ENGINE CONTROL SYSTEM

Abstract: An engine control system which controls ignition timing for, and fuel supply to, an engine by scanning a map by using as parameters a first item of data representing the number of revolutions of the engine and a second item of data representing engine load. The engine control system includes filter means for providing a third item of data by suppressing the rate of change of the second item of data. The third item of data is used in place of the second item of data for scanning the map only when the engine is in a pre­ determined range of operating conditions in which the rate of change of a manipulated variable of a throttle valve (34), the number of revolutions of the engine and the rate of change of the engine load are all less than respective predetermined values.

Description: BACKGROUND OF THE INVENTION This invention relates to engine control systems of the type which obtains control data by performing map scanning in accordance with the number of revolutions of an engine and the load applied to the engine, and more particularly it is concerned with an engine control system of the type described which is suitable for controlling internal combustion engines, such as gasoline engines for automotive vehicles. For internal combustion engines (hereinafter engines for short), such as gasoline engines for automotive vehicles, a control system generally referred to as an electronic control type engine control system is known as disclosed in US Patent No. 4,201,161, for example, which is designed to monitor the number of revolutions of an engine and the load applied to the engine and scans a map by using the obtained data as parameters, so as to obtain control data on fuel supply and ignition timing that are necessary for controlling the performance of the engine. The engine control system of the type in which a map is scanned as referred to hereinabove offers the advantage that it responds quickly to changes in engine operating conditions and is capable of admirably coping with a transient condition of the engine, so that engine control can be achieved satisfactorily. However, one problem encountered by this system is that, when the throttle valve is actuated and brought to a condition in which it is nearly fully open, a pulsation appears in the engine torque, with a result that surging occurs in engine speed and spoils riding comfort. SUMMARY OF THE INVENTION This invention has been developed for the purpose of obviating the aforesaid problem of the prior art. Accordingly, the invention has as its object the provision of an engine control system which is capable of suppressing a pulsation in torque while offering the advantage offered by the system relying on map scanning that the system responds quickly to changes in engine operating conditions. To accomplish the aforesaid object, the invention provides means for suppressing the rate of change of data representing a load applied to the engine, so as to obtain, only when the engine is in a predetermined range of operating conditions, at least one coefficient of correction by performing map scanning by using data whose rate of change is suppressed. BRIEF DESCRIPTION OF THE DRAWINGS Fig. 1 is a flow chart of the operation of the engine control system comprising one embodiment of the invention; Fig. 2 is a view of one example of engines equipped with an electronic engine control system which relies on map scanning; Fig. 3 is a view in explanation of a map used in the prior art; Figs. 4 and 5 are diagrams showing character­ istic curves in explanation of a problem encountered in the prior art; Fig. 6 is a view in explanation of the map used in the embodiment of the invention; and Fig. 7 is a view in explanation of the manner in which changes in data on the load applied to the engine are calculated in the present invention. DESCRIPTION OF THE PREFERRED EMBODIMENT Before describing a preferred embodiment of the invention, one example of the engine control system of the electronic control type of the prior art will be outlined by referring to Figs. 2-5. Referring to Fig. 2, an engine control system 1 comprises a microcomputer 2 and a peripheral control circuit 3. Air flow data AF from an air flow sensor which is in the form of a hot wire 20 mounted in a bypass passageway 11 in a suction conduit 10 of the engine, water temperature data WT from a water temperature sensor 21 mounted in an engine cooling water channel 12, air-fuel ratio data λ from an air-fuel ratio sensor 22 mounted in an exhaust pipe 13 of the engine and engine number-of-revolutions data N from a number-of-revolutions sensor, not shown, are fed into the control system 1 which does calculation on the data thus supplied, to provide control signals to a fuel injection valve 30, a bypass valve 31, an exhaust gas recirculation (EGR) control valve 32, a fuel pump 33 and an ignition coil, not shown, so that fuel supply, the number of revolutions for idling and EGR can be re­ gulated by controlling the fuel injection valve 30, bypass valve 31 and EGR control valve 32 respectively. Moreover, ignition control is effected by controlling the initiation and interruption of a current supply to the ignition coil. Meanwhile, the fuel pump 33 is controlled such that it is operated only when the engine key switch is in a starting position and the engine is rotating by its own power. The throttle valve 34 is provided with a throt­ tle sensor (or a throttle switch) 35, so that opening data Q TH for the throttle valve 34 or a signal which is turned on when the throttle valve 34 is brought to an idling condition or when the throttle valve 34 is restored to its original position after the acceleration pedal is released is inputted to the microcomputer 2. In Fig. 2, the fuel injection valve 30 is located downstream of the throttle valve 34 with respect to the direction of flow of air through valve 34 with respect to the direction of flow of air through the suction passageway. It is well known, however, that the fuel injection valve 30 may be mounted upstream of the throttle valve 34. Although not clearly shown in Fig. 2, many engines for which the control system shown is used are what are generally referred to as multicylinder engines provided with a plurality of cylinders. Thus a manifold 10M is located at the downstream end of the suction conduit 10, and another manifold 13M is located at the upstream end of the exhaust pipe 13. Operation of the control system of the prior art constructed as described hereinabove is as follows. The microcomputer 2 processes the air flow data from the air flow sensor 20 and does calculation on an air intake Q A per unit of time, and does calculation on a fuel supply F i per unit time by the following equation based on the air intake Q A per unit time and the data N representing the number of revolutions of the engine: Fi = + K ..... (1) where K: one of various coefficients of correction. Meanwhile the amount of fuel injected by the fuel injection valve 30 per unit of time is fixed, and in this type of system, what is generally referred to as intermittent fuel supply control is effected by setting a fuel injection cycle synchronous with the rotation of the engine, so as to inject fuel for a predetermined time in each injection cycle. Thus the fuel supply F i of equation (1) can be determined by the injection time T i for each injection cycle of the fuel injection valve 30. Therefore, equation (1) can be rewritten as follows: T i = K i ·F i = K i · + K ..... (2) where K i : the coefficient determined by fuel injection valve 30. Thus the control system 1 effects control in such a manner that calculation is done by equation (2) in a predetermined cycle or cyclically every 10 mS, for example, or at a predetermined number of revolutions in synchronism with the rotation of the engine to obtain new injection times T i successively to actuate the fuel injection valve 30 and open same, to provide a predetermined air-fuel ratio. In the foregoing descrip­ tion, the coefficients of correction are described as being represented by K. In actual practice, however, various corrections need be made in a accordance with the operating conditions of the engine, and the coefficients of correction should be expressed as K = (K₁, K₂ ... K n .) Thus, for practical purposes, a quantity T p is set by eliminating the coefficient of correction K from equation (2) and used as a basic amount of injection fuel. T p = K i ..... (3) It is therefore usual practice to effect engine control by providing the basic amount of injected fuel T p with various types of correction. In this electronic engine control system of the prior art, it has hitherto been customary to use, as a coefficient of correction K, a coefficient of correction KMR (KMR = f) which is obtained by performing the scanning of a memory map (a memory from which the stored data is read out by using two parameters) shown in Fig. 3 by using the basic amount of injected fuel T p and the number of revolutions N of the engine. At this time, the basic amount of the injected fuel T p represents the magnitude of a load applied to the engine, so that it will henceforth be referred to as an engine load T p . The same also applies to the ignition timing control referred to hereinabove. That is, the ignition timing is corrected by examining a map by using the engine load T p and the number of revolutions N. The map used is similar to that shown in Fig. 3 and has written thereto beforehand optimum corrections for ignition timing corresponding to the engine load T p and the number of revolutions N which are read out to provide a coefficient of correction KMR. The engine control system in which a map is scanned as described hereinabove offers the advantage that it responds quickly to changes in engine operating conditions and is capable of admirably coping with a transient condition of the engine, so that engine control can be achieved satisfactorily. However, one problem encountered by this system is that, when the throttle valve is actuated and brought to a position in which it is nearly fully open, a pulsation appears in engine torque, with a result that a surging occurs in engine speed and spoils riding comfort. This phenomenon is accounted for by the fact that the map scanning system using the engine load T p has as a parameter the air intake Q A (or the subatmos­ pheric pressure of air taken into the engine) as described hereinabove. The air intake Q A is susceptible to influences exerted by a pulsating stream of air taken into the engine when the throttle valve is nearly fully open. As a result, when the throttle valve is nearly fully open, the data T p representing the engine load shows a pulsation in spite of the load actually applied to the engine showing almost no change, and the coefficient of correction for the amount of injected fuel and the coefficient of correction for the ignition timing obtained by map scanning are also affected by the pulsation. In terms of engine control, the pulsation af­ fecting the coefficients of correction manifests itself was a fluctuation in the air/fuel ratio or in the igni­ tion timing corresponding to the pulsation in suction, when the engine is operating under a constant load. This cause a change to occur in the torque developed by the engine, so that a surging occurs in the engine speed and spoils riding comfort as described hereinabove. In view of the fact that, as shown in Figs. 4 and 5, the coefficient correction λ for the air-fuel ratio and the coefficient of correction τ for the ignition timing show a great change at the subatmos­ pheric pressure of the suction when the throttle valve is nearly fully open, this has great influences on engine performance. According to the invention, means is provided for producing data by suppressing the rate of change of the data representing the engine load whereby the suppressed data can be used for scanning the map only when the engine is in a predetermined range of operating conditions. When the engine is in the predetermined range of operating conditions, suppressed data is used for performing map scanning. A preferred embodiment of the invention will now be described by referring to Figs. 1, 2, 6 and 7. In the embodiment shown, it's hardware is similar to that of the system of the prior art shown in Fig. 2, and the only difference between the invention and the prior art lies in the manner in which map scanning is performed by the control system 1 with no difference existing between them in other points of control. The description will therefore be concerned hereinafter mainly with the map scanning performed in the control system. Fig. 1 is a flow chart for performing map scanning in the embodiment of the control system 1 in conformity with the invention. Map scanning is repeatedly performed once every ten mS, for example. In step 1, the air intake Q A based on the air flow data AF from the air flow sensor 20 and the data N representing the number of revolutions are inputted to the control system 1 which does calculation based thereon to obtain data T p . In step 2, the opening data ϑ TH from the throttle sensor 35 is examined to determine whether or not a change Δϑ TH in the opening data of the throttle valve 34 is more than a predetermined value. In step 3, the number of revolutions N is examined to determine whether or not it is more than a predetermined value. In step 4, it is determined whether or not a change ΔT p in the engine T p is more than a predetermined value. The operation shifts to step 5 only when all the results obtained in steps 2-4 are all in the negative. However, when any one of the results obtained in steps 2-4 is in the affirmative, the operation shifts to step 5 with regard to all the items of data. In steps 5 and 6, data T PDMP (an abbreviation of the damped value of T p ) for scanning a map is obtained. In step 5, the data T p obtained in step 1 is substituted as it is for T PDMP . In step 5, the data T p obtained in step 1 is substituted as it is for T PDMP . In step 6, data T PDMP (new) is obtained by calculating, in a predetermined proportion, a weighted mean of the data T p and the data T PDMP (old) of the previous operation. The predetermined proportion may be α : 1 or α = 1/64, for example. Then, operation shifts to step 7 after step 5 or step 6 is followed. In step 7, a map shown in Fig. 6 is scanned by using the data T PDMP and N, to obtain a coefficient of correction KMR. The difference in the results obtained in effecting control between the case in which the operation shifts from step 5 to step 7 and the case in which the operation shifts from step 6 to step 7 is as follows. In the former case, the data T PDMP used for scanning the map is the engine load T p itself, so that map scanning is performed by using the engine load T p and the number of revolutions N to obtain a coefficient of correction KMR, as is the case with the control system of the prior art outlined hereinabove. Thus the fuel supply or the ignition timing or both of them are corrected. In the latter case in which the operation shifts from step 6 to step 7, the major portion of the data T PDMP (old) used for scanning the map previously with only a portion of the data T p newly inputted being substituted into the data T PDMP , so that the rate of change of the data T p is greatly suppressed. When map scanning is performed by using the data T PDMP (new) in which the rate of change has been greatly suppressed, the appearance in the data T PDMP (new) of a change that is caused by a pulsation of a stream of air taken into the engine is avoided even if such change appears in the data T p . Thus the coefficient of correction KMR obtained by performing map scanning by using the data T PDMP (new) is almost imprevious to the influence exerted by a pulsation of a stream of air taken into the engine. For example, when the proportion (α = 1/64) referred to hereinabove is selected, the rate of change of the data T p can be suppressed to 1/64 by a simple arithmetic. Thus the influences exerted on engine performance by a pulsation of a stream of air taken into the engine can be avoided. When the operation shifts from step 6 to step 7, a delay might occur in effecting engine control, although influences exerted by a pulsation of a stream of air taken into the engine can be avoided because the rate of change of the engine load T p is suppressed as described hereinabove. To obviate this disadvantage, steps 2-4 are followed and step 6 is skipped in this embodiment when engine operating conditions are in a range in which a pulsation of a stream of air taken into the engine poses no serious problem and it is not desirable that the rate of change of the data T p be suppressed and a delay be caused to occur in effecting control of air flow and ignition timing. In this case, the data T p is substituted as it is for the data T PDMP in step 5. Operating conditions of the engine in which step 6 is not followed based on the determinations made in steps 2-4 will be described. Operating conditions of the engine in which step 6 is not followed based on the determinations made in steps 2-4 will be described. In step 2, it is determined whether or not a change ΔϑTH in the throttle valve opening is more than a predetermined value. Thus, when the throttle valve is suddenly operated or when the engine is accelerated or decelerated suddenly, step 6 is not followed. As a result, it is possible to avoid a reduction in the responsiveness of the engine and enables acceleration and deceleration to be satisfactorily achieved. In step 3, a decision is made to skip step 6 when the number of revolutions N of the engine exceeds a predetermined value. Generally, a pulsation of a stream of air taken into the engine markedly affects engine performance when the number of revolutions is low and gives rise to no serious problem when the number of revolutions is high. Meanwhile the operation performed in step 6n leads to a reduction in the responsiveness of the engine to control. Thus, by following step 3, it is possible to avoid an unnecessary reduction in the responsiveness of the engine to control. In step 4, it is determined whether or not the rate of change of the engine load T p has exceeded a predetermined value. When it is determined that the predetermined value is exceeded, step 6 is skipped to thereby enable a delay in effecting control to be avoided when the engine load actually undergoes a change. One example of the calculation done in step 4 to obtain a change ΔT p in the data T p will now be de­ scribed by referring to Fig. 7. When timing data T pn is inputted, the difference between a simple mean A (A = 1/2 T pn + 1/2 T pn-1 ) of the value of data T pn and the value of data T pn-1 obtained in the operation immediately before the operation producing the data T pn and a weighted mean B (B = 1/2 T pn-2 + 1/4 T pn-3 + 1/8 T pn-4 + ...) of the values of data T pn-2 , T pn-3 , T pn-4 ... obtained in operations more than two operations before the operation producing the data T pn , and the difference A - B is used as a change ΔT p . Thus ΔT p = A - B. In this example, it is possible to prevent the engine control system from misoperating when the data T p might undergo a change due to the introduction of a noise, for example. From the foregoing description, it will be appreciated that the invention enables a fluctuation in the torque generated by the engine to be satisfactorily suppressed which might otherwise be caused to occur by a pulsation of a stream of air taken into the engine, without reducing the responsiveness of the control system to operating conditions of the engine. Thus the problem of the prior art that a reduction in riding comfort that might otherwise be caused by a surging of engine speed can be solved. In the embodiment shown and described herein­ above, the engine load T p has been described as being calculated based on the air intake Q A and the data N representing the number of revolutions of the engine. However, the invention is not limited to this specific form of the embodiment and the engine load T p may also be calculated based on the opening of the throttle valve or the subatmospheric pressure of air taken into the engine.

Claims: 1. An engine control system (1) of the type which controls at least one of ignition timing for, and fuel supply to, an engine by scanning a map using as parameters a first item of data representing the number of revolutions of the engine and a second item of data representing engine load, wherein such engine control system (1) comprises: Filter means for providing a third item of data by suppressing the rate of change of said second item of data whereby the map is scanned by using the third item of data in place of the second item of data only when the engine is in a predetermined range of operating conditions. 2. An engine control system as claimed in claim 1, wherein said predetermined range is such that the rate of change of a manipulated variable of a throttle valve (34), the number of revolutions of the engine and the rate of change of the engine load are less than respective predetermined values in the predetermined range of operating conditions. 3. An engine control system as claimed in claim 1, wherein said filter means comprises a processor for providing the third item of data by calculating, in a predetermined proportion, a weighted mean of the current value of the second item of data that is cyclically inputted to the control system and the value of the second data inputted to the control system one cycle before the current value is inputted.

Inventors: MIYAKE, JUNJI, MORITA, KIYOMI
Applicants: HITACHI, LTD.
Application year: 1986
Main classification: F02D41
IPC codes: F02D43, F02D41, F02P5, F02B1