SYSTEM FOR IDENTIFYING MISFIRE CYLINDER IN INTERNAL COMBUSTION ENGINE

Abstract: A system for identifying a misfired cylinder of a multiple cylinder internal combustion engine is provided. The system comprises a sensor which monitors revolutional cycles of cylinders respectively to determine a parameter associated with a variation in an average effective pressure of the cylinder in a preselected relation to the revolutional cycles. When the parameter is less than a preselected level, the system corrects the parameter by a correction factor to provide a second parameter in order to prevent reduction in the average effective pressure due to wavering of engine speed after misfire occurs from causing erroneously detection of the misfire cylinder. The system then compares the second parameter with a slice level to detect occurrence of misfire and identifies the misfired cylinder.

Description: The present invention relates to a system for detecting a misfired cylinder of a multiple cylinder internal combustion engine in accordance with the prior art portion of claim 1 and to a method for detecting a misfired cylinder of a multiple cylinder internal combustion engine in accordance with the prior art portion of claim 10. In an internal combustion engine, misfires sometimes occur due to malfunctions in an ignition system or a fuel supply system such as a fuel injection valve or leakage of pressurized mixture for example. When the misfiring occurs, unfired fuel in a misfired cylinder is discharged to an exhaust system. This unfired fuel is then fired in a catalytic converter, causing damage to the catalytic converter. This damage to the catalytic converter causes exhaust emission control to be degraded, thereby increasing a concentration of harmful emissions. Therefore, it is necessary to monitor misfire to warn of misfiring or to execute fuel-cut control which is operable to cut fuel to be supplied to the misfired cylinder. US-A-4683856 discloses a control system for an internal combustion engine which detects engine vibrations to derive a roughness signal indicative of torque fluctuations due to misfiring. The roughness signal is compared to a reference signal to enrich an air-fuel mixture fed to the engine if the roughness signal exceeds the reference signal. An ISATA-paper "Experiences with a new method for measuring the engine roughness" by R. Latsch, E. Mausner, V. Bianchi, 1979 discloses a system for detecting a misfired cylinder based on engine speed variation. This system mathematically calculates a value LUn representative of engine roughness to determine a misfired cylinder based thereon. The engine roughness value LUn is derived by the following equations M - W = ϑ dω dt M - W = ϑ2π d(1/T) dt M - W = ϑ2π d(1/T) dζ X dζ dt Integrating the above equation with respect to one rotation of a crank shaft, the following equation is obtained. where M = engine output torque, W = load torque, ω = crank angular velocity, ϑ = inertia moment, t = time, T = a crank shaft rotational cycle value, ξ - a crank angle, j = 0, 1, 3, ...., Tj = 2 or 1 crank shaft rotational cycle, and Tj-1 = Tj one cycle before. Assuming that W is a constant and Tj = Tj-1 = Tj-2, the following equation is obtained. Since the left term of the above equation corresponds to a variation ΔPi of average effective pressure of the engine which closely relates to generation of misfire, calculation of the right term in relation to the crank shaft rotational cycle enables indirect monitoring of variation of the average effective pressure, thereby identifying a misfired cylinder. Thus, the misfire can be detected by determining as to whether the average effective pressure varies to decrease less than a preselected level or not. An equation of the engine roughness LUn corresponding to the variation ΔPi of the average effective pressure Pi is given by the following relation. LUn = - 4π²ϑ Δ(ΔTj) Tj³ The above equation may be simplified in order to calculate practically as follows. Δ (ΔTj) = (Tj-1 - Tj-2) - (Tj - Tj-1) where in a case of a four-cylinder engine, Tj-1 = a cycle 180° before 360° (one revolution), Tj-2 = a 180° cycle before 720° (two revolutions), Tj = the most recent 180° cycle and Tj³ is replaced with Tj, Tj-1, or Tj-2 in order to simplify calculation of Tj³. Assuming that the cycle 180° before 360° (one revolution of the engine) is denoted by a symbol "half", the 180° cycle before 720° (two revolutions) is a symbol "old", the most recent 180° cycle is denoted by a symbol "new" and the Tj³ is replaced with Tj-2 (a 180° cycle before 720° = old), the equation of the engine roughness LUn is simplified as follows. LUn = (half - old) - (new - half) old If the engine roughness LUn is determined according to the above equation, for example, a time chart as shown in Fig. 5 is obtained. In this time chart, a value LU1 corresponding to a #1cylinder of the four-cylinder engine is calculated by assigning the newest 180° cycle, a 180° cycle, one revolution before, affected by a cylinder pressure of the #4cylinder, and a 180° one cycle before affected by a cylinder pressure of the #1cylinder to "new", "half", and "old" when the newest value updated every TDC (180°) is affected by a cylinder pressure of the #1cylinder. Detection of a misfired cylinder according to the calculation of the value LUn is accomplished with logic wherein if the value LUn is less than a slice level SL determined by engine operating conditions, such as an engine speed and a basic injection quantity, it is concluded that misfire occurs, or if the values LUn are continuously less than the slice level SL, it is concluded that the initial value LUn is affected by the misfire. If the misfire, as shown in Fig. 5, continuously occurs in the #1cylinder, the values LU1 and LU3 respectively corresponding to the #1 and #3cylinders are negative values less than the slice SL. It is however concluded that the misfire occurs in the # 1cylinder since the value LU1 corresponding to the #1cylinder is the initial value. The slice level SL is memorized in a map or table so that it is set to a value intermediate a minimum value LUn when no misfire occurs in all cylinders and a minimum value when misfire occurs in any cylinder to ensure accuracy of the misfire detection relative to variation in the value LUn due to various engine operating condition (See Figs. 6 to 8). The misfire detection based on the above described engine roughness value LUn can provide proper detection accuracy when misfire occurs continuously in a particular cylinder. However, if one misfire occurs, as shown in Fig. 9, in a particular cylinder discontinuously, a wavering of normal engine combustion occurs after each misfire. Due to this wavering in the engine revolution, the engine roughness value LUn sometimes becomes a negative value over the slice level SL. This results in mis-detection wherein it is concluded that misfire occurs in a cylinder other than a misfired cylinder. For example, as shown in Fig. 9, if one misfire occurs in only #1cylinder every nine engine revloutions, while both a value LU1 of the #1cylinder and a value LU3 of the #3cylinders are negative values less than the slice level SL because cylinders are ignited in order of #1, #3, #4, and #2, it is concluded that the misfire occurs in the #1cylinder since the value LU1 of the #1cylinder is an initial value. However, if the misfire occurs discontinuously in the #1cylinder, engine speed varies after normal combustion occurs in the #1cylinder resulting in wavering revolution. This causes values LU2 and LU3 becomes negative values less than the slice level SL. As a result, an error is made in conclusion that misfire occurs in the #4cylinder because it is fired earlier than the #2cylinder. It will be appreciated that the prior art misfire detection system correctly identifies a misfired cylinder when misfire occurs continuously in a particular cylinder, however, accuracy of the misfire detection is reduced when the misfire occurs discontinuously in the particular cylinder. Starting from the above prior art, the present invention is based on the object of providing a system and method for identifying a misfired cylinder precisely even when the misfire occurs discontinuously in a particular cylinder to prevent erroneous misfire detections. This object is achieved by a system in accordance with claim 1 and by a method in accordance with claim 10. BRIEF DESCRIPTION OF THE DRAWINGS The present invention will be understood from the detailed description given hereinbelow and from the accompanying drawings of the preferred embodiments which are given for explanation and understanding only and are not intended to imply limitations to the invention. Fig. 1 is a block diagram which shows a system according to the present invention. Figs. 2a, 2b, 2c, 3, and 4 are flowcharts which show programs or sequences of logical steps performed by a system of the invention. Fig. 5 is a time-chart which shows occurrence of continuous misfire in first and third cylinders. Fig. 6, 7, 8 and 9 are time-charts which show a relation between misfire and a engine roughness value LUn. DESCRIPTION OF THE PREFERRED EMBODIMENT Referring now to the drawings, particularly to Fig. 1, a system according to the present invention is shown which monitors misfire of an internal combustion engine. Air is supplied to the internal combustion engine 1 through an air cleaner 2, an intake duct 3, a throttle chamber 4, and an intake manifold 5. The intake duct 3 includes an air-flow meter 6 which detects an intake air flow rate Q to output a signal indicative thereof to a control unit 9. The throttle chamber 4 includes a throttle valve 7 which is operated by an acceleration pedal (not shown) for controlling the intake air flow rate Q. The intake manifold 5 includes electromagnetic type fuel injection valves 8 (fuel nozzles) for every cylinder (in this embodiment, four cylinders are provided) which inject fuel in the intake manifold supplied by a fuel pump (not shown) under a preselected pressure controlled by a pressure regulator. The control unit 9 includes a micro-computer which is operable to control the flow rate of fuel or fuel injection quantity. The control unit 9 calculates a basic fuel injection quantity Tp given by a relation of Tp = K X Q/N (K = a constant) based on the intake air flow rate Q monitored by the air flow meter 6 and engine speed N determined by a signal from a crank angle sensor 10 incorporated in a distributor 13 and then compensates the basic fuel injection quantity Tp based on a coolant temperature Tw detected by a coolant temperature sensor 14 to provide a target fuel injection quantity Ti to output driving pulse signals indicative thereof to the fuel injection valves 8 synchroniously with engine revolutions, thereby injecting necessary quantity of fuel to the engine 8. The cylinders of the engine 1 include spark plugs 11 respectively to which high-voltage surges produced by ignition coils 12 are applied through the distributor 13 in regular order, thereby generating spark at the spark plugs to ignite a compressed air-fuel mixture. The high-voltage surge generation timing of the ignition coil 12 is controlled by a power transistor 12a. Control of ignition timing (or spark advance control) is accomplished by controlling on-off timing of the power transistor 12a utilizing an ignition control signal from the control unit 9. The control unit 9 retrieves a correction value ADV for the spark advance which corresponds to driving condition at that time from a map or table which memories proper correction values ADV, determined experimentally, for a plurality of engine operating regions respectively which are determined by the basic fuel injection quantity Tp and the engine speed N and detects a cylinder in which misfire occurs to indicate such misfire. The throttle valve 7 includes a throttle sensor which monitors a throttle valve opening (TVO) utilizing a potentiometer. The crank angle sensor 10 monitors crank angles of the cylinders of four-cylinder engine to provide angle reference signals REF every 180 degrees (in this embodiment, every 70 degrees before the 110 degrees after TDC (Top Dead Center)) and angular position signals POS every 1 or 2 degrees. Referring to Figs. 2 to 4, a flowchart of a program or sequence of logical steps is shown which is performed by the control unit 9 for monitoring misfire to identify the misfired cylinder. In this embodiment, a four-cylinder engine is used as an example and thus the program is carried out every 180 degrees of engine revolution. The program starts at step 100 every time a cylinder reaches TDC. Monitoring the TDC is accomplished by counting the number of crank angle position signals POS based on the crank angle reference signal REF which is output from the crank angle sensor 10 every 70° before the TDC. After entering the program in step 100, the routine proceeds to step 110 wherein a 180° revolution cycle (i.e., a TDC cycle) which is a period of time elapsed from the TDC of the previously fired cylinder to the TDC or the currently fired cylinder is determined. An up-to-date TDC cycle T0, a TDC cycle T1 of one program operational cycle before, a TDC cycle T2 two program operational cycles before, and a TDC cycle T3 in three program operational cycles before which are defined in the previous program operational cycle and are updated as T1, T2, T3, and T4 and the current up-to-date TDC cycle is always set to T0. The routine then proceeds to step 120 wherein an engine roughness value LU (i.e., engine speed variation) which corresponds to a variation in an average effective pressure of each cylinder is mathematically calculated according to the following equation utilizing the updated cycle T0, T2, and T4 derived in step 110. LU = (T2 - T4) - (T0 - T2) T4 The above equation is obtained by a manner as mentioned in the background of the art and simplified for facilitating calculation based on the revolution cycle T. This equation is essentially the same as that in relation to an LU value as shown in Fig. 5 if "new", "half", and "old" are replaced with T0, T2, and T4 respectively. The routine then proceeds to step 130 wherein it is determined as to whether the engine roughness value LU is less than zero or not to determine whether the average effective pressure varies to decrease or not. If a YES answer is obtained, that is, the engine roughness value LU is negative, it is concluded that the average effective pressure is reduced and the routine proceeds to step 140. In step 140, a correction factor "gain" for the value LU is retrieved from a map or table based on an absolute value of a parameter derived by dividing the value LU by a minimum value which is selected from among the old LU values. The table for the correction factor "gain" is such that when a value of | LU / min | is near to one "1" is assigned to the correction factor and as the value of | LU / min | nears zero, the correction factor suddenly approaches zero. Therefore, when the value LU is multiplied by the correction factor "gain" to adjust the value LU, if the newly calculated value LU is near the minimum value, the value LU is scarcely corrected, however, if the newly calculated value LU is nearer zero than the minimum value, the value LU is compensated so as to be decreased by a relatively great rate. It will be noted that if the value LU is sufficiently nearer zero than the minimum value, the value LU is adjusted to about zero. As described hereinafter, by comparing the value LU corrected by the correction factor "gain" with a slice level SL, determination is made as to whether the average effective pressure is reduced less than a preselected level for detecting a cylinder in which misfire occurs. However, a correction to extremely decrease the value LU by the correction factor "gain" is unable to detect misfire appropriately, and additionally, an extremely slight correction to decrease the value LU is unable to avoid mis-detection, as is an essential object of the present invention. Therefore, it is preferable to empirically provide the table for the correction factor "gain" based on so-called fuzzy theory. As described above, according to the correction a value of LU which is sufficiently nearer zero than the minimum value is adjusted to about zero with the correction factor "gain", as shown in Fig. 9; a value of LU which is slightly less than the slice level SL when the engine speed varies to create wavering revolution in normal-combustion after one misfire occurs discontinuously in a particular cylinder LU is corrected to a value near the slice level SL. Thus, error in misfire detection is prevented. Additionally, if misfire occurs and the value LU is continuously calculated less than the slice level SL as shown in Fig. 5, the smaller value LU is updated to the minimum value and the other is corrected so as to be slightly decreased by the correction factor "gain" because it is near the minimum value. Thus, it is appreciated that misfire can be detected similar to conventional manner. After determining the correction factor "gain" based on the value | LU/min | in step 140, the routine proceeds to step 150 wherein the value LU calculated in step 120 is multiplied by the correction factor "gain" and the result is set to a value ℓu. The routine proceeds to step 160 wherein it is determined whether the value LU calculated in step 120 is smaller than the minimum value from among the values LU derived until now. If a YES answer is obtained the routine proceeds to step 170 wherein the minimum value is updated. The routine then proceeds to step 180 wherein it is determined as to whether the value ℓu corrected in step 150 is smaller than the slice level SL or not. The slice level SL is retrieved from a map or table based on the basic injection quantity Tp and the engine speed N according to a program (executed as a background program) as shown in Fig. 3 and a value intermediate a minimum value LUn when no misfire occurs in all cylinders and a minimum value when misfire occurs in any cylinder is provided to ensure accuracy of the misfire detection relative to variation in the value LUn due to different engine operating conditions. It will be appreciated that the value ℓu when misfire occurs is less than the slice level SL and thus it is concluded that the average effective pressure is reduced extremely due to misfire. If a YES answer is obtained in step 180, the routine proceeds to step 200 wherein a timer is reset to zero to measure a period of time elapsed after the misfire detection. The routine proceeds to step 210 wherein it is determined as to whether a flag is "1" (one) or "0" (zero) in order that when the misfire is continuously monitored, a first value LU is given priority to identify a misfired cylinder. The flag is set to zero in step 190 when the value LU is more than or equal to zero in step 130 and when the value ℓn is more than or equal to the slice level in step 180. In an initial program cycle when the value ℓu is less than the slice level SL, and flag is zero and thus the routine proceeds to step 220. In step 220, a misfired cylinder is specified based on a value Icnt set in a counter to which one of numerical values of 1 to 4 is assigned according to a program as shown by a flowchart in Fig. 4 which corresponds to cylinder numbers 1 to 4 respectively. The program in Fig. 4 is performed in response to the crank angle reference signals REF output from the crank angle sensor 10 at an angular position 70° before TDC. The crank angle reference signals REF are, for example, pulse signals each having a different width corresponding to each cylinder and indicate reference spark angular positions of the cylinders. After entering the program in step 500, the routine proceeds to step 510 wherein it is determined which or the cylinders the currently output crank angle reference signal REF corresponds to. If the currently output crank angle reference signal REF corresponds to #4cylinder, the routine proceeds to step 520 wherein a value Icnt is set to "4". Similarly, in steps 530, 540, and 550, the values Icnt are respectively set to "1", "2", and "3" each corresponding to the cylinder which outputs the crank angle reference signal. The program then terminates in step 560. Return to Fig. 2b, in step 220 the numerical value indicated by the Icnt is determined to distinguish the current crank angle reference signal REF output from which of the cylinders. It is concluded based on the value ℓu that misfire (reduction over a preselected rate in the average effective pressure) occurs in a cylinder sparked prior to a cylinder represented by the Icnt because the cylinder sparked before that represented by Icnt produces pressure affecting the current TDC cycle. Therefore, since in this embodiment the cylinders are ignited in ignition timing order of #1, #3, #4, and #2, it is concluded that for example, if the Icnt indicates "2", misfire has occurred in the #4cylinder. It will be appreciated that according to the numerical value represented by the Icnt, a misfired cylinder is specified. Subsequently, in steps 230 to 260, "one" is added to a parameter in counters "lstcnt4", "lstcnt3", "lstcnt2", and "lstcnt1" which indicate the number of misfire generated in the cylinders #4, #3, #2, and #1 respectively to update them. After the number of misfires is set for the corresponding counter(s), the routine proceeds to step 270 wherein the flag is set to "1". Therefore, in the next program cycle, when the routine proceeds to step 210 after determination that the value ℓu is less than the slice level SL in step 130, it is conceded that the flag is "1". The routine then directly proceeds to step 300 as shown in Fig. 3c without determining a misfired cylinder. As a result, when the values ℓu less than the slice level SL are continuously calculated, it is concluded that misfire occurs in a cylinder corresponding to the first value. Therefore, for example, when misfire occurs in the #1cylinder successively as shown in Fig. 5 and the values ℓu (LU) corresponding to the #1 and #3 cylinders are less than the slice level SL continuously, it is concluded that the misfire occurs in only #1cylinder. In step 300, a coefficient X is retrieved from a map or table in relation to a period of time elapsed after conclusion that the value ℓu is less than the slice level SL. The coefficient X is utilized for correcting the minimum value of the value LU in the next step 310, which may be empirically provided suitably for the engine operating condition. In step 310, the minimum value is adjusted according to the following relation. min = min (1.0 - X) + SL X Thus, when the coefficient X is near zero, the minimum value is not corrected, however, as the coefficient X becomes great, the minimum value is converged to the slice level SL gradually. It will be thus noted that long period of time elapsed after the misfire detection causes the minimum value to approach the slice level SL. This adjustment of the minimum value provides further effective control that the value LU is converged to zero in steps 140 and 150. The value LU calculated under wavering of the engine speed caused by the misfire is corrected to a value near zero, thereby preventing misfire from being detected erroneously. Additionally, the adjustment of the minimum value to a value near the slice level SL obtains appropriate minimum value suitable for engine operating condition at that time when the minimum value of the value LU is increased dependent upon variation of the engine operating condition. Subsequently, the routine proceeds to step 320 wherein "1" (one) is added to a value in a counter which represents the number of program executions every operation after the misfire occurs for measuring a period of time elapsed from the misfire detection (i.e., the number of TDCs). The routine then proceeds to step 230 wherein it is determined whether the number of executions of program operation "Totalcnt" is less than a preselected number (for example, 1000) or not. If a NO answer is obtained the routine proceeds to step 340 wherein "1" (one) is added to the count value "Totalcnt" and the routine proceeds to step 450 wherein the program terminates. On the other hand, if a YES answer is obtained, the routine proceeds to step 350 the count value "Totalcnt" is reset to zero, after which the routine proceeds to steps 360 to 430 wherein a misfired cylinder number is indicated based on the values representing the numbers of misfire in cylinders respectively. For example, in step 350, it is determined as to whether the value "lstcnt1" representing the number of misfires in the #1cylinder is more than a preselected value until the count value "Totalcnt" reaches "1000". If a YES answer is obtained, the routine proceeds to step 370 wherein the generation of misfire in the #1cylinder is indicated on a display provided on the vehicle dash-board to give alarm to an operator or driver. Similarly, in steps 360, 380, 400, and 420, the values lstcnt 2 to lstcnt 4 are compared with the preselected value respectively to determine a generation rate of misfire. If the misfire is generated more than a preselected number of times, the misfired cylinder is displayed to the driver in steps 390, 410, and 430. Subsequently, the routine then proceeds to step 440 wherein the lstcnt1 to lstcnt 4 are reset to zero respectively for newly setting the number of misfires in each cylinder again during the time the count value "Totalcnt" takes to reach the preselected value. As mentioned above, while in this embodiment when the number of misfires is more than the preselected number of times, the misfired cylinder is displayed to the driver, fail-safe control such as fuel-cut control may be effected along with the alarm being given to the driver. Additionally, in the above embodiment, when the value LU is nearer zero than the minimum value, the value LU is corrected by the correction factor "gain" to be set to a value near zero, however, the slice level SL for detecting misfire may be decreased dependent upon a level of the minimum value to prevent the misfire from being erroneously detected based on the value LU which represents reduction in the average effective pressure smaller than the minimum value.

Claims: System for detecting a misfired cylinder of a multiple cylinder internal combustion engine comprising: sensor means (10) for monitoring a variation of an engine operating condition during each engine revolutional cycle; first means (110,120) for determining a first parameter associated with a variation in an average effective pressure of the cylinder based on the variation monitored by said sensor means; and second means (180) for identifying a misfired cylinder, characterized by third means (130-170) for correcting the first parameter (LU) by a predetermined correction factor (gain) to provide a second parameter if the first parameter is less than a preselected level, wherein said second means (180) identifies the misfired cylinder if the second parameter is less than a preselected slice level (SL). System as set forth in claim 1, characterized in that said third means (130-170) further determines a minimum parameter (min) from among the first parameters (LU) monitored in previous operational cycles of the system which indicates a maximum reduction in the average effective pressure of the cylinder, the preselected correction factor (gain) being determined by a preselected relation between the minimum parameter (min) and the first parameter (LU). System as set forth in claim 2, characterized in that said third means (130-170) compensates the first parameter (LU) by a small correction rate if the reduction in the average effective pressure represented by the first parameter (LU) approaches the maximum reduction. System as set forth in one of the claims 1 to 3, characterized in that said third means (130-170) compensates (300-320) the minimum parameter (min) to converge with the slice level (SL) over a period of time elapsed from the occurrence of the misfire. System as set forth in one of the claims 1 to 4, characterized in that said sensor means (10) monitors a cycle from the previous top dead center to the current top dead center, said first means (110-120) determines the first parameter (LU) according to the following relation: LU = (half - old) - (new - half) old wherein LU denotes the first parameter, new denotes an up-to-date cycle monitored by said sensor means, half denotes a cycle one stroke cycle before, and old denotes a cycle two stroke cycles before. System as set forth in one of the claims 1 to 5, characterized by display means for displaying the misfired cylinder to an operator when the misfire occurs in a particular cylinder more than a predetermined number of times. System as set forth in one of the claims 1 to 6, characterized by a second sensor means (10) for monitoring crank angles of the cylinders to provide signals indicative of top dead centers of the cylinders respectively, said sensor means monitoring revolutional cycles from the top dead center of a previous cylinder to the top dead center of a current cylinder. System as set forth in one of the claims 1 to 7, characterized in that said slice level (SL) is determined by a preselected relation between a fuel injection quantity (Tp) to the cylinders and an engine speed (N) so that the slice level (SL) is defined between a minimum parameter from among the first parameters when misfire occurs and a minimum parameter from among the first parameters when no misfire occurs. System as set forth in claim 3, characterized in that said third means (130-170) compensates the first parameter (LU) by said reduction rate if an absolute value obtained by dividing the first parameter by the minimum parameter (min) becomes close to one. Method of detecting a misfired cylinder of a multiple cylinder internal combustion engine, comprising the steps of monitoring (101a) variation of an engine operating condition during each engine revolutional cycle; determining (110,120) a first parameter associated with a variation in an average effective pressure of the cylinder based on the variation; and identifying (180) a misfired cylinder, characterized by the step of: correcting (130-170) the first parameter (LU) by a predetermined correction factor (gain) to provide a second parameter if the first parameter is less than a preselected level, wherein the misfired cylinder is identified if the second parameter is less than a preselected slice level (SL). Method as set forth in claim 10, characterized in that said correcting step comprises the step of determining a minimum parameter (min) from among the first parameters (LU) monitored in previous operational cycles which indicates a maximum reduction in the average effective pressure of the cylinder, the preselected correction factor (gain) being determined by a preselected relation between the minimum parameter (min) and the first parameter (LU). Method as set forth in claim 10 or 11, characterized in that said correcting step comprises the step of compensating the first parameter (LU) by a small correction rate if the reduction in the average effective pressure represented by the first parameter (LU) approaches the maximum reduction. Method as set forth in one of the claims 10 to 12, characterized in that said correcting step comprises the step of compensating (300-320) the minimum parameter (min) to converge with the slice level (SL) over a period of time elapsed from the occurrence of the misfire. Method as set forth in one of the claims 10 to 13, characterized in that said slice level (SL) is determined by a preselected relation between a fuel injection quantity (Tp) to the cylinders and an engine speed (N) so that the slice level (SL) is defined between a minimum parameter from among the first parameters when misfire occurs and a minimum parameter from among the first parameters when no misfire occurs. Method as set forth in one of the claims 10 to 14, characterized in that said correcting step comprises the step of compensating the first parameter (LU) by said reduction rate if an absolute value obtained by dividing the first parameter by the minimum parameter (min) becomes close to one.

Inventors: NAKANIWA, SHINPEI
Applicants: JAPAN ELECTRONIC CONTROL SYSTEMS CO., LTD.
Application year: 1990
Main classification: G01M15
IPC codes: F02D45, F02D41, F02P17, G01M15