JPS638296B2 - - Google Patents
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- Publication number
- JPS638296B2 JPS638296B2 JP55011349A JP1134980A JPS638296B2 JP S638296 B2 JPS638296 B2 JP S638296B2 JP 55011349 A JP55011349 A JP 55011349A JP 1134980 A JP1134980 A JP 1134980A JP S638296 B2 JPS638296 B2 JP S638296B2
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- JP
- Japan
- Prior art keywords
- fuel
- signal
- amount
- air amount
- air
- 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 Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
- Combined Controls Of Internal Combustion Engines (AREA)
- Electrical Control Of Ignition Timing (AREA)
Description
【発明の詳細な説明】
本発明はマイクロコンピユータを利用する内燃
機関の制御装置に係り、特に加速、減速のような
過渡運転時に燃焼室に供給される混合気の空燃
比、混合気量、点火時期をマイクロコンピユータ
を利用して最適状態に調整する内燃機関の制御装
置に関する。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a control device for an internal combustion engine that uses a microcomputer, and in particular controls the air-fuel ratio of the mixture supplied to the combustion chamber during transient operations such as acceleration and deceleration, the amount of the mixture, and the ignition. The present invention relates to a control device for an internal combustion engine that uses a microcomputer to adjust timing to an optimal state.
石油資源の高価格化、環境汚染により自動車エ
ンジンに対して燃費、排出ガス、動力性能を高い
次元で両立させることが求められるようになつ
た。これに対して特開昭54―58116号公報にある
ようなマイクロプロセツサの導入により、各運転
条件における吸入空気量信号、回転数信号より、
あらかじめ記憶されたテーブルから必要燃料量、
点火時期、排気環流量を補間計算、及び、冷却水
温、吸入空気温度による補正計算により求めてい
る。よつて定常運転時には、ほぼ理想的な燃料
量、点火時期、排気環流量を得ることが可能とな
つている。しかしながら、加速、減速のように過
渡運転時には、吸入空気量、回転数信号を取り込
んで燃料量、点火時期を算出するまでに時間がか
かるため、演算終了時にはすでに機関の運転条件
が変化しており、最適な燃料量、点火時期、排気
環流量を得ることは、現在困難な状況にある。し
かし、実用走行状態は大部分が過渡状態の連続で
あり過渡状態における最適な燃料量、点火時期、
排気環流量を得る制御法の確立が望まれている。 Due to the rising price of petroleum resources and environmental pollution, it has become necessary for automobile engines to achieve high levels of fuel efficiency, exhaust emissions, and power performance. In contrast, with the introduction of a microprocessor as described in Japanese Patent Application Laid-Open No. 54-58116, the intake air amount signal and rotation speed signal under each operating condition can be used to
Required fuel amount from a pre-stored table,
The ignition timing and exhaust recirculation amount are determined through interpolation calculations and correction calculations based on cooling water temperature and intake air temperature. Therefore, during steady operation, it is possible to obtain almost ideal fuel amount, ignition timing, and exhaust recirculation amount. However, during transient operations such as acceleration and deceleration, it takes time to take in the intake air amount and rotational speed signals and calculate the fuel amount and ignition timing, so by the time the calculation is finished, the engine operating conditions have already changed. Currently, it is difficult to obtain the optimal fuel amount, ignition timing, and exhaust recirculation amount. However, most of the practical driving conditions are a series of transient conditions, and the optimal fuel amount, ignition timing, and
It is desired to establish a control method to obtain the exhaust recirculation amount.
本発明の目的は過渡運転時にも少なくとも最適
な燃料量、点火時期、を行ない、燃費、排出ガス
の低減を同時に図る内燃機関の制御装置を提供す
ることにある。 SUMMARY OF THE INVENTION An object of the present invention is to provide a control device for an internal combustion engine that maintains at least the optimal fuel amount and ignition timing even during transient operation, thereby simultaneously reducing fuel consumption and exhaust gas.
従来技術の項でも述べたように、コンピユータ
演算に有限時間を要すること、さらに、演算が終
了しても、燃料を噴射するには燃料噴射時期まで
待つて燃料を噴射することになるので、実際の燃
料噴射時には運転条件が変化している。これをさ
けるため、実際の燃料噴射時の運転条件を従来の
データから予測して、即ち燃料噴射時に燃焼室内
に吸入される空気量、機関回転数を予測して、燃
料量、点火時期を演算し、過渡運転時にも常に最
適な燃料量、点火時期となるようにする。 As mentioned in the prior art section, computer calculations require a finite amount of time, and even after the calculations are completed, the fuel must be injected after waiting until the fuel injection timing. Operating conditions are changing at the time of fuel injection. In order to avoid this, the operating conditions during actual fuel injection are predicted from conventional data, that is, the amount of air sucked into the combustion chamber during fuel injection and the engine speed are predicted, and the amount of fuel and ignition timing are calculated. The fuel amount and ignition timing are always optimized even during transient operation.
第1図に本発明に適用される内燃機関制御装置
の構成図を示す。図において、吸入空気は、エア
クリーナ1、スロツトルボデイ2、絞り弁開度ス
イツチ7を有した絞り弁6、吸気管8、吸入弁9
を通つて燃焼室24に入る。吸入空気流量はスロ
ツトルボデイ2のバイパス通路3に設けられた熱
線式の空気流量計4により計測される。さらに1
3は排気管に設けられ排ガス中の酸素濃度を測定
する酸素センサ、12は機関冷却水の温度セン
サ、11はピストンである。燃料は燃料タンク1
7、燃料ポンプ18、燃料ダンパ19、フイルタ
20、燃圧レギユレータ21、燃料パイプ23を
通つて燃料噴射弁5より供給される。なお供給燃
料量はコンピユータ16において空気流量計4、
酸素センサ13、冷却水温センサ12よりの信号
に基づいて決定される。点火時期はコンピユータ
16の信号により点火コイル15で決定され、点
火プラグ10により点火される。なお、14は点
火時期を決めるためのクランク角センサである。 FIG. 1 shows a configuration diagram of an internal combustion engine control device applied to the present invention. In the figure, intake air is supplied to an air cleaner 1, a throttle body 2, a throttle valve 6 having a throttle valve opening switch 7, an intake pipe 8, and an intake valve 9.
through which it enters the combustion chamber 24. The intake air flow rate is measured by a hot wire type air flow meter 4 provided in the bypass passage 3 of the throttle body 2. 1 more
3 is an oxygen sensor provided in the exhaust pipe and measures the oxygen concentration in exhaust gas, 12 is an engine cooling water temperature sensor, and 11 is a piston. Fuel is in fuel tank 1
7. Fuel is supplied from the fuel injection valve 5 through the fuel pump 18, fuel damper 19, filter 20, fuel pressure regulator 21, and fuel pipe 23. The amount of fuel to be supplied is determined by the air flow meter 4,
It is determined based on the signals from the oxygen sensor 13 and the cooling water temperature sensor 12. Ignition timing is determined by an ignition coil 15 based on a signal from a computer 16, and ignition is performed by a spark plug 10. Note that 14 is a crank angle sensor for determining ignition timing.
第2図は、第1図のコンピユータ16の詳細図
である。入力信号としては、吸入空気量計4、機
関冷却水温センサ12、絞り弁開度スイツチ7な
どがある。これらアナログ入力はマチルプレクサ
30に入力され、時分割的に各センサの出力がセ
レクトされADコンバータ31に送られデジタル
信号となる。さらに、ON―OFF信号として入力
される情報、例えば、図示されてないがエンジン
のキースイツチ、スタータスイツチなどで、これ
らは、1ビツトのデジタル信号として扱う。さら
にクランク角センサ14のようにパルス列となる
信号も入力される。CPU33は、デジタル演算
処理を行うプロセシングセントラルユニツトであ
り、ROM32は制御プログラムおよび固定デー
タを格納するための記憶素子であり、RAM34
は読み出しおよび書き込み可能な記憶素子であ
る。I/O回路35は、31及び、各センサから
の信号をCPU33に送つたりCPU33からの信
号を噴射弁5、点火コイル15へ送る機能をも
つ。 FIG. 2 is a detailed diagram of the computer 16 of FIG. Input signals include an intake air amount meter 4, an engine cooling water temperature sensor 12, a throttle valve opening switch 7, and the like. These analog inputs are input to the multiplexer 30, and the outputs of each sensor are selected in a time-division manner and sent to the AD converter 31, where they become digital signals. Further, information inputted as an ON-OFF signal, for example, an engine key switch, a starter switch, etc. (not shown), is handled as a 1-bit digital signal. Further, a signal such as a pulse train from the crank angle sensor 14 is also input. The CPU 33 is a processing central unit that performs digital arithmetic processing, the ROM 32 is a storage element for storing control programs and fixed data, and the RAM 34
is a readable and writable storage element. The I/O circuit 35 has a function of sending signals from 31 and each sensor to the CPU 33, and sending signals from the CPU 33 to the injection valve 5 and the ignition coil 15.
第3図は第1図とは別の内燃機関制御装置であ
り、第1図は燃料噴射弁5が1本であつたのに対
し、第3図では、各シリンダに1本ずつ、シリン
ダ数の数だけの燃料噴射弁を吸入弁のごく近傍に
設けた例である。なお、40は機関が吸入する空
気量を測定する空気流量計41は排気環流量制御
用の弁である。上記の構成において、吸入空気量
信号より噴射燃料量を演算する従来方法について
第4図をもとに説明する。4シリンダ4サイクル
の場合を考えると、例えば第1シリンダに吸気行
程の間の空気流量計信号の代表値(例えば、吸気
行程の間の空気流量計信号の積算値、あるいは、
特定のクランク角における空気流量計信号を第1
シリンダの吸気行程の最後にCPU33に取り込
んで、あらかじめ記憶されたテーブルより燃料流
量を求める。この演算は、第1シリンダの圧縮行
程中に行なわれる。ここで点火順序を1―3―4
―2シリンダの順とすると、燃料噴射は、第1シ
リンダの爆発行程の初期即ち、第4シリンダの吸
入行程の初期に行なわれ、ここで噴射された燃料
は第4シリンダに吸入される。ところが、過渡運
転時には、この時、第4シリンダに吸入される空
気量はすでに第1シリンダの吸入行程のそれとは
異なつており、第4シリンダに吸入される混合気
の空燃比は所期のものとは異なつてくる。第4図
に燃料噴射時に、燃料量算出に使われた空気量信
号を破線Aで、その時、実際に各シリンダに吸入
された空気量を実線Bで示して、両者の時間的関
係を示す。このように演算時間と噴射待ち時間の
ために、定常運転時は問題ないが、過渡運転時に
は、実際にシリンダに入る混合気は、所期のもの
と原理的に大巾に異なつてくる。次にその補正方
法を説明する。 FIG. 3 shows an internal combustion engine control device different from that in FIG. 1, and whereas FIG. 1 had one fuel injection valve 5, in FIG. This is an example in which as many fuel injection valves as the number of fuel injection valves are provided in close proximity to the intake valve. Note that an air flow meter 41 40 that measures the amount of air taken in by the engine is a valve for controlling the flow rate of exhaust gas recirculation. In the above configuration, a conventional method of calculating the amount of injected fuel from the intake air amount signal will be explained with reference to FIG. Considering the case of 4 cylinders and 4 cycles, for example, the first cylinder is provided with a representative value of the air flow meter signal during the intake stroke (e.g., an integrated value of the air flow meter signal during the intake stroke, or
The air flow meter signal at a specific crank angle is
At the end of the cylinder's intake stroke, the fuel flow rate is taken into the CPU 33 and determined from a pre-stored table. This calculation is performed during the compression stroke of the first cylinder. Here, the firing order is 1-3-4
-2 cylinders in this order, fuel injection is performed at the beginning of the explosion stroke of the first cylinder, that is, at the beginning of the suction stroke of the fourth cylinder, and the fuel injected here is sucked into the fourth cylinder. However, during transient operation, the amount of air taken into the fourth cylinder is already different from that during the intake stroke of the first cylinder, and the air-fuel ratio of the mixture taken into the fourth cylinder is the desired one. It comes out differently. In FIG. 4, the air amount signal used to calculate the amount of fuel during fuel injection is shown by a broken line A, and the amount of air actually taken into each cylinder at that time is shown by a solid line B, thereby showing the temporal relationship between the two. Due to the calculation time and injection waiting time, there is no problem during steady operation, but during transient operation, the air-fuel mixture that actually enters the cylinder is fundamentally different from the expected one. Next, the correction method will be explained.
第5図において、第4図で説明したように、時
刻t3において、空気量信号の代表信号Qa3を取り
こんで燃料量を演算して、時刻t4より燃料の噴射
を始める。しかし、その時の実際の吸入空気量は
Qa5である。よつて、時刻t3において、Qa5を推定
する必要がある。その方法の1つとして、t2にお
ける空気量代表信号Qa2,t3におけるQa3信号を用
いて、Qa5の推定値をQa5′とすると
Qa5′=Qa3+X1(Qa3−Qa2) …(1)
ここで、X1は、重み係数で、例えば0.5〜2.0の
値を用いる。これを順次くり返す。減速の場合も
同様である。即ち、空気量信号取込み時の空気量
信号と1つ前の信号とを用いて外挿して実際に燃
料を噴く時の空気量信号を外挿するものである。
第6図にそのフローチヤートを示しており以下説
明する。 In FIG. 5, as explained in FIG. 4 , at time t3, the representative signal Q a3 of the air amount signal is taken in, the fuel amount is calculated, and fuel injection is started from time t4 . However, the actual amount of intake air at that time is
Q a5 . Therefore, it is necessary to estimate Q a5 at time t3 . One method is to use the air amount representative signal Q a2 at t 2 and the Q a3 signal at t 3 , and let the estimated value of Q a5 be Q a5 ′.Q a5 ′=Q a3 +X 1 (Q a3 − Q a2 )...(1) Here, X 1 is a weighting coefficient, and uses a value of 0.5 to 2.0, for example. Repeat this step by step. The same applies to deceleration. That is, the air amount signal when the air amount signal is taken in and the previous signal are used to extrapolate the air amount signal when fuel is actually injected.
The flowchart is shown in FIG. 6 and will be explained below.
ステツプ50において現在の代表空気量信号
Qaoを読み込み、次のステツプ60でRAMに記
憶しておいた前回の代表空気量信号Qao-1を読み
込む。次にステツプ70でQaoとQao-1を用いて噴
射時の推定空気量信号Qao+2を求める。この推定
空気量信号Qao+2は
Qao+2=Qao+X(Qao−Qao-1)
ここでX:係数
により定まる外挿式で求められる。 In step 50, the current representative air amount signal is
Q ao is read, and in the next step 60, the previous representative air amount signal Q ao-1 stored in the RAM is read. Next, in step 70, an estimated air amount signal Q ao+2 during injection is determined using Q ao and Q ao-1 . This estimated air amount signal Q ao+2 is obtained by an extrapolation formula determined by Q ao+2 = Q ao + X (Q ao - Q ao-1 ) where X: coefficient.
そしてステツプ80で推定空気量信号Qao+2で
噴射燃料量が計算される。 Then, in step 80, the amount of fuel to be injected is calculated using the estimated air amount signal Q ao+2 .
第8図は上述した動作を機能的に表わした対応
図で、空気流量計4の信号は外挿手段110へ送
られ、記憶手段120に記憶されていた前回取り
込まれた空気量信号Qao-1と今回取り込まれた空
気量信号Qaoから推定空気量Qao+2を求める。推定
空気量Qao+2が求まると噴射燃料決定手段130
でクランク角センサ14からの回転数信号Nとで
噴射パルスTPを求める。 FIG. 8 is a correspondence diagram functionally representing the above-mentioned operation, in which the signal of the air flow meter 4 is sent to the extrapolation means 110, and the previously captured air amount signal Q ao- stored in the storage means 120 is shown. 1 and the air amount signal Q ao taken in this time, calculate the estimated air amount Q ao+2 . When the estimated air amount Q ao+2 is determined, the injected fuel determining means 130
Then, the injection pulse T P is determined using the rotational speed signal N from the crank angle sensor 14.
さらに、第5図において、空気量の代表信号の
増減より、機関の加減速を検知して、加速、減速
の状況であると判断した場合には、吸気行程の間
の空気量信号の代表値でなく、吸気行程最終時の
空気量信号で、燃料量を演算する方法でも良い。
そのフローチヤートを第7図に示すが、第6図と
同番号は同機能を示している。そして、ステツプ
90において、QaoとQao-1の差が所定値εより大
きいと判断されると加速か減速を表わしているの
で、その場合はステツプ100に移り吸気工程最
終時の空気量信号Qaを読み込む。QaoとQao-1の
差が所定値εより小さいとステツプ70へ移り、
第6図と同様の動作を行う。 Furthermore, in Fig. 5, if the acceleration/deceleration of the engine is detected based on the increase/decrease in the air amount representative signal and it is determined that the engine is in an acceleration or deceleration situation, then the representative value of the air amount signal during the intake stroke is detected. Alternatively, the fuel amount may be calculated using the air amount signal at the end of the intake stroke.
The flowchart is shown in FIG. 7, and the same numbers as in FIG. 6 indicate the same functions. Then, in step 90, if it is determined that the difference between Q ao and Q ao-1 is larger than the predetermined value ε, it indicates acceleration or deceleration, so in that case, the process moves to step 100, where the air amount signal at the end of the intake stroke is Load Q a . If the difference between Q ao and Q ao-1 is smaller than the predetermined value ε, the process moves to step 70;
The same operation as in FIG. 6 is performed.
上述と同様なことが点火時期の設定の場合にも
起る。第5図において、時刻t3において、空気量
信号Qa3と機関回転数N3より点火時期を演算して
例えば20゜BTDCとしても、実際に点火する時刻
t4においては、機関回転数が変化しているため、
適正な点火時期とならない。よつて、時刻t3にお
いて、時刻t4における回転数を推定する必要があ
る。(1)式と同様にして、推定値N4′は、
N4′=N3+X2(N3−N2) …(2)
ここでX2は重み係数である。この推定値
N4′と、時刻t3における代表空気量信号Qa3より点
火時期を演算により求める。 The same thing as described above also occurs when setting the ignition timing. In Fig. 5, at time t3 , if the ignition timing is calculated from the air amount signal Qa3 and the engine speed N3 and is set to 20°BTDC, for example, the actual ignition time.
At t 4 , the engine speed is changing, so
Proper ignition timing is not achieved. Therefore, at time t3 , it is necessary to estimate the rotation speed at time t4 . Similarly to equation (1), the estimated value N 4 ′ is N 4 ′=N 3 +X 2 (N 3 −N 2 ) (2) where X 2 is a weighting coefficient. This estimate
The ignition timing is calculated from N 4 ′ and the representative air amount signal Q a3 at time t 3 .
上記のような補正により、機関の加減速時に
も、燃料室に供給される混合気の空燃比、混合気
量、点火時期を正確に最適値に保つことができる
ものである。 The above-described correction allows the air-fuel ratio of the air-fuel mixture supplied to the fuel chamber, the amount of air-fuel mixture, and the ignition timing to be accurately maintained at optimal values even when the engine is accelerated or decelerated.
第1図は本発明に適用される内燃機関の構成図
である。第2図は、第1図のコンピユータの詳細
を示す図である。第3図は本発明に適用される他
の内燃機関の構成図である。第4図は従来の燃料
量演算法の説明図である。第5図は、本発明の燃
料量演算法の説明図である。第6図,第7図は、
本発明のフローチヤート図、第8図は第6図の対
応機能図である。
4…空気流量計、5…燃料噴射弁、14…クラ
ンク角センサ、15…点火コイル、16…コンピ
ユータ。
FIG. 1 is a block diagram of an internal combustion engine to which the present invention is applied. FIG. 2 is a diagram showing details of the computer of FIG. 1. FIG. 3 is a configuration diagram of another internal combustion engine to which the present invention is applied. FIG. 4 is an explanatory diagram of the conventional fuel amount calculation method. FIG. 5 is an explanatory diagram of the fuel amount calculation method of the present invention. Figures 6 and 7 are
The flowchart of the present invention, FIG. 8, is a functional diagram corresponding to FIG. 6. 4...Air flow meter, 5...Fuel injection valve, 14...Crank angle sensor, 15...Ignition coil, 16...Computer.
Claims (1)
検出手段からの信号に基づいて燃料制御手段を制
御する制御信号を発生する制御装置を備えた内燃
機関の制御装置において、前記制御装置は、今回
取り込まれた空気量信号Qaoと前回取り込んだ空
気量信号Qao-1から燃料噴射時の推定空気量信号
Qaを Qa=Qao+X(Qao−Qao-1) ここでX:係数 よりなる式から求める外挿手段を備えていること
を特徴とする内燃機関の制御装置。[Scope of Claims] 1. A control device for an internal combustion engine comprising a control device that generates a control signal for controlling a fuel control device based on signals from at least an intake air amount detection device and an engine rotation speed detection device, The device calculates the estimated air amount signal at the time of fuel injection from the air amount signal Q ao taken in this time and the air amount signal Q ao-1 taken in last time.
A control device for an internal combustion engine, comprising extrapolation means for calculating Q a from an equation consisting of Q a = Q ao +X (Q ao −Q ao-1 ), where X is a coefficient.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1134980A JPS56107929A (en) | 1980-01-31 | 1980-01-31 | Controller for internal combunstion engine |
| US06/229,840 US4424568A (en) | 1980-01-31 | 1981-01-30 | Method of controlling internal combustion engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1134980A JPS56107929A (en) | 1980-01-31 | 1980-01-31 | Controller for internal combunstion engine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS56107929A JPS56107929A (en) | 1981-08-27 |
| JPS638296B2 true JPS638296B2 (en) | 1988-02-22 |
Family
ID=11775555
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP1134980A Granted JPS56107929A (en) | 1980-01-31 | 1980-01-31 | Controller for internal combunstion engine |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS56107929A (en) |
Families Citing this family (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS58172446A (en) * | 1982-04-02 | 1983-10-11 | Honda Motor Co Ltd | Internal combustion engine operating state control device |
| JPS58174130A (en) * | 1982-04-06 | 1983-10-13 | Nissan Motor Co Ltd | Fuel supply controller of internal-combustion engine |
| JPH0613859B2 (en) * | 1983-03-24 | 1994-02-23 | 日本電装株式会社 | Control device for internal combustion engine |
| JPS59221435A (en) * | 1983-05-31 | 1984-12-13 | Hitachi Ltd | Control method for fuel injection |
| JPS606030A (en) * | 1983-06-22 | 1985-01-12 | Honda Motor Co Ltd | Internal combustion engine operating state control method |
| JPS5915656A (en) * | 1983-06-22 | 1984-01-26 | Honda Motor Co Ltd | Operation state control device of internal-combustion engine |
| DE3486373T2 (en) * | 1983-11-04 | 1995-06-29 | Nissan Motor | Vehicle engine control system with the ability to convey the operating state of the engine and to select the appropriate operating scheme. |
| JPH0647958B2 (en) * | 1984-06-29 | 1994-06-22 | 日産自動車株式会社 | Engine fuel supply controller |
| US4548185A (en) * | 1984-09-10 | 1985-10-22 | General Motors Corporation | Engine control method and apparatus |
| JP2611757B2 (en) * | 1985-06-29 | 1997-05-21 | 三菱自動車工業株式会社 | Engine fuel control device |
| JPS62157260A (en) * | 1985-12-28 | 1987-07-13 | Mikuni Kogyo Co Ltd | fuel supply device |
| JPH07116962B2 (en) * | 1986-03-17 | 1995-12-18 | トヨタ自動車株式会社 | Air-fuel ratio controller for internal combustion engine |
| JPH01113546A (en) * | 1987-10-27 | 1989-05-02 | Japan Electron Control Syst Co Ltd | Internal combustion engine intake air temperature detection device |
| JPH01237333A (en) * | 1987-10-27 | 1989-09-21 | Japan Electron Control Syst Co Ltd | Internal combustion engine control device |
| JPH01125532A (en) * | 1987-11-10 | 1989-05-18 | Japan Electron Control Syst Co Ltd | Controller for internal combustion engine |
| JP2567535B2 (en) * | 1991-12-19 | 1996-12-25 | 本田技研工業株式会社 | Internal combustion engine operating state control device |
| JP3239575B2 (en) * | 1993-08-31 | 2001-12-17 | 株式会社デンソー | Temperature prediction device and temperature control device for internal combustion engine |
| EP1787019A1 (en) * | 2004-08-27 | 2007-05-23 | Optimum Power Technology, L.P. | Predictive engine combustion management |
| JP6583295B2 (en) * | 2017-01-18 | 2019-10-02 | トヨタ自動車株式会社 | Vehicle control device |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6060025B2 (en) * | 1977-10-19 | 1985-12-27 | 株式会社日立製作所 | car control method |
-
1980
- 1980-01-31 JP JP1134980A patent/JPS56107929A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS56107929A (en) | 1981-08-27 |
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