JPH076440B2 - Internal combustion engine control method - Google Patents
Internal combustion engine control methodInfo
- Publication number
- JPH076440B2 JPH076440B2 JP18066887A JP18066887A JPH076440B2 JP H076440 B2 JPH076440 B2 JP H076440B2 JP 18066887 A JP18066887 A JP 18066887A JP 18066887 A JP18066887 A JP 18066887A JP H076440 B2 JPH076440 B2 JP H076440B2
- Authority
- JP
- Japan
- Prior art keywords
- fuel injection
- injection amount
- air
- amount
- value
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- Electrical Control Of Ignition Timing (AREA)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
- Combined Controls Of Internal Combustion Engines (AREA)
Description
【発明の詳細な説明】 〔産業上の利用分野〕 本発明は、内燃機関(以下、エンジンという。)の制御
方法に係り、特に吸入空気量センサ(以下、エアフロー
センサという。)や燃料インジエクタ(以下、インジエ
クタという。)の特性のずれを補償するに好適な制御方
法に関する。Description: TECHNICAL FIELD The present invention relates to a control method for an internal combustion engine (hereinafter referred to as an engine), and particularly to an intake air amount sensor (hereinafter referred to as an air flow sensor) and a fuel injector (hereinafter referred to as an air flow sensor). Hereinafter, it will be referred to as an injector).
一般に、燃料の噴射制御には空燃比フイードバツク方式
が用いられる。この制御方式はエアフローセンサにより
検出した吸入空気量とエンジンの回転数とから基本燃料
噴射量を求め、次いでこの基本燃料噴射量に排ガス中の
O2濃度をフイードバツク量として帰還するO2フードバツ
ク補正係数やその他の補正係数を掛け、これにバツテリ
電圧補正分を加えた値を通常燃料噴射量を算出し、この
算出された通常燃料噴射量をもつてインジエクタの開弁
時間を制御するものである。Generally, an air-fuel ratio feedback system is used for fuel injection control. This control method calculates the basic fuel injection amount from the intake air amount detected by the air flow sensor and the engine speed, and then calculates the basic fuel injection amount to the basic fuel injection amount.
The normal fuel injection amount is calculated by multiplying the O 2 hood back correction factor and other correction factors that return the O 2 concentration as the feed back amount, and adding this value to the battery voltage correction amount to calculate the normal fuel injection amount. This is to control the valve opening time of the injector.
すなわち、通常燃料噴射量に相当するパルス幅(以下、
通常噴射パルス幅という。)Tiは下式により求められ
る。That is, the pulse width corresponding to the normal fuel injection amount (hereinafter,
It is called a normal injection pulse width. ) Ti is calculated by the following formula.
Ti=TP×K2×α×KL+TS ……(1) TP=K1×QA/N ……(2) ここで、TPは基本燃料噴射量に相当する基本噴射パルス
幅,K1は定数,QAは吸入空気量,Nはエンジン回転数,K2は
エンジン冷却水温その他による補正係数,αは空燃比フ
イードバツク(O2フイードバツク)による補正係数,KL
は学習値,TSは、インジエクタの無効パルス幅(バツテ
リ電圧補正分)を表わす。学習制御は空燃比フイードバ
ツクによるαの最大値と最小値の中心値(すなわち、平
均値)からの偏差を学習して学習値KLを得る。これによ
り、常に良好な空燃比が得られる。Ti = T P × K 2 × α × K L + T S (1) T P = K 1 × Q A / N (2) where T P is the basic injection pulse corresponding to the basic fuel injection amount. Width, K 1 is a constant, Q A is the intake air amount, N is the engine speed, K 2 is a correction coefficient based on the engine cooling water temperature, etc., α is a correction coefficient based on the air-fuel ratio feedback (O 2 feedback), and K L
Is the learning value, and T S is the reactive pulse width of the injector (battery voltage correction amount). The learning control learns the deviation from the central value (that is, the average value) of the maximum value and the minimum value of α due to the air-fuel ratio feedback and obtains the learning value K L. As a result, a good air-fuel ratio can always be obtained.
一方、エンジンの出力を最大限に引出すために点火時期
制御も同時に行われるのが普通である。点火時期制御は
基本噴射パルス幅TPとエンジン回転数Nにより制御用プ
ロセツサのメモリ内に格納された制御マツプから補間計
算により求められ、ピストン位置に適合する点火時期に
制御しようとするものである。On the other hand, it is usual that the ignition timing control is also performed at the same time in order to maximize the output of the engine. The ignition timing control is determined by interpolation calculation from the control map stored in the memory of the control processor based on the basic injection pulse width T P and the engine speed N, and the ignition timing is controlled to match the piston position. .
なお、空燃比の学習制御装置として関連するものに、例
えば特開昭58−172242号公報等が挙げられる。Note that, as a device related to the air-fuel ratio learning control device, there is, for example, JP-A-58-172242.
上記した従来技術においては、エアフローセンサの特性
のずれ(後述する第4図参照)が点火時期制御に及ぼす
影響について考慮されていないため、エアフローセンサ
の特性がずれた場合に点火時期にずれが生じるという問
題があつた。すなわち、(2)式からわかるように基本
噴射パルス幅TPには何らの学習結果も反映されていない
ため、エアフローセンサの特性のずれに供なつて基本噴
射パルス幅TPの値も変動し、その結果、誤つた点火時期
をマツプの中から検索することになるからである。な
お、エアフローセンサの特性ずれの原因には、例えば、
製造時のバラツキや経年劣化等がある。In the above-mentioned related art, since the influence of the characteristic deviation of the air flow sensor (see FIG. 4 described later) on the ignition timing control is not taken into consideration, the deviation of the ignition timing occurs when the characteristic of the air flow sensor deviates. There was a problem. That is, (2) because it does not reflect well any learning results the basic injection pulse width T P As seen from the equation, also varies the value of the deviation in the test of connexion basic injection pulse width T P characteristic of the air flow sensor As a result, the incorrect ignition timing is retrieved from the map. The cause of the characteristic deviation of the air flow sensor is, for example,
There are variations during manufacturing and deterioration over time.
一方、経年変化による特性のずれはセンサ類に止まら
ず、アクチユエータ類にも生じることである。エンジン
の空燃比制御において特に問題となるのは、インジエク
タの噴射ノズル径が経年的に拡大するという点である。
インジエクタの特性変化は燃料噴射量に直接関係するの
で空燃比の変動に大きな影響が生じるからである。イン
ジエクタの特性変化は第3図により後述する。On the other hand, the characteristic shift due to aging does not only occur in sensors but also in actuators. A particular problem in controlling the air-fuel ratio of the engine is that the injector nozzle diameter of the injector increases over time.
This is because the change in the characteristics of the injector is directly related to the fuel injection amount and therefore has a great influence on the fluctuation of the air-fuel ratio. The change in characteristics of the injector will be described later with reference to FIG.
本発明の目的は、エアフローセンサおよびインジエクタ
の特性のずれを補償し、エンジンの最大能力を引出しう
る制御方法を提供することにある。It is an object of the present invention to provide a control method capable of compensating for the deviation of the characteristics of the air flow sensor and the injector and drawing out the maximum capacity of the engine.
上記目的は、実際の空燃比の目標値からの偏差を、エア
フローセンサとインジエクタに関連する補正係数にそれ
ぞれ所定の割合にて配分して学習させ、点火時期に関連
する基本噴射量を補正し、かつ、インジエクタに関連す
る通常噴射量を補正することにより達成される。The above-mentioned purpose, the deviation from the target value of the actual air-fuel ratio, the correction coefficient related to the air flow sensor and the injector is learned by allocating at a predetermined ratio, and the basic injection amount related to the ignition timing is corrected, And it is achieved by correcting the normal injection amount related to the injector.
すなわち、本発明は、内燃機関の吸入空気量(QA)およ
び回転数(N)に基づいて基本燃料噴射量(TP)を算出
し、前記回転数および基本燃料噴射量に基づいて点火時
期を制御するとともに、排ガス中の酸素濃度および前記
基本燃料噴射量に基づいて空燃比を目標値に適合させる
べく通常燃料噴射量(Ti)をフイードバツク学習制御
(α,KL)する内燃機関の制御方法において、実際の空
燃比の目標値からの偏差(αmean−1.0)を前記吸入空
気量検出手段および噴射装置の特性変化に応じた割合
(β)で前記基本燃料噴射量の学習値(KL1)ならびに
前記通常燃料噴射量の学習値(KL2)にそれぞれ配分し
て点火時期および通常燃料噴射量を制御することを特徴
とするものである。That is, according to the present invention, the basic fuel injection amount (T P ) is calculated based on the intake air amount (Q A ) and the rotational speed (N) of the internal combustion engine, and the ignition timing is calculated based on the rotational speed and the basic fuel injection amount. Control of the internal combustion engine that controls the fuel injection amount (Ti) in order to adjust the air-fuel ratio to the target value based on the oxygen concentration in the exhaust gas and the basic fuel injection amount (α, K L ). In the method, the deviation (αmean−1.0) from the actual target value of the air-fuel ratio is a learning value (K L1 ) of the basic fuel injection amount at a rate (β) according to the characteristic changes of the intake air amount detection means and the injection device. ) And the learned value (K L2 ) of the normal fuel injection amount, respectively, to control the ignition timing and the normal fuel injection amount.
次に、本発明に係る実施例を図面に基づいて説明する。 Next, an embodiment according to the present invention will be described with reference to the drawings.
第2図に、本発明を適用するエンジン制御システムの概
要を示す。エンジン1に吸入される空気量QAをエアフロ
ーセンサ2で検出し、制御回路3により、通常燃料噴射
量Tiを決定し、インジエクタ4が駆動される。燃焼した
ガスは、排気管に設けたO2センサ5にて空燃比が検出さ
れ、上記制御回路3はこの信号に応じて通常燃料噴射量
Tiをフイードバツク補正し、最適な空燃比を得る。この
時の通常噴射パルス幅Tiは、先に示した(1)式および
(2)式からなる下式により求める。FIG. 2 shows an outline of an engine control system to which the present invention is applied. The air flow sensor 2 detects the air amount Q A drawn into the engine 1, the control circuit 3 determines the normal fuel injection amount Ti, and the injector 4 is driven. The air-fuel ratio of the burned gas is detected by the O 2 sensor 5 provided in the exhaust pipe, and the control circuit 3 responds to this signal by the normal fuel injection amount.
Correct the Ti feed back to obtain the optimum air-fuel ratio. The normal injection pulse width Ti at this time is obtained by the following equations including the equations (1) and (2) shown above.
ここで、K1は定数,QAは吸入空気量,Nはエンジン回転数,
K2はエンジン冷却水温などによる補正係数,αは空燃比
補正係数(O2フイードバツク補正係数),TSはバツテリ
電圧補正分である。O2センサによる空燃比フイードバツ
クは、(1)式の空燃比補正係数αにより行なう。 Where K 1 is a constant, Q A is the intake air amount, N is the engine speed,
K 2 is the correction coefficient based on the engine cooling water temperature, α is the air-fuel ratio correction coefficient (O 2 feed back correction coefficient), and T S is the battery voltage correction. The air-fuel ratio feedback check by the O 2 sensor is performed by the air-fuel ratio correction coefficient α of the equation (1).
ここで、空燃比補正係数αは、初期値1.0(つまり、目
標値と同じ)であり、O2センサ5の出力により第5図に
示す動きをする。実際に用いられる空燃比補正係数とし
ては、αの最大値αmaxと、最小値αminの平均値αmean
が用いられる。この空燃比補正係数の平均値αmeanをも
とに下式により2つの学習値KL1,KL2を求める。The air-fuel ratio correction coefficient α has an initial value of 1.0 (that is, the same as the target value), and the output of the O 2 sensor 5 causes the movement shown in FIG. As the air-fuel ratio correction coefficient actually used, the maximum value αmax of α and the average value αmean of the minimum value αmin are used.
Is used. Based on the average value αmean of the air-fuel ratio correction coefficient, two learning values K L1 and K L2 are obtained by the following formula.
δ1=(αmean−1.0)×β ……(4) δ2=(αmean−1.0)−δ1 ……(5) KL1=KL1(前回迄)+δ1×γ1 ……(6) KL2=KL2(前回迄)+δ2×γ2 ……(7) ここで(4)式は、空燃比補正係数平均値αmeanの1.0
からの偏差の配分割合β分を第1配分係数δ1とする。
第2配分係数δ2は、空燃比補正係数平均値αmeanの1.
0からの偏差から第1配分係数δ1を引いた残りとす
る。インジエクタに関する第1の学習値KL1は第1配分
係数δ1に所定の重みづけ係数γ1をかけて、前回迄の
第1学習値KL1に加算しておく。一方、エアフローセン
サに関する第2学習値KL2も第2配分係数δ2に所定の
重みづけ係数γ2をかけて、前回迄の第2学習値KL2に
加算しておく。各学習値KL1,KL2は第7図のようなマツ
プに格納される。δ 1 = (αmean−1.0) × β …… (4) δ 2 = (αmean−1.0) −δ 1 …… (5) K L1 = K L1 (until the previous time) + δ 1 × γ 1 …… (6) K L2 = K L2 (until last time) + δ 2 × γ 2 (7) Here, equation (4) is 1.0 of the air-fuel ratio correction coefficient average value αmean.
The distribution ratio β of the deviation from is defined as the first distribution coefficient δ 1 .
The second distribution coefficient δ 2 is 1. of the air-fuel ratio correction coefficient average value αmean.
The remainder is obtained by subtracting the first distribution coefficient δ 1 from the deviation from 0. The first learning value K L1 relating to the injector is multiplied by the first distribution coefficient δ 1 by a predetermined weighting coefficient γ 1 and added to the first learning value K L1 up to the previous time. On the other hand, the second learning value K L2 related to the air flow sensor is also added to the second learning value K L2 up to the previous time by multiplying the second distribution coefficient δ 2 by a predetermined weighting coefficient γ 2 . The learning values K L1 and K L2 are stored in a map as shown in FIG.
次に、インジエクタ4とエアフローセンサ2の特性変化
の傾向について説明する。インジエクタ4の場合、第3
図に示すように、通常噴射パルス幅T1と噴射される燃料
の関係を示す勾配がaからbへと変化してゆく。一方、
エアフローセンサ2の場合は、第4図に示すように、吸
入空気量とセンサ2の出力電圧の関係が一定量シフトす
る傾向がある。このことから、吸入空気量の少ない低負
荷域では、エアフローセンサ2の特性変化の影響が大き
く、逆に負荷が増えるに従つて、エアフローセンサ2の
影響が小さくなつてゆく。この点に着目し、前出の配分
割合βをエンジン1の負荷に相当する基本パルス幅T
P((2)式)に応じて第6図の如く変化させることに
より、前記αmeanの1.0からの偏差を、エアフローメー
タとインジエクタの各々の特性の変化を補正することが
できる。Next, the tendency of characteristic changes of the injector 4 and the air flow sensor 2 will be described. In the case of Injector 4, the third
As shown in the figure, the gradient indicating the relationship between the normal injection pulse width T 1 and the injected fuel changes from a to b. on the other hand,
In the case of the air flow sensor 2, as shown in FIG. 4, the relationship between the intake air amount and the output voltage of the sensor 2 tends to shift by a certain amount. From this, in the low load region where the amount of intake air is small, the influence of the characteristic change of the air flow sensor 2 is large, and conversely, as the load increases, the influence of the air flow sensor 2 becomes smaller. Paying attention to this point, the distribution ratio β described above is set to the basic pulse width T corresponding to the load of the engine 1.
By changing it according to P (equation (2)) as shown in FIG. 6, the deviation of αmean from 1.0 can be corrected for the changes in the characteristics of the air flow meter and the injector.
この第1の学習値KL1と第2の学習値KL2を用いて、通常
噴射パルス幅Tiは次式のように求まる。Using the first learning value K L1 and the second learning value K L2 , the normal injection pulse width Ti is obtained by the following equation.
Ti=Tp1×K2×α×KL1+TS ……(8) TP1=K1×QA/N×KL2 ……(9) 上記(9)式からわかるように、新しい基本噴射パルス
幅TP1は第2の学習値KL2を含んでおり、したがつてエア
フローセンサ2の特性変化(第4図)に応じて順次適正
値に修正されることになるため、点火時期マツプを正し
く検索することができる。Ti = Tp 1 × K 2 × α × K L1 + T S・ ・ ・ (8) T P1 = K 1 × Q A / N × K L2 …… (9) As can be seen from the above formula (9), a new basic injection The pulse width T P1 includes the second learning value K L2 , and accordingly, the pulse width T P1 is sequentially corrected to an appropriate value according to the characteristic change of the air flow sensor 2 (FIG. 4). You can search correctly.
また、(8)式からわかるように、通常噴射パルス幅Ti
は上記した正しい値の基本噴射パルス幅TP1をベースに
し、これにインジエクタ4の特性変化(第3図)に応じ
た第1の学習値KL1を含んでいるため、インジエクタ4
の現在の状況に応じた正確な値で求めることができる。Also, as can be seen from equation (8), the normal injection pulse width Ti
Is based on the basic injection pulse width T P1 of the correct value described above, and includes the first learning value K L1 corresponding to the characteristic change of the injector 4 (FIG. 3).
It can be obtained with an accurate value according to the current situation of.
なお、吸入空気量検出手段としてのエアフローセンサに
は、吸気管内圧力とエンジン回転数とから検出する方
式、スロツトル開度とエンジン回転数とから検出する方
式等の種々のものがあるが、本発明はこれらのいずれの
方式においても適用可能であり、同等の効果を得ること
ができる。There are various types of air flow sensors as the intake air amount detecting means, such as a method of detecting from the intake pipe internal pressure and engine speed, a method of detecting from the throttle opening and engine speed, and the like. Can be applied to any of these methods, and an equivalent effect can be obtained.
次に,以上の制御フローを整理して第1図に示し、各ス
テツプ順に説明する。第1図のフローを大別すると、ス
テツプ101〜103は前処理フロー、ステツプ104〜109は本
発明に係る学習処理フロー、ステツプ110は新たな基本
噴射パルス幅TP1の計算フロー、ステツプ111は新たな通
常噴射パルス幅Tiの計算フロー,ステツプ112は点火時
期マツプの検索フローとして考えることができる。Next, the above control flow is summarized and shown in FIG. 1, and will be described in order of each step. The flow of FIG. 1 is roughly divided into steps 101 to 103 for preprocessing, steps 104 to 109 for learning processing according to the present invention, step 110 for calculating a new basic injection pulse width T P1 , and step 111 for The new normal injection pulse width Ti calculation flow, step 112, can be considered as a search flow for the ignition timing map.
まず、エアフローセンサ2およびエンジン回転数センサ
(図示せず)からの出力信号により吸入空気量QAが計算
され、エンジン回転数Nが求められる〔ステツプ10
1〕。First, the intake air amount Q A is calculated from the output signals from the air flow sensor 2 and the engine speed sensor (not shown), and the engine speed N is obtained [Step 10
1].
次に、この吸入空気量QA、エンジン回転数Nおよび定数
K1により、前述の(2)式で基本噴射パルス幅TPが計算
される〔ステツプ102〕。Next, this intake air amount Q A , engine speed N and constant
Based on K 1 , the basic injection pulse width T P is calculated by the above equation (2) [step 102].
次に、O2センサ5の出力信号が取込まれ〔ステツプ10
3〕、ステツプ104においてO2フイードバツク制御中か否
かが判断される〔ステツプ104〕。その結果、フイード
バツク中でない場合(NO)には学習する必要がないので
ステツプ110にジヤンプし、そのまま通常噴射制御およ
び点火時期制御が行われる〔ステツプ110〜112〕。一
方、フイードバツク中である場合(YES)には、フイー
ドバツク量を制御量に反映させて学習する必要があるの
で、次のステツプ105に進む。ステツプ105では、O2セン
サ5の出力信号が反転(第5図参照)したか否かが判断
される。この判断は次のステツプ106の計算の前提とな
る。判断の結果、反転してない場合(NO)は学習できな
いのでステツプ110にジヤンプし、それ以降の通常噴射
制御および点火時期制御が行われる〔ステツプ110〜11
2〕。一方、反転が確認される(YES)と、次のステツプ
106に進む。Next, the output signal of the O 2 sensor 5 is taken in [Step 10
3], it is determined in step 104 whether or not the O 2 feedback back control is being performed [step 104]. As a result, if the feedback is not in progress (NO), there is no need to learn, so the control is skipped to step 110, and normal injection control and ignition timing control are performed as is [steps 110 to 112]. On the other hand, if the feedback is being performed (YES), it is necessary to reflect the feedback amount on the control amount for learning, so the process proceeds to the next step 105. At step 105, it is judged if the output signal of the O 2 sensor 5 is inverted (see FIG. 5). This judgment is a premise for the calculation of the next step 106. As a result of the judgment, if it is not reversed (NO), learning cannot be performed, so the control is jumped to step 110, and the subsequent normal injection control and ignition timing control are performed [steps 110 to 11].
2]. On the other hand, if reversal is confirmed (YES), the next step
Proceed to 106.
ステツプ106では、O2フイードバツク量の最大値αmaxと
最小値αminの平均値αmeanを算出する。At step 106, an average value αmean of the maximum value αmax and the minimum value αmin of the O 2 feedback amount is calculated.
ステツプ107では、先にステツプ102で求めた基本噴射パ
ルス幅TPに応じてエアフローセンサ2の特性変化を考慮
し学習値の配分割合βを第6図の関係から求める。な
お、TPはエンジン1の負荷に相当する値である。At step 107, the learning value distribution ratio β is obtained from the relationship shown in FIG. 6 in consideration of the characteristic change of the air flow sensor 2 in accordance with the basic injection pulse width T P obtained at step 102. Note that T P is a value corresponding to the load of the engine 1.
ステツプ108では、先に求められた配分割合βを加味し
て(4)式により第1配分係数δ1を求め、つづいてこ
の第1配分係数δ1を加味して(5)式により第2配分
係数δ2が計算される。この計算により実際の空燃比の
目標値からの偏差(すなわち、αmean−1.0)を吸入空
気量QAおよびインジエクタの状態に応じた割合で配分す
ることが行われる。In step 108, the first distribution coefficient δ 1 is calculated by the expression (4) by adding the distribution ratio β previously obtained, and then the first distribution coefficient δ 1 is added by the expression (5) by the expression (5). The distribution coefficient δ 2 is calculated. By this calculation, the deviation of the actual air-fuel ratio from the target value (that is, αmean−1.0) is distributed at a rate according to the intake air amount Q A and the state of the injector.
ステツプ108では、求めた第1,第2の各配分係数δ1,δ
2、各重み付け係数γ1,γ2、を前回までの第1学習値
KL1,第2学習値KL2に反映させ((6),(7)式参
照)、新たな各学習値を作成する。In step 108, the obtained first and second distribution coefficients δ 1 , δ
2 , each weighting coefficient γ 1 , γ 2 is the first learning value up to the previous time
This is reflected in K L1 and the second learning value K L2 (see equations (6) and (7)), and new learning values are created.
ステツプ110では、エアフローセンサ2に関する第2の
学習値KL2を基本噴射パルス幅に反映させて新たな基本
噴射パルス幅TP1を作成する。In step 110, the second learned value K L2 for the air flow sensor 2 is reflected in the basic injection pulse width to create a new basic injection pulse width T P1 .
ステツプ111では上記新たな基本噴射パルス幅TP1をベー
スにし、さらにインジエクタ4に関する第1の学習値K
L1を反映させて新たな通常噴射パルス幅Tiを作成する。
以後は次の学習時まで、この通常噴射パルス幅Tiにてイ
ンジエクタ4が制御される。Step 111 is based on the new basic injection pulse width T P1 and the first learning value K for the injector 4 is added.
A new normal injection pulse width Ti is created by reflecting L1 .
Thereafter, the injector 4 is controlled by the normal injection pulse width Ti until the next learning.
ステツプ112では新たな基本噴射パルス幅TP1とエンジン
回転数Nにより点火時期マツプを検索し、検索された正
しい点火時期に制御される。In step 112, the ignition timing map is searched by the new basic injection pulse width T P1 and the engine speed N, and the searched ignition timing is controlled to the correct ignition timing.
本発明によれば、インジエクタと空気量検出手段の各々
の特性変化を区別して学習することができるので、空燃
比と点火時期の両方を正しく制御できるという効果があ
る。According to the present invention, since the characteristic changes of the injector and the air amount detecting means can be learned separately, there is an effect that both the air-fuel ratio and the ignition timing can be correctly controlled.
第1図は本発明に係る実施例を示すフローチヤート、第
2図はエンジン制御装置の概要を示すブロツク図、第3
図はインジエクタの特性を示す説明図、第4図はエアフ
ローセンサの特性を示す説明図、第5図は空燃比フイー
ドバツク量を示す説明図、第6図は基本噴射パルスに応
じた配分割合を示す説明図、第7図は第1および第2の
学習値のマツプ例を示す説明図である。 1……エンジン、2……エアフローセンサ、3……制御
回路、4……インジエクタ、5……O2センサ、104〜109
……学習ステツプ、110……基本噴射パルス幅算出ステ
ツプ、111……通常噴射パルス幅算出ステツプ、112……
点火マツプ検索ステツプ。FIG. 1 is a flow chart showing an embodiment according to the present invention, FIG. 2 is a block diagram showing an outline of an engine control device, and FIG.
FIG. 4 is an explanatory view showing the characteristics of the injector, FIG. 4 is an explanatory view showing the characteristics of the air flow sensor, FIG. 5 is an explanatory view showing the air-fuel ratio feedback back amount, and FIG. 6 is a distribution ratio according to the basic injection pulse. Explanatory drawing, FIG. 7 is explanatory drawing which shows the example of a map of a 1st and 2nd learning value. 1 ... Engine, 2 ... Air flow sensor, 3 ... Control circuit, 4 ... Injector, 5 ... O 2 sensor, 104-109
...... Learning step, 110 …… Basic injection pulse width calculation step, 111 …… Normal injection pulse width calculation step, 112 ……
Ignition map search step.
───────────────────────────────────────────────────── フロントページの続き (51)Int.Cl.6 識別記号 庁内整理番号 FI 技術表示箇所 F02P 5/15 ─────────────────────────────────────────────────── ─── Continuation of the front page (51) Int.Cl. 6 Identification code Internal reference number FI technical display area F02P 5/15
Claims (1)
いて基本燃料噴射量を算出し、前記回転数および基本燃
料噴射量に基づいて点火時期を制御するとともに、排ガ
ス中の酸素濃度および前記基本燃料噴射量に基づいて空
燃比を目標値に適合させるべく通常燃料噴射量をフイー
ドバツク学習制御する内燃機関の制御方法において、 実際の空燃比の目標値からの偏差を前記吸入空気量検出
手段および噴射装置の特性変化に応じた割合で前記基本
燃料噴射量の学習値ならびに前記通常燃料噴射量の学習
値にそれぞれ配分して点火時期および通常燃料噴射量を
制御することを特徴とする内燃機関の制御方法。1. A basic fuel injection amount is calculated based on an intake air amount and a rotational speed of an internal combustion engine, an ignition timing is controlled based on the rotational speed and a basic fuel injection amount, and the oxygen concentration in exhaust gas and the In a control method for an internal combustion engine, in which feedback control is performed on the normal fuel injection amount to adjust the air-fuel ratio to a target value based on the basic fuel injection amount, a deviation of the actual air-fuel ratio from the target value is detected by the intake air amount detection means and In the internal combustion engine, the ignition timing and the normal fuel injection amount are controlled by distributing to the learned value of the basic fuel injection amount and the learned value of the normal fuel injection amount at a rate according to the characteristic change of the injector. Control method.
Priority Applications (5)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP18066887A JPH076440B2 (en) | 1987-07-20 | 1987-07-20 | Internal combustion engine control method |
| US07/215,815 US4991102A (en) | 1987-07-09 | 1988-07-06 | Engine control system using learning control |
| GB8816203A GB2207779B (en) | 1987-07-09 | 1988-07-07 | Engine control system using learning control |
| DE3823277A DE3823277A1 (en) | 1987-07-09 | 1988-07-08 | ENGINE CONTROL SYSTEM |
| KR1019880008489A KR0123561B1 (en) | 1987-07-09 | 1988-07-08 | Engine control system using learning control |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP18066887A JPH076440B2 (en) | 1987-07-20 | 1987-07-20 | Internal combustion engine control method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS6424142A JPS6424142A (en) | 1989-01-26 |
| JPH076440B2 true JPH076440B2 (en) | 1995-01-30 |
Family
ID=16087222
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP18066887A Expired - Fee Related JPH076440B2 (en) | 1987-07-09 | 1987-07-20 | Internal combustion engine control method |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH076440B2 (en) |
Families Citing this family (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5448090A (en) * | 1994-08-03 | 1995-09-05 | International Business Machines Corporation | Structure for reducing parasitic leakage in a memory array with merged isolation and node trench construction |
| WO2006043571A1 (en) | 2004-10-18 | 2006-04-27 | Seiko Epson Corporation | Encapsulation product, process for producing the same, and ink composition |
| JP5034286B2 (en) | 2005-04-19 | 2012-09-26 | セイコーエプソン株式会社 | Method for producing electrophoretic particles |
| JP4207161B2 (en) | 2005-04-20 | 2009-01-14 | セイコーエプソン株式会社 | Microencapsulated metal particles and method for producing the same, aqueous dispersion, and ink jet ink |
| JP2007100575A (en) * | 2005-10-04 | 2007-04-19 | Toyota Motor Corp | Control device for internal combustion engine |
| JP4561667B2 (en) * | 2006-03-28 | 2010-10-13 | トヨタ自動車株式会社 | Fuel supply control device for internal combustion engine |
| CN102892999B (en) * | 2011-05-13 | 2016-03-30 | 丰田自动车株式会社 | Control devices for internal combustion engines |
| DE102021201323A1 (en) * | 2021-02-12 | 2022-08-18 | Robert Bosch Gesellschaft mit beschränkter Haftung | Method and device for operating an internal combustion engine with a predetermined air-fuel mixture |
-
1987
- 1987-07-20 JP JP18066887A patent/JPH076440B2/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| JPS6424142A (en) | 1989-01-26 |
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