CONTROL SYSTEM FOR INTERNAL COMBUSTION ENGINE

Abstract: A control system for an internal combustion engine comprises: first means (6,8,10,12,14) for monitoring engine driving conditions; second means (11;S24) for deriving a basic fuel supply quantity (Tp) on the basis of said engine driving conditions; third means (11;S25,S26,S111,S112) for deriving a variation speed (▵ A) of an intake air path area (A) on the basis of the engine driving conditions; fourth means (11;S27 to S36;S114 to S120) for deriving a correction value for said basic fuel supply quantity on the basis of the variation speed (▵ A) of the intake air path area; and fifth means (11;S37;S121) for controlling the fuel supply quantity on the basis of the basic fuel supply quantity corrected with the correction value, wherein said third means (S25,S26,S111,S112) derive said intake air path area (A) from an opening angle (TV0) of the throttle valve and an opening angle of a bypass passage (18).

Description: The present invention relates to a control system for an internal combustion engine in accordance with the prior art portion of claim 1 and to a method of controlling an internal combustion engine in accordance with the prior art portion of claim 2. It is conventionally known in typical engine control to monitor an intake air related parameter representative of an intake air amount and an engine speed related parameter representative of an engine revolution speed. Based on the intake air related parameter and the engine speed related parameter, a basic fuel supply amount Tp is derived. The basic fuel supply amount Tp is corrected by a correction value which is derived on the basis of various correction parameters, such as an engine coolant temperature and so forth. The corrected value is output as a final fuel supply data Ti. On the other hand, a spark ignition timing id is determined on the basis of the basic fuel supply amount Tp and the engine speed. In order to monitor the intake air related parameter, an air flow meter or an intake air pressure sensor has been used. Because of lag of such air flow meter or intake air pressure sensor, the intake air related parameter varies to increase and decrease following to actual variation of the intake air flow amount with a certain lag time. In the case of acceleration, such lag of response in variation of the intake air related parameter results in leaner mixture to raise emission problem by increasing the amount of NO x and HC. Furthermore, due to lag in variation of average effective pressure, acceleration shock and degradation of engine acceleration characteristics can be caused. In addition, since the fuel supply amount becomes smaller than that required, spark advance tends to be excessively advanced to cause engine knocking. In order to avoid such drawbacks caused by lag of the air flow meter or the intake air pressure sensor, Japanese Patent First (unexamined) Publication (Tokkai) Showa 60-201035 discloses a technique for correcting the intake air flow rate measured by the air flow meter or the intake air pressure measured by the intake air pressure sensor according to a variation ratio of a throttle valve open angle in order to derive an assumed intake air flow rate or an assumed intake air pressure. In such a system, since the fuel supply amount is derived on the basis of the corrected intake air related parameter, i.e. intake air flow rate or intake air pressure, fluctuation of air/fuel ratio can be minimized for better transition characteristics. However, because the intake air flow rate and the intake air pressure do not correspond linearly to the throttle valve open angle, extensive work has been required for determining correction values for respective throttle valve angular positions. By extensive work for setting the correction values, cost for the control unit becomes high. Furthermore, though the proposal in the aforementioned Japanese Patent First Publication 60-201035 improves resonse characteristics, it cannot achieve a satisfactorily high precision level because the disclosed system does not concern difference of timing between a timing of measurement of the intake air flow rate or the intake air pressure and a timing of variation of the throttle valve angular position. Patent Abstracts of Japan, Vol. 9, No. 279 (M-427), (2002), November 7, 1985, discloses a fuel injection system for an internal combustion engine computing a reference injection quantity on the basis of the rotational beat of the engine and the negative suction pressure, determining the variation ratio of the opening angle of the throttle valve to determine whether there is an acceleration demand or not. If an acceleration condition is detected, the fuel injection quantity is changed. Moreover, the injection angle, the injection completion timing and the injection start timing are determined. Patent Abstracts of Japan, Volume 9, No. 162(M-394) (JP-A-60 035 158) discloses a fuel injection device which increases the fuel injection during accelleration periods by generating an asynchronous temporary pulse. The accelleration condition is detected on the basis of the change amount of the throttle valve opening. This reference does not mention the deriving of the variation speed of the intake air path area from both the opening angle of the throttle and the opening angle or opening degree of a by-pass passage. Starting from the above prior art, the present invention is based on the object of providing a control system for an internal combustion engine and a method of controlling an internal combustion engine providing an improved control characteristic at the transition state of the engine driving condition. This object is achieved by a control system in accordance with claim 1 and by a method of controlling an internal combustion engine in accordance with claim 2. Preferred embodiments of the invention will be described hereinafter with reference to the attached drawings, in which: Fig. 1 is a schematic block diagram showing the preferred embodiment of a fuel supply control system according to the present invention; Fig. 2 is a block diagram showing detail a control unit of the preferred embodiment of the fuel supply control system of Fig. 1; Fig. 3 a flowchart of a routine for deriving a intake air pressure on the basis of an intake pressure indicative signal of a intake air pressure sensor; Figs. 4(a), 4(b) and 4(c) are flowcharts showing a sequence of an interrupt routine for deriving a fuel injection amount; Figs. 5(a) and 5(b) are flowcharts showing a sequence of interrupt routine for setting an engine idling controlling duty ratio and assuming an altitude for altitude dependent fuel supply amount correction; Fig. 6 is a flow chart of an interrupt routine for deriving an air/fuel ratio feedback controlling correction coefficient on the basis of an oxygen concentration in an exhaust gas; Figs. 7(a) and 7(b) are flowcharts showing a sequence of background job executed by the control unit of Fig. 2; Fig. 8 is a flowchart of a routine for deriving an average assumed altitudes; Fig. 9 is a chart showing relationship between an air/fuel ratio, basic fuel injection amount Tp and a throttle valve angle; Fig. 10 is a graph showing basic induction volume efficiency versus an intake air pressure, experimentally obtained; Fig. 11 is a graph showing variation of an intake air flow rate (Q) in relation to an intake air path area (A); Fig. 12 is a graph showing a basic engine load (Q/N) in relation to a ratio of intake air path area (A) versus an engine speed (N); and Fig. 13 is a flow chart showing another emnbodiment of a fuel injection amount derivation routine to be executed in place of the routine of Figs. 4(a), 4(b) and 4(c). DESCRIPTION OF THE PREFERRED EMBODIMENT Referring now to the drawings, particularly to Fig. 1, the preferred embodiment of a fuel supply control system, according to the present invention, will be discussed in terms of fuel supply control for a fuel injection internal combustion engine. The fuel injection internal combustion engine 1 has an air induction system including an air cleaner 2, an induction tube 3, a throttle chamber 4 and an intake manifold 5. An intake air temperature sensor 6 is provided in the air cleaner 2 for monitoring temperature of an intake air to produce an intake air temperature indicative signal. A throttle valve 7 is pivotably disposed within the throttle chamber 4 to adjust an intake air path area according to depression magnitude of an accelerator pedal (not shown). A throttle angle sensor 8 is associated with the throttle valve 7 to monitor the throttle valve angular position to produce a throttle angle indicative signal TVO. The throttle angle sensor 8 incorporates an idling switch 8A which is designed to detect the throttle valve angular position in substantially closed position. In practice, the idling switch 8A is held OFF while throttle valve open angle is greater than a predetermined engine idling criterion and ON while the throttle valve open angle is smaller than or equal to the engine idling criterion. An intake air pressure sensor 9 is provided in the induction tube 3 at the orientation downstream of the throttle valve 7 for monitoring the pressure of the intake air flow through the throttle valve 7 for producing an intake air pressure indicative signal. In the shown embodiment, a plurality of fuel injection valves (only one is shown) 10 are provided in respective branch paths in the intake manifold 5 for injecting the controlled amount of fuel for respectively associated engine cylinder. Each fuel injection valve 10 is connected to a control unit 11 which comprises a microprocessor. The control unit 11 feeds a fuel injection pulse for each fuel injection valve 10 at a controlled timing in synchronism with the engine revolution cycle to perform fuel injection. The control unit 11 is also connected to an engine coolant temperature sensor 12 which is inserted into an engine coolant chamber of an engine block to monitor temperature of the engine coolant and produces an engine coolant temperature indicative signal Tw. The control unit 11 is further connected to an oxygen sensor 14 disposed within an exhaust passage 13 of the engine. The oxygen sensor 14 monitors oxygen concentration contained in an exhaust gas flowing through the exhaust passage 13 to produce an oxygen concentration indicative signal. The control unit is additionally connected to a crank angle sensor 15, a vehicle speed sensor 16 and a transmission neutral switch 17. The crank angle sensor 15 monitors angular position of a crank shaft and thus monitors angular position of engine revolution cycle to produce a crank reference signal ϑ ref at every predetermined angular position, e.g. at every crankshaft angular position 70 ° before top-dead center (BTDC), and a crank position signal at every predetermined angle, e.g. 1° of engine revolution. The transmission neutral switch 17 detects setting of neutral position of a power transmission (not shown) to output transmission neutral position indicative HIGH level signal N T . Furthermore, the control unit 11 receives the intake air temperature indicative signal from the intake air temperature sensor 6 and throttle angular position indicative signal of the throttle angle sensor 8, the idling switch 8A and the intake air pressure sensor 9. In the shown embodiment, an auxiliary air passage 18 is provided to the air induction system and by-passes the throttle valve 7 for supplying an auxiliary air. An idling speed adjusting auxiliary air flow control valve 19 is provided in the auxiliary air passage 18. The auxiliary air flow control valve 19 is further connected to the control unit 11 to receive an idling speed control signal which is a pulse train having ON period and OFF period variable depending upon the engine driving condition for adjusting duty ratio of open period of the auxiliary air control valve 11. Therefore, by the idling speed control signal, the engine revolution speed during idling control signal, the engine idling speed can be controlled. Generally, the control unit 11 comprises CPU 101, RAM 102, ROM 103 and input/output interface 104. The input/output interface 104 has an analog-to-digital (A/D) converter 105, an engine speed counter 106 and a fuel injection signal output circuit 107. The A/D converter 105 is provided for converting analog form input signals such as the intake air temperature indicative signal Ta from the intake air temperature sensor 6, the engine coolant temperature indicative signal Tw of the engine coolant temperature sensor 12, the oxygen concentration indicative signal O₂, a vehicle speed indicative signal VSP of the vehicle speed sensor 16 and so forth. The engine speed counter 106 counts clock pulse for measuring interval of occurrences of the crank reference signal ϑ ref to derive an engine speed data N on the basis of the reciprocal of the measured period. The fuel injection signal output circuit 107 includes a temporary register to which a fuel injection pulse width for respective fuel injection valve 10 is set and outputs drive signal for the fuel injection signal at a controlled timing which is derived on the basis of the set fuel injection pulse width and predetermined intake valve open timing. Detail of the discrete form construction of the control unit will be discussed from time to time with the preferred process of the fuel injection control to be executed by the control unit, which process will be discussed herebelow with reference to Figs. 3 to 13. Fig. 3 shows a routine for deriving an intake air pressure data P B on the basis of the intake air pressure indicative signal V PB which is originally voltage signal variable of the voltage depending upon the magnitude of the intake air pressure. The shown routine of Fig. 3 is triggered and executed every 4 ms by interrupting a background job which may include a routine for governing trigger timing of various interrupt routines, some of which will be discussed later. Immediately after starting execution of the routine of Fig. 3, the intake air pressure indicative signal V PB is read out at a step S1. Then, a intake air pressure map 110 which is set in ROM 103 in a form of one-dimensional map, is accessed at a step S2. At the step S2, map look-up is performed in terms of the read intake air pressure indicative signal V PB to derive the intake air pressure data PB. After deriving the intake pressure data PB (mmHg), process returns to the background job. Figs. 4(A) and 4(B) show a sequence of fuel injection amount Ti derivation routine which is executed at every 10 ms. Immediately after starting execution, input sensor signals including the throttle angle indicative signal TVO are read out at a step S11. At the step S11, the intake air pressure data PB which is derived through the routine of Fig. 3 is also read out. At at step S12, a throttle valve angular displacement rate ▵TVO is derived. In practice, the throttle valve angular displacement rate ▵TVO is derived by comparing the throttle angle indicative signal value TVO read in the step S11 with the throttle angle indicative signal value read in the immediately preceding execution cycle. For this purpose, RAM 102 is provided a memory address 111 for storing the throttle angle indicative signal value TVO to be used in derivation of the throttle valve angular displacement rate ▵TVO in the next execution cycle. Therefore, at the end of process in the step S12, the content of the TVO storing memory address 111 is updated by the throttle valve indicative signal value read at the step S11. Then, the throttle valve displacement rate ▵TVO is compared with an acceleration threshold and a deceleration threshold to check whether acceleration or deceleration of the engine is demanded or not, at a step S13. When the throttle angle displacement rate ▵TVO is greater than or equal to the acceleration threshold or smaller than the deceleration threshold as checked at the step S13, further check is performed at a step S14, whether the current cycle is the first cycle in which the acceleration demand or deceleration is detected. For enabling this judgement, a flag FLACC is set in a flag register 112 in CPU 101 when acceleration or deceleration demand is at first detected. Though there is no illustrated routine of resetting the FLACC flag in the flag register 112, it may be preferable to reset the FLACC flag after a given period of termination of the acceleration or deceleration demand. When the first occurrence of acceleration or deceleration demand is detected at the step S15, a timer 113 for measuring a period of time, in which acceleration or deceleration demand is maintained is maintained, is reset to clear a timer value TACC to zero (0). After the step S14, a flag FALT in a flag register 114 which is indicative of enabling state of learning of assuming of altitude depending upon the engine driving condition while it is set and indicative of inhibited state of learning while it is reset, is reset at a step S16. On the other hand, when the acceleration or deceleration demand is not detected as checked at the step S13 or when the FLACC flag of the FLACC flag register is set as checked at the step S14, the timer value TACC of the TACC timer 113 is incremented by 1, at a step S17. Thereafter, the timer value TACC is compared with a delay time indicative reference value TDEL which represents lag time between injection timing of the fuel and delivery timing of the fuel to the engine cylinder, at a step S18. Consequently, the time indicative reference value TDEL is variable depending upon the atomization characteristics of the fuel. When the timer value TACC is greater than the time indicative reference value TDEL, process goes to the step S16. On the other hand, when the timer value TACC is smaller than or equal to the time indicative reference value, the FALT flag is set at a step S19. After one of the steps S16 and S19, process goes to a step S20 of Fig. 4(B). At the step S20, a basic induction volumetric efficiency η vo (%) is derived in terms of the intake air pressure data PB. The experimentally derived relationship between the intake air pressure PB and and the induction volumetric efficiency η vo is shown in Fig. 10. In order to derive the basic induction volumetric efficiency η vo , one-dimensional table is set in a memory block 115 of ROM 103, which memory block will be hereafter referred to as η vo map . At a step S21, an engine condition dependent volumetric efficiency correction coefficient K FLAT which will be hereater referred to as K FLAT correction coefficient , and altitude dependent correction coefficient K ALT which will be hereafter referred to as K ALT correction coefficient are read out. Then, at a step S22, an induction volumetric efficiency Q CYL is derived by the following equation: Q CYL = η vo x K FLAT x K ALT After the step S22, in which the induction volume efficiency Q CYL is derived, the intake air temperature signal value Ta is read at a step S23. At the step S23, it is also performed to derive an intake air temperature dependent correction coefficient K TA , which will be hereafter referred to as K TA correction coefficient . Practically, in order to enable derivation of the intake air temperature dependent is performed by map look us against a memory address 116 of ROM 103, in which map of the intake air temperature dependent correction coefficient K TA is set in terms of the intake air temperature Ta. A basic fuel injection amount Tp is derived at a step S24 according to the following equation: Tp = K con x PB x Q CYL x K TA At a step S25, an air intake path area A is derived on the basis of the throttle valve angular position represented by the throttle angle indicative signal TVO and an auxiliary air control pulse width ISC DY which is determined through an engine idling speed control routine illustrated in Figs. 5(a) and 5(b). In practice, the intake air flow path area A TH is derived through map look up by looking a primary path area map set in a memory block 130 in ROM 103 in terms of the throttle valve angular position TVO. Similarly, the auxiliary intake air flow path area A ISC is derived through map look-up by looking up an auxiliary air flow path map set in a memory block 131 of ROM 103 in terms of the duty cycle ISC DY of the auxiliary air control pulse. Respective primary path area map and the auxiliary intake air flow path map are set to vary the value according to variation of the throttle valve angular position TVO and the auxiliaty air control pulse duty cycle ISC DY as shown in block of the step S25. In the practical process of derivation of the intake air path area A at the step S25, a a value A LEAK set in view of an amount of air leaking through a throtle adjusting screw, an air regulator and so forth. Therefore, the intake air path area A can be practically derived by the following equaition: A = A th + A ISC + A LEAK At a step S26, a variation ratio ▵A of the intake air path area A in a unit time, e.g. within an interval of execution cycles, is derived. Thereafore, a lag time t LAG from derivation of the intake air path area variation ratio ▵A to open timing of respective intake valves of the engine cyliders. Practically, the crank angle position at the time of derivation of the intake air path area variation ratio ▵A is detected and compared with preset intake valve open timing of respective intake valve. Therefore, the lag time t LAG as derived is represented by a difference Δϑ of the crank shaft angular position from the angular position at which the intake air path area variation ratio is derived to the crank shaft angular positions at which respective intake valve opens. Therefore, the lag time t LAG is derived as ▵ϑ/N. Then, correction value ▵Tpi (i is a sign showing number of engine cylinder and therefore vaires 1 through 4, in case of the 4-cylinder engine) of the basic fuel injection amount Tp for each cylinder is derived by: ▵Tpi = ▵A/N x t LAG x K where K is a constant set at a value proportional to Tp x N/Q (Q: intake air flow rate) and ▵A is a variation rate of intake air path area A within a unit time (interval between execution cycle) at a step S28. Here, a relationship between the intake air path area A and the intake air flow rate Q can be illustrated as shown in Figs. 11 and 12. As seen from Fig. 12, over the engine speed range between 800 rpm to 6000 rpm, relationship between Q/N and A/Q are maintained to vary substantially linearly proportional to each other. Particularly, at the torque peak, the lineality of the relationship between the Q/N and A/N is clear. Therefore, the intake air flow rate variation ▵Q from derivation timing of the intake air path variation ratio ▵A to the intake value open timing substantially correspond to ▵A/N x t LAG . Therefore, the correction value ▵Tpi derived by the foregoing equation substantially correspond to variation of fuel demand at respective engine cylinder. Based on the correction value ▵Tpi derived at the step S28, the basic fuel injection amount Tpi for respective engine cylinder is derived by: Tpi = Tp + ▵Tpi Then, at a step S30, crank shaft angular position ϑ is checked to detect the cylinder number i utilizing the crank reference signal ϑ ref to which the fuel is to be supplied. Based on the result at the step S30, one of the steps S31 to S34 is selected to set the basic fuel injection amount Tp by the corrected value Tpi at the step S29. At a step S35, a correction coefficient COEF which includes an acceleration enrichment correction coefficient, a cold engine enrichment correction coefficient and so forth as components, and a battery voltage compensating correction value Ts are derived. Derivation of the correction coefficient COEF is performed in per se well known manner which does not require further discussion. At a step S36, an air/fuel ratio dependent feedback correction coefficient K λ which will be hereafter referred to as K λ correction coefficient , and a learning correction coefficient K LRN which is derived through learning process discussed later and will be hereafter referred to as K LRN correction coefficient are read out. Then, at a step S37, the fuel injection amount Ti is derived according to the following equation: Ti = Tp x K λ x K LRN x COEF + Ts The control unit 11 derives a fuel injection pulse having a pulse width corresponding to the fuel injection amount Ti and set the fuel injection pulse in the temporary register in the fuel injection signal output circuit 107. The basic fuel injection amount Tp thus corrected through the routine set forth above, can be utilized for deriving a spark ignition timing. Since the fuel injection amount derived through the foregoing routine is precisely correspond to the instantaneous engine demand, precise spark ignition timing control becomes possible. Particularly, Utilizing the fuel injection amount Tp thus derived allows substantially precise spark igntiion timing control at the engine transition state and is effective for suppression of the engine knocking. Figs. 5(A) and 5(B) show a sequence of routine for deriving an idling speed control pulse signal and assuming altitude. The shown routine in Figs. 5(A) and 5(B) is performed at every 10 ms. The trigger timing of this routine is shifted in phase at 5 ms relative to the routine of Figs. 4(A) and 4(B) and therefore will not interfere to each other. Immediately after starting execution, a signal level of the idle switch signal S IDL from the idle switch 8a is read at a step S41. Then, the idle switch signal level S IDL is checked whether it is one (1) representing the engine idling condition or not, at a step S42. When the idle switch signal level S IDL is zero (0) as checked at the step S42 and thus indicate that the engine is not in idling condition, an auxiliary air flow rate ISC L is set at a given fixed value which is derived on the basis of the predetermined auxiliary air control parameter, such as the engine coolant temperature Tw, at a step S43. On the other hand, when the idle switch signal level S IDL is one as checked at the step S42 and thus represents the engine idling condition, the engine driving condition is checked at a step S44 whether a predetermined FEEDBACK control condition which will be hereafter referred to as ISC condition , is satisfied or not. In the shown embodiment, the engine speed data N, the vehicle speed data VSP and the HIGH level transmission neutral switch signal N T are selected as ISC condition determining parameter. Namely, ISC condition is satisfied when the engine speed data N is smaller than or equal to an idling speed criterion, the vehicle speed data VSP is smaller than a low vehicle speed critrion, e.g. 8 km/h, and the transmission neutral switch signal level is HIGH. When ISC condition is not satisfied as checked at the step S44, the auxiliary air flow control signal ISC L is set at a feedback control value F.B. which is derived to reduce a difference between the actual engine speed and a target engine speed which is derived on the basis of the engine coolant temperature, at a step S45. On the other hand, when the ISC condition is satisfied as checked at the step S44, a boost controlling auxiliary air flow rate ISC BCV is set at a value determined on the basis of the engine speed indicative data N and the intake air temperature Ta for performing boost control to maintain the vacuum pressure in the intake manifold constant, at a step S46. As seen in the block of the step S46 in Fig. 5(A), the auxiliary air flow rate (m³/h) is basically determined based on the engine speed indicative data N and is corrected by a correction coefficient (%) derived on the basis of the intake air temperature Ta. At a step S47, an stable engine auxiliary air flow rate ISC E is drived at a value which can prevent the engine from falling into stall condition and can maintain the stable engine condition. Then, the stable engine auxiliary air flow rate ISC E is compared with the boost controlling auxiliary air flow rate ISC BCV at a step S48. When the boost controlling auxiliary air flow rate ISC BCV is greater than or equal to the stable engine auxiliary air flow rate ISC E , the boost controlling auxiliary air flow rate ISC BVC is set as the auxiliary air control signal value ISC L , at a step S49. On the other hand, when the stable engine auxiliary air flow rate ISC E is greater than the boost controlling auxiliary air flow rate ISC BCV , the auxiliary air control signal value ISC L is set at the value of the stable engine auxiliary air flow rate ISC E at a step S50. After one of the step S49 and S50, the FALT flag is checked at a step S51. When the FALT flag is set as checked at the step S51, an intake air pressure P BD during deceleration versus the engine speed indicative data N is derived at a step S52, which intake air pressure will be hereafter referred to as decelerating intake air pressure . In practice, the decelerating intake air pressure P BD is set in one-dimensional map stored in a memory block 117 in ROM 103. The P BD map is looked up in terms of the engine speed indicative data N. Then, a difference of the intake air pressure P B and the decelerating intake air pressure P BD is derived at a step S53, which difference will be hereafter referred to as pressure difference data ▵BOOST . Utilizing the pressure difference data ▵BOOST derived at the step S53, an assumed altitude data ALT₀ (m) is derived. The assumed altitude data ALT₀ is set in a form of a map set in a memory block 118 so as to be looked up in terms of the pressure difference data ▵BOOST. After one of the step S43, S45 and S54 or when the FALT flag is not set as checked at the step S51, an auxiliary air control pulse width ISC DY which defines duty ratio of OPEN period and CLOSE period of the auxiliary air control valve 19, is derived on the basis of the auxiliary air control signal value at a step S55. Fig. 6 shows a routine for deriving the feedback correction coefficient K λ . The feedback correction coefficient K λ is composed of a proportional (P) component and an integral (I) component. The shown routine is triggered every given timing in order to regularly update the feedback control coefficient K λ . In the shown embodiment, the trigger timing of the shown routine is determined in synchronism with the engine revolution cycle. The feedback control coefficient K λ is stored in a memory block 118 and cyclically updated during a period in which FEEDBACK control is performed. At a step S61, the engine driving condition is checked whether it satisfies a predetermined condition for performing air/fuel ratio dependent feedback control of fuel supply. In practice, a routine (not shown) for governing control mode to switch the mode between FEEDBACK control mode and OPEN LOOP control mode based on the engine driving condition is performed. Basically, FEEDBACK control of air/fuel ratio is taken place while the engine is driven under load load and at low speed and OPEN LOOP control is performed otherwise. In order to selectively perform FEEDBACK control and OPEN LOOP control, the basic fuel injection amount Tp is taken as a parameter for detecting the engine driving condition. For distinguishing the engine driving condition, a map containing FEEDBACK condition indicative criteria Tp ref is set in an appropriate memory block of ROM. The map is designed to be searched in terms of the engine speed N. The FEEDBACK condition indicative criteria set in the map are experimentally obtained and define the engine driving range to perform FEEDBACK control The basic fuel injection amount Tp derived is then compared with the FEEDBACK condition indicative criterion Tp ref . When the basic fuel injection amount Tp is smaller than or equal to the FEEDBACK condition indicative criterion Tp ref a delay timer in the control unit and connected to a clock generator, is reset to clear a delay timer value. On the other hand, when the basic fuel injection amount Tp is greater than the FEEDBACK condition indicative criterion Tp ref the delay timer value t DELAY is read and compared with a timer reference value t ref . If the delay timer value t DELAY is smaller than or equal to the timer reference value t ref , the engine speed data N is read and compared with an engine speed reference N ref . The engine speed reference N ref represents the engine speed criterion between high engine speed range and low engine speed range. Practically, the engine speed reference N ref is set at a value corresponding to a high/low engine speed criteria, e.g. 3800 r.p.m. When the engine speed indicative data N is smaller than the engine speed reference N ref , or after the step 1106, a FEEDBACK condition indicative flag FL FEEDBACK which is to be set in a flag register 119 in the control unit 100, is set. When the delay timer value t DELAY is greater than The timer reference value t ref , a FEEDBACK condition indicative flag FL FEEDBACK is reset. By providing the delay timer to switch mode of control between FEEDBACK control and OPEN LOOP control, hunting in selection of the control mode can be successfully prevented. Furthermore, by providing the delay timer for delaying switching timing of control mode from FEEDBACK control to OPEN LOOP mode, FEEDBACK control can be maintained for the period of time corresponding to the period defined by the timer reference value. This expands period to perform FEEDBACK control and to perform learning. Therefore, at the step S61, a FEEDBACK condition indicative flag FL FEEDBACK is checked. When the FEEDBACK condition indicative flag FL FEEDBACK is not set as checked at the step S61, which indicates that the on-going control mode is OPEN LOOP. Therefore, process directly goes END. At this occasion, since the feedback correction coefficient K λ is not updated, the content in the memory block 118 storing the feedback correction coefficient is held in unchanged. When the FEEDBACK condition indicative flag FL FEEDBACK is set as checked at a step S61, the oxygen concentration indicative signal O₂ from the oxygen sensor 14 is read out at a step S62. The oxygen concentration indicative signal value O₂ is then compared with a predetermined rich/lean criterion V ref which corresponding to the air/fuel ratio of stoichiometric value, at a step S63. In practice, in the process, judgment is made that the air/fuel mixture is lean when the oxygen concentration indicative signal value O₂ is smaller than the rich/lean criterion V ref , a lean mixture indicative flag FL LEAN which is set in a lean mixture indicative flag register 120 in the control unit 100, is checked at a step S64. On the other hand, when the lean mixture indicative flag FL LEAN is set as checked at the step S64, a counter value C of a faulty sensor detecting timer 121 in the control unit 100 is incremented by one (1), at a step S65. The counter value C will be hereafter referred to as faulty timer value . The, the faulty timer value C is compared with a preset faulty timer criterion C₀ which represents acceptable maximum period of time to maintain lean mixture indicative O₂ sensor signal while the oxygen sensor 20 operates in normal state, at a step S66. When the faulty timer value C is smaller than the faulty timer criterion C₀, the rich/lean inversion indicative flag FL INV is reset at a step S67. Thereafter, the feedback correction coefficient K λ is updated by adding a given integral constant (I constant), at a step S68. On the other hand, when the faulty timer value C as checked at the step S66 is greater than or equal to the faulty timer criterion C₀, a faulty sensor indicative flag FL ABNORMAL is set in flag register 123 at a step S69. After setting the faulty sensor indicative flag FL ABNORMAL process goes END. On the other hand, when the lean mixture indicative flag FL LEAN is not set as checked at the step S64, fact of which represents that the air/fuel mixture ratio is adjusted changed from rich to lean, an rich/lean inversion indicative flag FL INV which is set in a flag register 122 in the control unit 100, is set at a step S70. Thereafter, a rich mixture indicative flag FL RICH which is set in a flag register 124, is reset and the lean mixture indicative flag FL LEAN is set, at a step S71. Thereafter, the faulty timer value C in the faulty sensor detecting timer 121 is reset and the faulty sensor indicative flag FL ABNORMAL is reset, at a step S72. Then, the feedback correction coefficient K λ is modified by adding a proportional constant (P constant), at a step S73. On the other hand, when the oxygen concentration indicative signal value O₂ is greater than the rich/lean criterion V ref as checked at the step S63, a rich mixture indicative flag FL RICH which is set in a rich mixture indicative flag register 124 in the control unit 100, is checked at a step S74. When the rich mixture indicative flag FL RICH is set as checked at the step S74, the counter value C of the faulty sensor detecting timer 121 in the control unit 100 is incremented by one (1), at a step S75. The, the faulty timer value C is compared with the preset faulty timer criterion C₀, at a step S76. When the faulty timer value C is smaller than the faulty timer criterion C₀, the rich/lean inversion indicative flag FL INV is reset at a step S77. Thereafter, the feedback correction coefficient K λ is updated by subtracting the I constant, at a step S78. On the other hand, when the faulty timer value C as checked at the step S76 is greater than or equal to the faulty timer criterion C₀, a faulty sensor indicative flag FL ABNORMAL is set at a step S79. After setting the faulty sensor indicative flag FL ABNORMAL process goes END. When the rich mixture indicative flag FL RICH is not set as checked at the step S74, fact of which represents that the air/fuel mixture ratio is just changed from lean to rich, an rich/lean inversion indicative flag FL INV which is set in a flag register 122 in the control unit 100, is set at a step S80. Thereafter, a rich mixture indicative flag FL LEAN is reset and the rich mixture indicative flag FL RICH is set, at a step S81. Thereafter, the faulty timer value C in the faulty sensor detecting timer 121 is reset and the faulty sensor indicative flag FL ABNORMAL is reset, at a step S82. Then, the feedback correction coefficient K λ is modified by subtracting the P constant, at a step S83. After one of the process of the steps S68, S69, S73, S78, S79 and S83, process goes to the END. It should be noted that, in the shown embodiment, the P component is set at a value far greater than that of I component. Figs. 7(A) and 7(B) show a sequence of a routine composed as a part of the main program to be executed by the control unit 11 as the background job. The shown routine is designed to derive K FLAT correction coefficient, K LRN correction coefficient and altitude dependent correction coefficient, and to derive the assumed altitude. At a step S91 which is triggered immediately after starting shown routine, K FLAT correction coefficient is derived in terms of the engine speed data N and the intake air pressure data PB for correcting the basic induction volumetric efficiency η vo . In practice, the K FLAT correction coefficients are set in a form of two-dimensional look-up table in a memory block 125 of ROM 102. Therefore, the K FLAT correction coefficient is derived through map look up in terms of the engine speed data N and the intake air pressure data PB. Here, as will be appreciated that magnitude of variation of the induction volumetric efficiency in relation to variation of the engine speed is relative small. Therefore, the K FLAT correction coefficient can be set as a function of the intake air pressure PB. In this case, since the variation range of the K FLAT correction coefficient can be concentrated in the vicinity of one (1). Therefore, number of grid for storing the correction coefficient values for deriving the K FLAT correction coefficient in terms of the engine speed and the intake air pressure can be small. In addition, since delay of updating of the K FLAT correction coefficient cannot cause substantial error, interval of updating of the K FLAT correction coefficient can be set long enough to perform in the background job. Although the updating interval is relatively long, accuracy in derivation of the induction volumetric efficiency can be substantially improved in comparison with the manner of derivation described in the aforementioned Tokkai Showa 58-41230, in which the correction coefficient is derived solely in terms of the engine speed, since the K FLAT correction coefficient derived in the shown routine is variable depending on not only the engine speed data N but also the intake air pressure PB. At a step S92, the K LRN correction coefficient is derived on the basis of the engine speed data N and the basic fuel injection amount Tp. In order to enable this, a K LRN correction coefficients are set in a form of a two-dimensional look-up map in a memory address 126 in RAM 103. The K LRN correction coefficient derived at the step S92 is modified by adding a given value derived as a function of an average value of K λ correction coefficient for updating the content in the address of the memory block 126 corresponding to the instantaneous engine driving range at a step S93. In practice, updating value K LRN(new) of the K LRN correction coefficient is derived by the following equation: K LRN(new) = K LRN + K λ /M where M is a given constant value. Thereafter, the FALT flag is checked at a step S94. When the FALT flag is not set, process goes END. On the other hand, when the FALT flag is set as checked at the step S94, an error value ▵λ ALT which represents an error from a reference air/fuel ratio (λ = 1) due to altitude variation, at a step S95. In the process done in the step S95, the error value ▵λ ALT corresponds a product by multiplying the average value K λ by the modified K LRN correction coefficient K LRN(new) and the K ALT correction coefficient. At a step S96, an intake air flow rate data Q is derived by multiplying the basic fuel injection amount Tp by the engine speed data N. Then, based on the error value ▵λ ALT derived at the step S95 and the intake air flow rate data Q derived at the step S96, an altitude indicative data ALT₀ is derived from a two-dimensional map stored in a memory block 127 of RAM 103. Here, as will be appreciated, the error value ▵λ ALT is increased according to increasing of altitude which cases decreasing of air density. On the other hand, the error value ▵λ ALT decreases according to increasing of the intake air flow rate Q. Therefore, the variation of the altitude significantly influence for error value ▵λ ALT . Therefore, in practice, the assumed altitude ALT₀ to be derived in the step S97 increases according to decreasing of the intake air flow rate Q and according to increasing of the error value ▵λ ALT . The assumed altitude data ALT₀ is stored in a shift register 128. At a step S98, an average value ALT of the assumed altitude ALT₀ is derived over given number (i) of precedingly derived assumed altitude data ALT₀. For enabling this, the interrupt routine of Fig. 8 is performed at every given timing, e.g. every 10 sec. In the routine of Fig. 8, sorting of the stored assumed altitude data ALT is performed at a step S101. Namely, the shift register 128 is operated to sort the assumed altitude data ALT in order of derivation timing. Namely, most recent data is set as ALT₁ and the oldest data is set as ALt i . At the step S98, the average altitude data ALT is derived by the following equation: ALT = W₀ x ALT₀ + W₁ x ALT₁ ... W i x ALT i where W₀, W₁ ... W i are constant (W₀ > W₁ > ... > W i ; W₀ + W₁ ... W i = 1) Utilizing the intake air flow rate data Q derived at the step S96 and the average altitude data ALT derived at the step S98, the K ALT correction coefficient is derived, at a step S99. In the process of the step S99, map look-up against a two-dimensional map set in a memory block 129 in ROM 102 is performed in terms of the intake flow rate Q and the average altitude data ALT . Here, it will be noted that when the altitude is increased to case decreasing of the atmospheric pressure to reduce resistance for exhaust gas. Therefore, at higher altitude, induction volumetric efficiency is increased even at the same intake air pressure to that in the lower altitude. By this, the air/fuel mixture to be introduced into the engine cylinder becomes leaner. On the other hand, the exhaust pressure becomes smaller as decreasing the intake air flow rate and thus subject greater influence of variation of the atmospheric pressure. Therefore, the K ALT correction coefficient is set to be increased at higher rate as increasing of the average altitude data ALT and as decreasing the intake air flow rate Q. In summary, a fuel injection amount in L-Jetronic type fuel injection is derived on the basis of the engine speed N and the intake air flow rate Q. As is well known, the basic fuel injection amout is derived by: Tp = K cONL x Q/N where K CONL = F/A (F/I gradient) x 1/60 x (number of cylinder) F/A: reciprocal of air/fuel ratio F/I gradient (ms/kg) = 1/(fuel flow rate per injection (ℓ) x ρ ρ: specific gravity of fuel Here, the intake air flow rate Q can be illustrated by: where Pn = P v = 1/2 V₀ x η v x N η v is volumetric efficiency R = Rm (= 29.27) T = Tm PV = nRT K M (equation of state of gas) V₀: total exhaust gas amount M ³ Tm: absolute temperature of intake air T ; n: intake air weight K R: constant of gas M T ⁻¹ From the above equation, the equation for deriving Tp can be modified to: Tp = K CONL x {(N x 60 x V₀)/(2 Rm x Tm ref ) x Pn x η v x K TA }/N where 1/Tm = K TA /Tm ref Tm ref is a reference temperature, e.g. 30 °C K TA is a intake air temperature dependent correction coefficient which becomes 1 when the intake air temperature is reference temperature and increases according to lowering of the intake air temperature below the reference temperature and decreases according to rising of the intake air temperature above the reference temperature. Here, assuming K COND = K CONL x (60 x V₀)/(2 Rm x 303 ° K) the equation for deriving Tp can be modified as follow: where Vro is BDC (bottom dead center) cylinder volume; Vr′ is BDC remained exhaust gas volume; and Vr′ ref is standard remained exhaust gas volume = {1 - 1/E x (Vr′/Vr)}/{1 - 1/E x (Vr′ ref /Vr)} Vr is TDC (top dead center) cylinder volume Vr′/Vr = (Pr/PB) 1/K E: compression ratio; K: relative temperature; Pr: exhaust gas pressure (abs) As will be appreciated herefrom, by employing the K ALT correction coefficient, error in λ control, altitude dependent error versus of the intake air pressure in deceleration or in acceleration at a certain altitude versus that in the standart altitude, can be satisfactorily compensated without requiring an exhaust pressure sensor and atmospheric pressure sensor. Fig. 13 shows a modified routine for deriving the fuel injection amount Ti. In the shown routine, fuel injection amount is increased and decreased with a fuel injection amount correction value dervied on the basis of intake air path area variation speed. Similarly to the former embodiment, various sensor signals, relevant engine driving condition indicative data, such as the engine speed data N, intake air pressure data PB and so forth, at a step S110. Thereafter, at a step S111, an air intake path area A is derived on the basis of the throttle valve angular position represented by the throttle angle indicative signal TVO and the auxiliary air control pulse width ISC DY . Similarlt to the routine shown in Figs. 4(a) to 4(c), the intake air flow path area A TH is derived through map look up by looking a primary path area map set in a memory block 130 in ROM 103 in terms of the throttle valve angular position TVO. Similarly, the auxiliary intake air flow path area A ISC is derived through map look-up by looking up an auxiliary air flow path map set in a memory block 131 of ROM 103 in terms of the duty cycle ISC DY of the auxiliary air control pulse. Therefore, the intake air path area A can be practically derived by the following equaition: A = A th + A ISC + A LEAK At a step S112, a variation ratio ▵A of the intake air path area A in a unit time, e.g. within an interval of execution cycles, is derived. The derived intake air path area variation ratio ▵A is checked at the step S113. When the intake air path area variation ratio ▵A is greater than zero, an enrichment correction coefficient K RICH is dervied at a step S114. Practically, an acceleration enrihment correction value K ACC is derived on the basis of ▵A/N which represents intake air path area variation ratio per engine revolution cycle. Derivation process of the acceleration enrichment value K ACC is performed by looking-up the map set in a memory block (not shown) in ROM 103. At the step S114, the enrichment correction coefficient K RICH is derived by: K RICH = K ACC x A ACC where A ACC is an enrichment correction value derived based on variaous enrichment demand indicative engine parameter, such as an engine coolant temperature Tw and so forth. At a step S115, a fuel injection amount T IR for an acceleration demand responsive asynchronous fuel injection is derived on the basis of ▵A/N and various correction coefficients. The basic asynchronous fuel injection amount TA IR is derived by map look-up performed against a map set in ROM 103 in terms of ▵A/N. By multiplying the derived basic asynchronous fuel injection amount TA IR by the correction coefficients, the asynchronous fuel injection amount T IR is derived. Subsequently, derived fuel injection amount T IR is output at step S116. Therefore, fuel injection for the amount T IR is performed irrespective of the engine revolution cycle for temporary enrichment. On the pther hand, when the intake air path area variation ratio ▵A as checked at the step S113, fuel decreasing correction coefficient K LEAN is derived at a step S117. The fuel decreasing correction coefficient K LEAN is composed of a deceleration demand dependent component KA DEC derived on the basis of |▵A |/N and other correction coefficients. In practice, the fuel decreasing correction coefficient K LEAN is derived by multiplying the deceleration demand dependent component KA DEC by other correction coefficient. When the intake air path area variation ratio ▵A is zero as checked at the step S113, the enrichment correction coefficient K RICH and the fuel decreasing correction coefficient K LEAN are both set to zero at a step S118. After one of the step S116, S117 and S118, basic fuel injection amount Tp is derived substantially the same manner as that performed at the step S24 in the former embodiment, at a step S119. Then, correction values, such as K λ , K LRN , COEF, Ts and so forth are derived or read out at a step S120. In this shown routine, the correction coefficient COEF is derived by the following equaition: COEF = K RICH - K LEAN + K MR + K AS + K AS + K TW ... where K MR is a mixture ratio dependent correction coefficient K AS is an engine start-up enrichment correction coefficient K Tw is an engine coolant temperature dependent correction coefficient. Based on the basic fuel injection amount Tp derived at the step S119 and correction coefficient and correction value derived at the step S120, the fuel injection amount Ti is derived at a step S121. According to this embodiment, the fuel injection control characteristics at the engine transition condition can be signiticantly improved by introducing the factor of the intake air path area variation. Therefore, precise emission control becomes possible to minimize polutant, such as NO x , HC, CO, in the exhaust gas. Furthermore, by this, imcomplete combustion in the vicinity of the spark plug, after burning, hesitation, acceleration shock, shift shock in an automatic transmission can be successfully eliminated. Furthermore, since the shown embodiment of the fuel supply control system derives the basic fuel injection amount by multiplying the intake air pressure PB by the induction volumetric efficiency Q CYL , modifying the product with intake air temperature dependent correction coefficient K TA , and multiplying the modified product by the constant K CON , the resultant value as the basic fuel injection amount can be satisfactorily precise. It should be appreciate that the invention is applicable not only the specific construction of the fuel injection control systems but also for any other constructions of the fuel injection systems.

Claims: A control system for an internal combustion engine, comprising: a) first means (6,8,10,12,14) for monitoring engine driving conditions; b) second means (11;S24) for deriving a basic fuel supply quantity (Tp) on the basis of said engine driving conditions; c) third means (11;S25,S26,S111,S112) for deriving a variation speed (ΔA) of an intake air path area (A) on the basis of the engine driving conditions; d) fourth means (11;S27 to S36;S114 to S120) for deriving a correction value for said basic fuel supply quantity on the basis of the variation speed (ΔA) of the intake air path area; and e) fifth means (11;S37;S121) for controlling the fuel supply quantity on the basis of the basic fuel supply quantity corrected with the correction value characterized in that said third means (S25,S26,S111,S112) derive said intake air path area (A) from an opening angle (TVO) of the throttle valve and an opening angle of a bypass passage (18). Method of controlling an internal combustion engine, comprising the steps of: monitoring (S11) engine driving conditions; deriving a basic fuel supply quantity (Tp) on the basis of said engine driving conditions; deriving (S25,S26,S111,S112) a variation speed (ΔA) of an intake air path area (A) on the basis of the engine driving conditions; deriving (11;S28 to S36; S114 to S120) a correction value for said basic fuel supply quantity on the basis of the variation speed (ΔA) of the intake air path area; and controlling (S37,S121) the fuel supply quantity on the basis of the basic fuel supply quantity corrected with the correction value, characterized in that the step of deriving the variation speed comprises deriving (S25,S26,S111,S112) said intake air path area (A) from an opening angle (TVO) of the throttle valve and an opening angle of a bypass passage (18).

Inventors: NAKINAWA, SHINPEI, TOMISAWA, NAOKI
Applicants: JAPAN ELECTRONIC CONTROL SYSTEMS CO., LTD.
Application year: 1988
Main classification: F02D41
IPC codes: F02D41, F02D37