JPH06241103A - Engine controlling method - Google Patents

Engine controlling method

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Publication number
JPH06241103A
JPH06241103A JP4729593A JP4729593A JPH06241103A JP H06241103 A JPH06241103 A JP H06241103A JP 4729593 A JP4729593 A JP 4729593A JP 4729593 A JP4729593 A JP 4729593A JP H06241103 A JPH06241103 A JP H06241103A
Authority
JP
Japan
Prior art keywords
control
engine
target value
acceleration
transient
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.)
Granted
Application number
JP4729593A
Other languages
Japanese (ja)
Other versions
JP3017615B2 (en
Inventor
Shinji Kimura
信治 木村
Yoshio Sugishima
凱夫 杉島
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Horiba Ltd
Original Assignee
Horiba Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Horiba Ltd filed Critical Horiba Ltd
Priority to JP5047295A priority Critical patent/JP3017615B2/en
Publication of JPH06241103A publication Critical patent/JPH06241103A/en
Application granted granted Critical
Publication of JP3017615B2 publication Critical patent/JP3017615B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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  • Combined Controls Of Internal Combustion Engines (AREA)

Abstract

PURPOSE:To improve following performance and stability of engine control by calculating acceleration up to a target value from rotating speed of an engine and the operating pattern of the target value of torque, and automatically converting control of the engine at the stabilized part and the transient part of the operating pattern. CONSTITUTION:The operating pattern of the target value (101) of rotating speed of an engine is outputted, and the deviation of the target value (101) from a command value (106) is found out. This deviation value is inputted into a control means 102 for carrying out integral control and a control means 103 for carrying out proportional control. Acceleration up to the target value is detected 104 from the stabilized part and the transient part of the operation pattern of the target value, and a converting device 105 is switched and controlled in complanc with the magnitude of the acceleration on the basis of its detected result. Namely, when control of the engine is carried out to the transient part, control of the engine is switched into proportional control for placing emphasis on good following performance. And when control of the engine is carried out to the stabilized part, control of the engine is switched into integral control for placing emphasis on stability so as to control engine while setting the output signal of a selected control means 102 or 103 as a command value 106.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】この発明は、エンジンの回転数や
トルクの目標値の運転パターンから制御値を出力するエ
ンジン制御方法に関するものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an engine control method for outputting a control value from an operation pattern of a target value of engine speed or torque.

【0002】[0002]

【従来の技術】従来この種制御方法は、図4に示すよう
に、ステップ201で目標値を出力し、続いて、フィー
ドバック制御を行い(ステップ202)、制御値を出力
する(ステップ203)ようにしていた。例えば、エン
ジンの回転数−時間特性の運転パターンを示す図2にお
いて、運転パターンを、定常直線Aの定常部Sから直線
的に変化する過渡直線Bの過渡部Tを経て再び定常直線
Cの定常部Sに至るような目標値に設定してある。
2. Description of the Related Art Conventionally, in this type of control method, as shown in FIG. 4, a target value is output in step 201, feedback control is subsequently performed (step 202), and a control value is output (step 203). I was doing. For example, in FIG. 2 showing the operation pattern of the engine speed-time characteristic, the operation pattern is changed from the stationary portion S of the stationary straight line A to the transient portion T of the transient straight line B that changes linearly and then again to the stationary straight line C. The target value is set so as to reach the section S.

【0003】[0003]

【発明が解決しようとする課題】しかし、上記従来の制
御方法では、定常部Sと過渡部Tの全域を、ステップ2
02に示したように、1つの制御だけでカバーしている
から、運転の進行に伴い、図2に細線で示すような、追
従遅れが過渡部Tの上がり部分で発生して過渡直線Bか
ら大きくずれた変位曲線bになったり、過渡部Tに続く
定常部Sではオーバーシュートが大きくなって安定性に
欠ける不安定曲線fを呈するようになる。これでは、目
標値に対しエンジンを精度良く運転するのは難しい。
However, in the above-mentioned conventional control method, the whole area of the steady part S and the transient part T is set to the step 2
As shown in 02, since only one control is covered, a follow-up delay as shown by a thin line in FIG. The displacement curve b deviates greatly, or the steady portion S following the transitional portion T has a large overshoot and exhibits an unstable curve f lacking in stability. With this, it is difficult to operate the engine accurately with respect to the target value.

【0004】この発明は、上記問題に鑑みてなしたもの
で、その目的は、エンジンの回転数やトルクの目標値に
対しエンジンを精度良く運転できるエンジン制御方法を
得ることである。
The present invention has been made in view of the above problems, and an object thereof is to obtain an engine control method capable of accurately operating an engine with respect to target values of engine speed and torque.

【0005】[0005]

【課題を解決するための手段および作用】この発明で
は、エンジンに対する制御を実施するにあたり、自動切
換え手段として、比例制御に積分制御を組み合わせた公
知の(比例+積分)制御動作を用いているけれども、定
常部と過渡部の両方を1つの制御方式でカバーしなけれ
ばならなかったことによるエンジンの運転精度の限界を
克服するために、本発明者らは、加速度を検出して、そ
の大きさにより制御動作を切り換えることができること
に着目した。この観点から、まず、本発明者らは、加速
度を容易に検出できるための運転パターンを、エンジン
の回転数やトルクの目標値に対して導入し、続いて、目
標値から検出される加速度により、定常部と過渡部での
上記問題点を解消するために、その大きさに応じて、定
常部では安定性を重視した制御方式を選択し、一方、過
渡部では、追従性を重視した制御方式を選択するよう制
御を切り換えるのが好ましいと判断するに至った。
According to the present invention, a known (proportional + integral) control operation in which proportional control is combined with integral control is used as automatic switching means for performing control of the engine. In order to overcome the limitation of operating accuracy of the engine due to having to cover both the stationary part and the transient part with one control method, the present inventors have detected acceleration and determined its magnitude. We focused on the fact that the control operation can be switched by. From this point of view, the present inventors first introduce an operation pattern for easily detecting the acceleration with respect to the target value of the engine speed or torque, and then, based on the acceleration detected from the target value. In order to solve the above problems in the steady part and the transient part, a control method that emphasizes stability is selected in the steady part according to its size, while in the transient part, control that emphasizes followability is selected. We have decided that it is preferable to switch the control so as to select the method.

【0006】かくして、この発明は、エンジンの回転数
やトルクの目標値の運転パターンから目標値に対する加
速度を算出し、その算出結果に基づいて、エンジンに対
する制御を運転パターンの定常部と過渡部とで自動切換
えすることからなるエンジン制御方法を提供するもので
ある。
Thus, according to the present invention, the acceleration with respect to the target value is calculated from the operation pattern of the target value of the engine speed or torque, and based on the calculation result, the control of the engine is performed by the steady part and the transient part of the operation pattern. The present invention provides an engine control method including automatic switching by.

【0007】すなわち、この発明は、目標値の加速度算
出により、エンジンに対する制御を運転パターンの定常
部と過渡部とでこれら各部に見合った制御方式を選択す
ることで自動切換えし、それによって、定常部が不安定
であったのを安定にできるとともに、過渡部では追従遅
れが生じていたのを緩和できる。
That is, according to the present invention, by calculating the acceleration of the target value, the control of the engine is automatically switched by selecting the control method corresponding to each of the steady part and the transient part of the operation pattern, and thereby the steady state is achieved. It is possible to stabilize the unstable part and to alleviate the delay in tracking in the transient part.

【0008】[0008]

【実施例】以下、この発明に係るエンジン制御方法の実
施例を、図面に基づいて説明する。図1において、エン
ジン制御方法は、まず、ステップ101で、エンジンの
回転数の目標値の運転パターンを出力し、続いて、フィ
ードバック制御(積分制御)を行う(ステップ102参
照)とともに、異なるフィードバック制御(比例制御)
も行う(ステップ103参照)。一方、図2に示す目標
値の運転パターンの定常部Sおよび過渡部Tから目標値
に対する加速度を算出し(ステップ104参照)、その
算出結果(図3参照)に基づく加速度の大きさにより、
エンジンに対する制御を過渡部Tに対して行う場合に
は、追従性を重視した上記フィードバック制御(比例制
御)に切換え、また、定常部Sに対して行う場合は、安
定性を重視した上記フィードバック制御(積分制御)に
切換える(ステップ105参照)。この際、加速度の大
きさP,Q(P>Q)は、図3に示すように、過渡部T
の方(大きさP)が定常部Sのもの(大きさQ)より大
であるのが一般的である。また、上記切換えは、図3に
おいて、例えば、加速度の大きさがY値(Y=一定)を
基準にすることで行うことができる。また、エンジンに
対する制御(比例/積分)を加速度の大きさP,Qに基
づいて適切に自動切換えする機能を有する自動切換え装
置が備わっている。最後に、ステップ106で、各々の
指令値を制御値として出力する。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS An embodiment of an engine control method according to the present invention will be described below with reference to the drawings. In FIG. 1, in the engine control method, first, in step 101, an operation pattern of a target value of the engine speed is output, and subsequently feedback control (integral control) is performed (see step 102), and different feedback control is performed. (Proportional control)
Is also performed (see step 103). On the other hand, the acceleration with respect to the target value is calculated from the steady portion S and the transitional portion T of the operation pattern of the target value shown in FIG. 2 (see step 104), and the magnitude of the acceleration based on the calculation result (see FIG. 3)
When the control for the engine is performed on the transient portion T, the feedback control (proportional control) that emphasizes followability is switched, and when the control on the steady portion S is performed, the feedback control that emphasizes stability is performed. The mode is switched to (integral control) (see step 105). At this time, the magnitudes P and Q (P> Q) of the acceleration are as shown in FIG.
Is generally larger (size P) than that of the stationary part S (size Q). Further, the above switching can be performed, for example, by referring to the Y value (Y = constant) as the magnitude of acceleration in FIG. Further, an automatic switching device having a function of appropriately and automatically switching control (proportional / integral) to the engine based on the magnitudes P and Q of the acceleration is provided. Finally, in step 106, each command value is output as a control value.

【0009】その結果、図2に点線で示すような曲線
d,gを得た。すなわち、過渡部Tの上がり部分では、
過渡直線Bから大きくずれた変位曲線bに比べて追従遅
れを緩和した形状の変位曲線dになっており、また、過
渡部Tに続く定常部Sではオーバーシュートが大きくな
って安定性に欠ける不安定曲線fに比べてオーバーシュ
ートの小さい安定した安定曲線gを呈しているのが分か
る。
As a result, curves d and g shown by dotted lines in FIG. 2 were obtained. That is, in the rising part of the transitional part T,
The displacement curve b has a shape in which the tracking delay is relaxed as compared with the displacement curve b which is largely deviated from the transient line B, and the steady portion S following the transient portion T has a large overshoot and lacks stability. It can be seen that a stable stable curve g having a smaller overshoot than the stable curve f is exhibited.

【0010】このように本実施例では、エンジンの回転
数やトルクの目標値の運転パターンから目標値に対する
加速度の大きさを求め、その大きさP,Qにより、公知
の制御手法に切換える自動比例/積分切換制御を用いた
ので、追従遅れが過渡部Tの上がり部分で発生したり、
過渡部Tに続く定常部Sではオーバーシュートが大きく
なって安定性に欠けたりすることを防止でき、目標値に
対しエンジンを精度良く運転できる。
As described above, in this embodiment, the magnitude of the acceleration with respect to the target value is obtained from the operation pattern of the target value of the engine speed and the torque, and the proportional P and Q are used to switch to a known control method. Since the / integral switching control is used, a follow-up delay may occur at the rising portion of the transient portion T,
In the steady portion S following the transitional portion T, it is possible to prevent the overshoot from becoming large and lack of stability, and the engine can be operated accurately with respect to the target value.

【0011】[0011]

【発明の効果】以上のようにこの発明では、目標値の加
速度算出により、エンジンに対する制御を運転パターン
の定常部と過渡部とでこれら各部に見合った制御方式を
選択することで自動切換えし、それによって、定常部が
不安定であったのを安定にできるとともに、過渡部では
追従遅れが生じていたのを緩和でき、その結果、エンジ
ンの回転数やトルクの目標値に対する追従性、安定性を
向上でき、エンジンの運転精度が良くなる効果がある。
As described above, according to the present invention, by calculating the acceleration of the target value, the control of the engine is automatically switched by selecting the control method corresponding to each of the steady part and the transient part of the operation pattern. This makes it possible to stabilize the steady part that was unstable, and alleviate the tracking delay that occurred in the transient part.As a result, the trackability and stability of the engine speed and torque to the target values can be reduced. And the operating accuracy of the engine is improved.

【図面の簡単な説明】[Brief description of drawings]

【図1】この発明の一実施例を示すフローチャート構成
説明図である。
FIG. 1 is a flow chart configuration explanatory view showing an embodiment of the present invention.

【図2】エンジンの回転数の目標値の運転パターンおよ
び制御結果を示すエンジンの回転数−時間特性図であ
る。
FIG. 2 is an engine speed-time characteristic diagram showing an operation pattern of a target value of the engine speed and a control result.

【図3】上記実施例における目標値の加速度を示す特性
図である。
FIG. 3 is a characteristic diagram showing acceleration of a target value in the above embodiment.

【図4】従来例を示すフローチャートである。FIG. 4 is a flowchart showing a conventional example.

【符号の説明】[Explanation of symbols]

A,C…目標値の運転パターンの定常直線、B…目標値
の運転パターンの過渡直線、S…目標値の運転パターン
における定常部、T…目標値の運転パターンにおける過
渡部、P,Q…加速度の大きさ。
A, C ... Steady straight line of target value operation pattern, B ... Transient straight line of target value operation pattern, S ... Steady part in target value operation pattern, T ... Transient part in target value operation pattern, P, Q ... The magnitude of acceleration.

Claims (2)

【特許請求の範囲】[Claims] 【請求項1】 エンジンの回転数やトルクの目標値の運
転パターンから目標値に対する加速度を算出し、その算
出結果に基づいて、エンジンに対する制御を運転パター
ンの定常部と過渡部とで自動切換えすることからなるエ
ンジン制御方法。
1. An acceleration for a target value is calculated from an operation pattern of a target value of engine speed and torque, and control of the engine is automatically switched between a steady part and a transient part of the operation pattern based on the calculation result. Engine control method consisting of things.
【請求項2】 自動切換えが、定常部では積分制御を行
い、過渡部では比例制御を行うように施される請求項1
に記載のエンジン制御方法。
2. The automatic switching is performed such that integral control is performed in a steady part and proportional control is performed in a transient part.
The engine control method described in.
JP5047295A 1993-02-12 1993-02-12 Engine control method Expired - Fee Related JP3017615B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP5047295A JP3017615B2 (en) 1993-02-12 1993-02-12 Engine control method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP5047295A JP3017615B2 (en) 1993-02-12 1993-02-12 Engine control method

Publications (2)

Publication Number Publication Date
JPH06241103A true JPH06241103A (en) 1994-08-30
JP3017615B2 JP3017615B2 (en) 2000-03-13

Family

ID=12771298

Family Applications (1)

Application Number Title Priority Date Filing Date
JP5047295A Expired - Fee Related JP3017615B2 (en) 1993-02-12 1993-02-12 Engine control method

Country Status (1)

Country Link
JP (1) JP3017615B2 (en)

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS58165108A (en) * 1982-03-26 1983-09-30 Mitsubishi Heavy Ind Ltd Controller of marine engine
JPS592960U (en) * 1982-06-29 1984-01-10 日野自動車株式会社 Sudden acceleration detection device
JPS5949346A (en) * 1982-09-13 1984-03-21 Japan Electronic Control Syst Co Ltd Air-fuel ratio control device of internal-combustion engine of electronically controlled fuel injection type
JPH0250037A (en) * 1988-05-24 1990-02-20 Stelrad Group Ltd Heating and ventilation unit for high temperature ventilation system
JPH02201060A (en) * 1989-01-31 1990-08-09 Mitsubishi Motors Corp Engine output control device
JPH03275954A (en) * 1990-03-26 1991-12-06 Japan Electron Control Syst Co Ltd Control device for air-fuel ratio of internal combustion engine using fuel of different kind
JPH05106488A (en) * 1991-04-19 1993-04-27 Robert Bosch Gmbh Idling revolution controller for internal combustion engine

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS58165108A (en) * 1982-03-26 1983-09-30 Mitsubishi Heavy Ind Ltd Controller of marine engine
JPS592960U (en) * 1982-06-29 1984-01-10 日野自動車株式会社 Sudden acceleration detection device
JPS5949346A (en) * 1982-09-13 1984-03-21 Japan Electronic Control Syst Co Ltd Air-fuel ratio control device of internal-combustion engine of electronically controlled fuel injection type
JPH0250037A (en) * 1988-05-24 1990-02-20 Stelrad Group Ltd Heating and ventilation unit for high temperature ventilation system
JPH02201060A (en) * 1989-01-31 1990-08-09 Mitsubishi Motors Corp Engine output control device
JPH03275954A (en) * 1990-03-26 1991-12-06 Japan Electron Control Syst Co Ltd Control device for air-fuel ratio of internal combustion engine using fuel of different kind
JPH05106488A (en) * 1991-04-19 1993-04-27 Robert Bosch Gmbh Idling revolution controller for internal combustion engine

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