations of said particular control parameter and measuring said slope in accordance with a change in engine output between adjacent ones of said series of measurement windows.

31. The method as in claim 29, wherein said another perturbation mode includes generating a periodic perturbation waveform having said frequency greater than said resonant frequency and applying a first perturbation to said particular control parameter during a first part of each period of said waveform and a second perturbation of opposite polarity to that of said first perturbation to said particular control parameter during a second part of each period of said waveform.

32. The method as in claim 31, wherein step (b) includes in a measurement mode corresponding to said another perturbation mode creating a series of contiguous first and second measurement windows associated respectively with said first part and said second part of said period of said perturbation waveform, each of said measurement windows in said series lagging its associated part of said period of said waveform by a predetermined phase shift.

33. The system as in claim 29, wherein said another operating mode is an upper speed range of said engine and said given operating mode is a lower speed range of said engine.

34. The method as in claim 28, wherein said particular control parameter and said one control parameter are the same.

35. A method of controlling a power producing engine having at least one engine control parameter affecting an engine output, said engine having a drive train combination having at least one resonant frequency, said method comprising:

(a) perturbing intermittently a particular said control parameter about a base line value in at least one perturbation mode in a given operating mode of said engine which includes said resonant frequency;

(b) measuring a slope of said engine output with respect to said particular control parameter; and

(c) controlling one said control parameter so as to obtain a desired value of said slope, wherein said particular control parameter and said one control parameter are different.

36. A method of controlling a multi-cylinder internal combustion engine having an engine output affected by at least one engine control parameter, said method comprising:

(a) establishing a plurality of combinations of cylinders of said engine, each of said combinations of cylinders including at least one cylinder;

(b) selecting each of said combinations in turn;

(c) perturbing a particular said control parameter of each of said combinations of cylinders at the time it is selected in step (b) by applying a first perturbation to said particular control parameter, permitting a period to elapse without perturbing said particular control parameter, applying a second perturbation of opposite polarity to that of said first perturbation to said particular control parameter and permitting another period to elapse without perturbing said particular control parameter;

(d) creating a series of measurement windows following each perturbation of said particular control parameter, each series of measurement windows occupying part of the interval between successive perturbations;

(e) calculating the slope of said engine output with respect to said particular control parameter for each of said combinations in turn from the change in engine output between adjacent measurement windows; and

(f) applying a correction based on said slope to at least one said control parameter associated with the currently selected cylinder combination.

40. The method as in claim 36 or 37, wherein each of said combinations comprises a single cylinder.

41. The method as in claim 36 or 37, wherein each of said cylinder combinations comprises all cylinders of said engine except one.

42. The method as in claim 36 or 37, wherein a value of said at least one control parameter is established prior to its being corrected in step (f) as a function of engine output and load on said engine.

43. The method as in claim 36 or 37, wherein said particular control parameter is an ignition timing parameter.

44. The method as in claim 36 or 37, wherein step (f) or step (h) respectively includes correcting a single engine parameter and wherein both said particular control parameter and said at least one control parameter corrected in step (f) or step (h) respectively are an ignition timing parameter.

45. The method as in claim 36 or 37, wherein said particular control parameter is an ignition timing parameter and said at least one control parameter corrected in step (f) or step (h) respectively is a single engine fuel control parameter.

46. The method as in claim 36 or 37, wherein said particular control parameter is an ignition timing parameter and step (f) or step (h) respectively includes correcting two said control parameters comprising an ignition timing parameter and an engine fuel control parameter.

37. A method of controlling a multi-cylinder internal combustion engine having an engine output affected by at least one engine control parameter, said method comprising:

(a) establishing a plurality of combinations of cylinders of said engine, each of said combinations of cylinders including at least one cylinder;

(b) selecting each of said combinations in turn;

(c) when said engine is in an upper speed range, perturbing a particular said control parameter of each of said combinations of cylinders at the time it is selected in step (b) by generating a periodic perturbation waveform and applying a first perturbation to said particular control parameter during a first part of each period of said perturbation waveform and a second perturbation of opposite polarity to that of said first perturbation during a second part of said perturbation waveform;

(d) when said engine is in a lower speed range, perturbing said particular control parameter of each of said combinations of cylinders at the time it is selected in step (b) by applying a first perturbation to said particular control parameter, permitting a period to elapse without perturbing said particular control parameter, applying a second perturbation of opposite polarity to that of said first perturbation to said particular control parameter and permitting another period to elapse without perturbing said particular control parameter;

(e) in said upper speed range, creating a first series of contiguous first and second measurement windows associated respectively with said first and second parts of the perturbation waveform, each measurement window lagging its respective part of the perturbation waveform by a predetermined phase shift;

(f) in said lower speed range, creating a second series of measurement windows following each perturbation of said particular control parameter, each series of measurement windows occupying part of the interval between successive perturbations;

(g) in both said upper and lower speed ranges, calculating the slope of engine output with respect to said particular control parameter for each of said combinations in turn from the change in engine speed between adjacent measurement windows; and

(h) applying a correction based on said slope to at least one said engine control parameter associated with the currently selected cylinder combination.

38. The method as in claim 37, wherein said internal combustion engine includes a flywheel, a resilient shaft means connected to said flywheel, and a gear means connected to said shaft means, said flywheel, said shaft means and said gear means forming a resonant system having a particular resonant frequency for each gear ratio of said gear means, and wherein said periodic perturbation waveform is caused to have a frequency greater than a highest resonant frequency of said resonant system when said engine is in said upper speed range, and each measurement window in said second series of measurement windows is equal to a whole number of quarters of said resonant frequency of said resonent system corresponding to a current gear ratio of said gear means.

39. The method as in claim 37, wherein step (g) includes accumulating respectively during each window of said first series of measurement windows and said second series of measurement windows the fire periods having central points which fall within each window to produce a total fire period for each window, so that said slope is calculated in accordance with said total fire period for each window.