FI125058B - Control system and control method for internal combustion engine, and internal combustion engine - Google Patents
Control system and control method for internal combustion engine, and internal combustion engine Download PDFInfo
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- FI125058B FI125058B FI20145008A FI20145008A FI125058B FI 125058 B FI125058 B FI 125058B FI 20145008 A FI20145008 A FI 20145008A FI 20145008 A FI20145008 A FI 20145008A FI 125058 B FI125058 B FI 125058B
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D43/00—Conjoint electrical control of two or more functions, e.g. ignition, fuel-air mixture, recirculation, supercharging or exhaust-gas treatment
- F02D43/04—Conjoint electrical control of two or more functions, e.g. ignition, fuel-air mixture, recirculation, supercharging or exhaust-gas treatment using only digital means
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/02—Circuit arrangements for generating control signals
- F02D41/14—Introducing closed-loop corrections
- F02D41/1401—Introducing closed-loop corrections characterised by the control or regulation method
- F02D41/1402—Adaptive control
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D28/00—Programme-control of engines
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/30—Controlling fuel injection
- F02D41/38—Controlling fuel injection of the high pressure type
- F02D41/3809—Common rail control systems
- F02D41/3836—Controlling the fuel pressure
- F02D41/3845—Controlling the fuel pressure by controlling the flow into the common rail, e.g. the amount of fuel pumped
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M55/00—Fuel-injection apparatus characterised by their fuel conduits or their venting means; Arrangements of conduits between fuel tank and pump F02M37/00
- F02M55/02—Conduits between injection pumps and injectors, e.g. conduits between pump and common-rail or conduits between common-rail and injectors
- F02M55/025—Common rails
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/02—Circuit arrangements for generating control signals
- F02D41/14—Introducing closed-loop corrections
- F02D41/1401—Introducing closed-loop corrections characterised by the control or regulation method
- F02D2041/1409—Introducing closed-loop corrections characterised by the control or regulation method using at least a proportional, integral or derivative controller
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/02—Circuit arrangements for generating control signals
- F02D41/14—Introducing closed-loop corrections
- F02D41/1401—Introducing closed-loop corrections characterised by the control or regulation method
- F02D2041/141—Introducing closed-loop corrections characterised by the control or regulation method using a feed-forward control element
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/02—Circuit arrangements for generating control signals
- F02D41/14—Introducing closed-loop corrections
- F02D41/1401—Introducing closed-loop corrections characterised by the control or regulation method
- F02D2041/1413—Controller structures or design
- F02D2041/1422—Variable gain or coefficients
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D2200/00—Input parameters for engine control
- F02D2200/02—Input parameters for engine control the parameters being related to the engine
- F02D2200/06—Fuel or fuel supply system parameters
- F02D2200/0602—Fuel pressure
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D2250/00—Engine control related to specific problems or objectives
- F02D2250/31—Control of the fuel pressure
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
- Combined Controls Of Internal Combustion Engines (AREA)
- Feedback Control In General (AREA)
Description
Control system and control method for an internal combustion engine, and an internal combustion engineControl system and control method for an internal combustion engine, and an internal combustion engine
TECHNICAL FIELDTECHNICAL FIELD
The invention concerns in general the technology of internal combustion engines, such as large diesel engines. In particular the invention concerns the way in which feedback control is utilized to control the values of dynamic quantities in the internal combustion engine during its operation.The invention concerns in general technology of internal combustion engines such as large diesel engines. In particular, the invention concerns the way in which the feedback control is utilized to control the values of the dynamic quantities in the internal combustion engine during its operation.
BACKGROUND OF THE INVENTIONBACKGROUND OF THE INVENTION
Operating a modern internal combustion engine, such as a large diesel engine, involves setting up and running a number of feedback control loops to control the respective processes that take place as a part of the operation of the engine. Fig 1 is a schematic illustration of a process 101 and a controller 102 that applies feedback control. A sensor 103 monitors the state of the process 101 and produces a feedback value, which is an indicator of a measured dynamic quantity such as e.g. pressure, temperature, speed, frequency, flow rate, surface level, or the like. The controller 102 compares the feedback value to a setpoint value and produces an output on the basis of the comparison. The output constitutes a control signal to an actuator 104, with the aim of changing the state of the process 101 so that the difference between the feedback value and the setpoint value would become as small as possible. Known feedback control schemes may include for example proportional control, integral control, and/or derivative control. In these the intensity of corrective action depends on current difference to setpoint (proportional), weighted sum of current and previous differences (integral), or slope of the difference over time (derivative).Operating a modern internal combustion engine, such as a large diesel engine, involves setting up and running a number of feedback control loops to control the corresponding processes that take place as part of the operation of the engine. Fig. 1 is a schematic illustration of a process 101 and a controller 102 that apply feedback control. The sensor 103 monitors the state of the process 101 and produces a feedback value which is an indicator of a measured dynamic quantity such as e.g. pressure, temperature, speed, frequency, flow rate, surface level, or the like. The controller 102 Compares the feedback value to a setpoint value and produces an output on the basis of the comparison. The output results in a control signal to an actuator 104, with the aim of changing the state of the process 101 so that the difference between the feedback value and the setpoint value would become as small as possible. Known feedback control schemes may include, for example, proportional control, integral control, and / or derivative control. In these, the intensity of the corrective action depends on the current difference to setpoint (proportional), the weighted sum of the current and previous differences (integral), or the slope of the difference over time (derivative).
Disturbances are factors that tend to change the state of the process 101. Measurable disturbances are those, the effects of which are known beforehand and/or can be measured online with reasonable accuracy. Additionally there are non-measurable disturbances, which may involve e.g. the mechanical wear of components in the process 101. The effect of non-measurable disturbances on the state of the process 101 are difficult, if not impossible, to predict.Disturbances are the factors that tend to change the state of the process 101. Measurable disturbances are those the effects of which are known beforehand and / or can be measured online with reasonable accuracy. Additionally, there are non-measurable disturbances that may involve e.g. the mechanical wear of components in the process 101. The effect of non-measurable disturbances on the state of the process 101 are difficult, if not impossible, to predict.
Pure closed-loop feedback control such as in fig. 1 involves the inherent disadvantage that it only reacts to effects that have already taken place in the process, and thus involves certain latency and dynamics. Fig. 2 illustrates how this disadvantage can be at least partly dealt with by adding an element of feed-forward control. The control system shown in fig. 2 comprises, in addition to the elements explained above in association with fig. 1, a feed-forward controller 201. It is configured to receive one or more input values that are indicative of the currently actual measurable disturbances. The feed-forward controller 201 produces an output that is at least partly based on its input value(s). The outputs of both the feedback controller 102 and the feed-forward controller 201 are coupled to a combiner 202, which delivers their combination as a control signal to the actuator 104. The combination is not necessarily a straightforward sum, but it is intuitive to think that the way in which the actuator 104 should affect the state of the process 101 takes into account the outputs of both controllers.Pure closed-loop feedback control such as in FIG. 1 involves the inherent disadvantage that it only reacts to the effects that it has already taken place in the process, and thus involves certain latency and dynamics. Figure 2 illustrates how this disadvantage can be at least partially dealt with by adding an element of feed-forward control. The control system shown in fig. 2 comprising, in addition to the elements explained above, in association with fig. 1, a feed-forward controller 201. It is configured to receive one or more input values that are indicative of currently measurable disturbances. The feed forward controller 201 produces an output that is at least partially based on its input value (s). The outputs of both the feedback controller 102 and the feed forward controller 201 are coupled to a combiner 202 which delivers their combination as a control signal to the actuator 104. The combination is not necessarily a straightforward sum, but it is intuitive to think. that way in which the actuator 104 should affect the state of the process 101 takes into account the outputs of both controllers.
As an example we may think that the process 101 is common rail fuel injection, and the sensor 103 monitors the pressure in the fuel delivery line delivering fuel to injectors for injecting into cylinders of the internal combustion engine. In this example the actuator 104 drives the flow control valve, which controls the fuel flow into the fuel delivery line (i.e. the rail). A deliberate increase in injection duration is a measurable disturbance. If only feedback control was applied according to fig. 1, the increased injection duration would cause a pressure drop. The sensor 103 would convey decreasing pressure values to the feedback controller 102, which would then try to compensate the measured pressure drop by using the actuator 104 to open more the flow control valve. Latency and dynamics in the feedback control loop would mean that a certain transient drop in the common rail pressure was inevitable.As an example we may think that process 101 is a common rail fuel injection, and sensor 103 monitors the pressure in the fuel delivery line delivering fuel to the injectors for injection into the cylinders of the internal combustion engine. In this example, the actuator 104 drives the flow control valve, which controls the fuel flow into the fuel delivery line (i.e., the rail). Deliberate increase in injection duration is a measurable disturbance. If only feedback control was applied according to fig. 1, the increased injection duration would cause a pressure drop. The sensor 103 would convey the decreasing pressure values to the feedback controller 102, which would then try to compensate the measured pressure drop by using the actuator 104 to open more the flow control valve. Latency and Dynamics in the feedback control loop would mean that a certain transient drop in the common rail pressure was inevitable.
If the control system of fig. 2 was in use, the feed-forward controller 201 would receive information about the increase in injection duration in real time. The feed-forward controller 201 can then react quickly by producing an output signal which, after going through the combiner 202, increases the fuel flow into the rail faster than in the simple feedback control case explained above.If the control system of FIG. 2 was in use, the feed forward controller 201 would receive information about the increase in injection duration in real time. The feed forward controller 201 can then react quickly by producing an output signal which, after going through the combiner 202, increases the fuel flow to the rail faster than in the simple feedback control case explained above.
The weakness of the combined control approach of fig. 2 is that the feedforward controller 201 inevitably operates on the basis of assumptions about how the measurable disturbances will affect the process. Such assumptions may lose their accuracy over time, or they may fail to take into account unexpected changes. For example, in a new engine that receives clean fuel a command to increase injection duration by a certain fraction of crank angle will cause a certain increase in the injected amount of fuel per cycle. If 5000 hours of operation have passed since the last injector overhaul, and/or if the consistency of the fuel is not quite what it should be, the same command may cause a significantly different increase in the injected amount of fuel. Mechanical wear of injectors and varying consistency of fuel are examples of non-measurable disturbances.The weakness of the combined control approach of FIG. 2 is that the feedforward controller 201 inevitably operates on the basis of assumptions about how measurable disturbances will affect the process. Such assumptions may lose their accuracy over time, or they may fail to take into account Unexpected changes. For example, in a new engine that receives clean fuel a command to increase injection duration by a certain fraction of the crank angle will cause a certain increase in the injected amount of fuel per cycle. If 5000 hours of operation have passed since the last injector overhaul, and / or if the consistency of the fuel is not quite what it should be, the same command may cause a significant different increase in the injected amount of fuel. Mechanical wear of injectors and varying consistency of fuel are examples of non-measurable disturbances.
SUMMARY OF THE INVENTIONSUMMARY OF THE INVENTION
The following presents a simplified summary in order to provide a basic understanding of some aspects of various invention embodiments. The summary is not an extensive overview of the invention. It is neither intended to identify key or critical elements of the invention nor to delineate the scope of the invention. The following summary merely presents some concepts of the invention in a simplified form as a prelude to a more detailed description of exemplifying embodiments of the invention. A method, control system, and an internal combustion engine would be needed in which the control approach could take into account also non-measurable disturbances, despite them being non-measurable. The control approach should be versatile so that it could be applied to controlling various processes in the internal combustion engine.The following presents a simple summary in order to provide a basic understanding of some aspects of various invention embodiments. The summary is not an extensive overview of the invention. It is neither intended to identify the key or critical elements of the invention nor to delineate the scope of the invention. The following summary merely presents some concepts of the invention in a simplified form as a prelude to a more detailed description of the exemplifying embodiments. A method, a control system, and an internal combustion engine would be needed in which control approach could take into account also non-measurable disturbances, despite being non-measurable. The control approach should be versatile so that it could be applied to controlling various processes in the internal combustion engine.
Advantageous objectives of the invention are achieved by using a primary controller for feedback-type control and a secondary controller for feed-forward-type control, and by additionally making the secondary controller aware of trends in the output of the primary controller so that the operation of the secondary controller can be changed in an adaptive manner. A desired kind of adaptation of the secondary controller can be implemented so that the aim is to maintain the output of the primary controller at a fixed value, which may be zero or other corresponding "neutral" value. A neutral output of the primary controller is defined as the output the primary controller produces when it does not try to actively affect the state of the controlled process. Filtering, such as taking a mean or median value over a predefined time window, can be applied in order to make the adaptation of the secondary controller concentrate on trends in the primary controller output rather than transients.Advantageous objectives of the invention are achieved by using a primary controller for feedback-type control and a secondary controller for feed-forward-type control, and by addition making the secondary controller aware of Trends in output of the primary controller so that operation of the secondary controller can be changed in an Adaptive Manner. The desired kind of adaptation of the secondary controller can be implemented so that the aim is to maintain the output of the primary controller at a fixed value which may be zero or other corresponding "neutral" value. The neutral output of the primary controller is defined as the output of the primary controller is produced when it does not try to actively affect the state of the controlled process. Filtering, such as taking a mean or median value over a predefined time window, can be applied in order to make the adaptation of the secondary controller Concentrate on Trends in the primary controller output rather than transients.
The exemplary embodiments of the invention presented in this patent application are not to be interpreted to pose limitations to the applicability of the ap pended claims. The verb "to comprise" is used in this patent application as an open limitation that does not exclude the existence of also unrecited features. The features recited in depending claims are mutually freely combinable unless otherwise explicitly stated.The exemplary embodiments of the invention presented in this patent application are not to be interpreted to limit the applicability of the claimed claims. The verb "to comprise" is used in this patent application as an open limitation that does not exclude the existence of also unrecited features. The features recited in depending claims are mutually freely combinable unless otherwise explicitly stated.
The novel features which are considered as characteristic of the invention are set forth in particular in the appended claims. The invention itself, however, both as to its construction and its method of operation, together with additional objects and advantages thereof, will be best understood from the following description of specific embodiments when read in connection with the accompanying drawings.The novel features which are considered as characteristic of the invention are set Forth in particular in the appended claims. The invention itself, however, both as to its construction and its method of operation, together with additional objects and advantages, will be best understood from the following description of specific embodiments when read in conjunction with the accompanying drawings.
BRIEF DESCRIPTION OF DRAWINGSBRIEF DESCRIPTION OF DRAWINGS
Fig. 1 illustrates a prior art feedback control scheme, fig. 2 illustrates a known combination of feedback and feed-forward control, fig. 3 illustrates an adaptive control system and method, fig. 4 illustrates an example of adapting a transfer function, fig. 5 illustrates another example adapting a transfer function, fig. 6 illustrates another example of adapting a transfer function, and fig. 7 illustrates the application of an adaptive control system for control ling fuel pressure in a common rail.Figure 1 illustrates an a prior art feedback control scheme; 2 illustrates a known combination of feedback and feed-forward control, FIG. 3 illustrates an Adaptive control system and method, FIG. 4 illustrates an example of adapting a transfer function, FIG. 5 illustrates another example adapting a transfer function, FIG. 6 illustrates another example of adapting a transfer function, and FIG. 7 illustrates the application of an adaptive control system for control Ling fuel pressure in a common rail.
DETAILED DESCRIPTION OF EMBODIMENTS OF THE INVENTIONDETAILED DESCRIPTION OF EMBODIMENTS OF THE INVENTION
Fig. 3 can be read as an illustration of a control system for an internal combustion engine, by associating the illustrated entities with functional blocks of the control system. Alternatively fig. 3 can be read as an illustration of a method for controlling a process in an internal combustion engine, by associating the illustrated entities with method steps. Both interpretations are explained in more detail below.Fig. 3 can be read as an illustration of a control system for an internal combustion engine by associating illustrated entities with functional blocks of the control system. Alternatively, FIG. 3 can be read as an illustration of a method for controlling a process in an internal combustion engine, by associating illustrated entities with method steps. Both interpretations are explained in more detail below.
As illustrated in fig. 3, the control system comprises a primary controller 301 that is configured to compare a feedback value to a setpoint value and to produce a primary output. The primary output is formed on the basis of said comparison; as a very simple example any change in the primary output may be proportional to the difference between the feedback value and the setpoint value. More elaborate relations between the primary output and the result of the comparison are possible. For example, there may be a "dead zone" of the very smallest comparison results that cause no change in the primary output at all, and/or the proportionality (if any) between any change to the primary output and the difference between the feedback value and the setpoint value may be linear, squared (and signed), or exponential, or it may have some other form.As illustrated in fig. 3, the control system consists of a primary controller 301 that is configured to compare a feedback value to a setpoint value and to produce a primary output. The primary output is formed on the basis of said comparison; as a very simple example any change in the primary output may be proportional to the difference between the feedback value and the setpoint value. More elaborate relationships between the primary output and the result of the comparison are possible. For example, there may be a "dead zone" of very smallest comparison results that cause no change in the primary output at all, and / or proportionality (if any) between any change to the primary output and the difference between the feedback value and setpoint value may be linear, squared (and signed), or exponential, or it may have some other form.
The feedback value is an indicator of a measured dynamic quantity in a process 101 of the internal combustion engine. For example, if the dynamic quantity to be measured is pressure, the sensor 103 is a pressure sensor that may convert the measured pressure to a corresponding voltage, current, or resistance value. The feedback value could be even a mechanical displacement, for example if the measurement of pressure was based on a reversible deformation caused by said pressure, but since the implementation of feedback control typically involves an electronic control system, feedback values in electric form are preferable. A secondary controller 302 is configured to receive an input value and to produce a secondary output. The words "primary" and "secondary" are just names that are used for the sake of unambiguous literal reference, and they include no connotations about e.g. the mutual significance of the control functions, or the respective control functions taking place in some particular order. The input value is schematically shown as coming to the secondary controller 302 from the left, and it is an indicator of a measurable disturbance affecting the process 101.The feedback value is an indicator of the measured dynamic quantity in a process 101 of the internal combustion engine. For example, if the dynamic quantity to be measured is the pressure, the sensor 103 is a pressure sensor that can convert the measured pressure to a corresponding voltage, current, or resistance value. The feedback value could even be a mechanical displacement, for example if the measurement of pressure was based on a reversible deformation caused by the pressure, but since the implementation of the feedback control typically involves an electronic control system, the feedback values in electric form are preferable. The secondary controller 302 is configured to receive an input value and to produce a secondary output. The words "primary" and "secondary" are just names that are used for the sake of unambiguous literal reference, and they include no connotations about e.g. the mutual significance of the control functions, or the corresponding control functions taking place in some particular order. The input value is schematically shown as coming to the secondary controller 302 from the left, and it is an indicator of a measurable disturbance affecting the process 101.
The production of a secondary output in the secondary controller 302 takes place according to a transfer function. A simple example of a transfer function is a time-independent transfer function s = s(t) according to which each input value / results in a corresponding output s. More elaborate transfer functions may be used: for example, if the output s should depend not only on the input / but also at the time t at which the input comes to the secondary controller 302, we may write the general expression s = s(t, t)The production of a secondary output in the secondary controller 302 takes place according to a transfer function. A simple example of a transfer function is a time-independent transfer function s = s (t) according to which each input value / results in a corresponding output s. More elaborate transfer functions can be used: for example, if the output s should depend not only on input / but also at time t at which input comes to secondary controller 302, we may write the general expression s = s (t, t)
The output value s(t) to be produced at a particular time t may include a weighted sum of the current input value i(t) and some previous input values according to the general formula ΣΝ ani(t - ri) n= o where the an are summing weights and the i(t - n) are the input values at times t, (M), (t-2), ... (t-N). The present invention does not place any particular restrictions to the transfer function, but in graphical illustrations and examples it is most straightforward to use a time-independent one-to-one relationship that maps each input value to a corresponding output value. A combiner 303 is coupled to receive the primary output from the primary controller 301 and the secondary output from the secondary controller 302. It is coupled to deliver a combination of them as a control signal to an actuator 104, which in turn is configured to affect the process 101. The word combination is used here in a wide sense. It may mean a simple sum of the primary and secondary outputs, or it may mean a weighted sum, a filtered sum, and/or some other result that takes into account the outputs of both controllers and has a range of possible values that is suited to drive the actuator 104 so that the desired effect on the process 101 is achieved.The output value s (t) to be produced at a particular time t may include the weighted sum of the current input value i (t) and some previous input values according to the general formula ΣΝ ani (t - ri) n = o where the an are summing weights and the i (t - n) are the input values at times t, (M), (t-2), ... (tN). The present invention does not place any particular restrictions on the transfer function, but in graphical illustrations and examples it is now straightforward to use a time-independent one-to-one relationship that maps each input value to the corresponding output value. The combiner 303 is coupled to receive the primary output from the primary controller 301 and the secondary output from the secondary controller 302. It is coupled to deliver a combination of them as a control signal to an actuator 104, which in turn is configured to affect the process 101. The word combination is used here in a wide sense. It may mean a simple sum of the primary and secondary outputs, or it may mean a weighted sum, a filtered sum, and / or some other result that takes into account the outputs of both controllers and has a range of possible values that is suited to drive the actuator 104 so that the desired effect on the process 101 is achieved.
The secondary controller 302 is coupled to receive the primary output as such and/or some derivative thereof. The word derivative as used here means "something that is derived from", and is thus not restricted to e.g. a time derivative. Examples of derivatives meant here are for example a mean or median value of the primary output over a predefined time window.The secondary controller 302 is coupled to receive the primary output as such and / or some derivative number. The word derivative as used here means "something that is derived from" and is thus not restricted to e.g. a time derivative. Examples of derivatives meant here are an example of a mean or median value of a primary output over a predefined time window.
The secondary controller 302 is configured to adapt its transfer function based at least partly on an aim of maintaining the primary output at a fixed value. This fixed value is preferably a so-called neutral value; in other words, the act of adapting the transfer function in the secondary controller aims at achieving a situation in which the primary controller would not try to actively affect the state of the controlled process 101.The secondary controller 302 is configured to adapt its transfer function based on at least a portion of the target to maintain the primary output at a fixed value. This fixed value is preferably a so-called neutral value; in other words, the act of adapting the transfer function in the secondary controller aims at reaching the situation in which the primary controller would not try to actively affect the state of the controlled process 101.
Adapting the transfer function is illustrated in the following with some examples, and with reference to figs. 4, 5, and 6. In fig. 4 the leftmost case illustrates a situation where the transfer function takes initially the form of a rela tively smooth curve. At some moment the secondary controller becomes aware that the primary output (or a derivative thereof, as mentioned above) has the value Aj. The secondary controller is configured to respond by augmenting or scaling all outputs given by the transfer function with a constant that is equal or proportional to the value Ax (being equal is a special case of being linearly proportional, with the linear proportionality constant 1). Augmenting all outputs of the transfer function by Δχ is shown in the middle part of fig. 4. If we assume that the transfer function was initially of the form s = s(i), it is now 5 = s(i) + Aj. As an alternative, if all outputs given by the transfer function would be scaled (rather than augmented) with a constant proportional to the value A1; the new transfer function would be of the form s = aA1s(t). A combination of scaling with a proportionality constant a and augmenting with proportionality constant b, the new transfer function could be expressed as s = a^s{i) + bA±.Adapting the transfer function is illustrated in the following with some examples and with reference to the figs. 4, 5, and 6. In fig. 4 the leftmost case illustrates a situation where the transfer function takes the form of a rela tively smooth curve. At some point the secondary controller becomes aware that the primary output (or a derivative number as mentioned above) has the value Aj. The secondary controller is configured to respond by augmenting or scaling all the outputs given by the transfer function with constant that is equal or proportional to the value Ax (being equal is a special case of being linearly proportional, with linear proportionality constant 1). Augmenting all outputs of the transfer function by Δχ is shown in the middle part of fig. 4. If we assume that the transfer function was originally of the form s = s (i), it is now 5 = s (i) + Aj. As an alternative, if all the outputs given by the transfer function would be scaled (rather than augmented) with a constant proportional to the value A1; the new transfer function would be of the form s = aA1s (t). A combination of scaling with proportionality constant a and augmenting with proportionality constant b, the new transfer function could be expressed as s = a ^ s {i) + bA ±.
The concept of being proportional can be generalized to mean all cases where the magnitude of the augmenting or scaling constant increases unambiguously and monotonously with increasing values of Δ^ Thus dependencies that qualify as proportional are e.g. linear proportionality, exponential proportionality, logarithmic proportionality, and piecewise defined proportionality.The concept of being proportional can be generalized to mean all cases where magnitude of augmentation or scaling constant increases unambiguously and monotonously with increasing values of Δ ^ Thus dependencies that qualify as proportional are e.g. linear proportionality, exponential proportionality, logarithmic proportionality, and piecewise defined proportionality.
Simultaneously the middle part of fig. 4 shows that a next value of the primary output (or a derivative thereof, as mentioned above) is received, and has the value -Δ2. During the time period that is known to have affected the generation of this primary output, the input / to the secondary controller had some other, relatively large value, for which reason the circled-cross symbol of the newly received primary output (or derivative thereof) appears in the right-hand part of the input/output diagram. The following response of the secondary controller in adapting the transfer function is shown in the right part of fig. 4: this time the secondary controller responds by augmenting all outputs of the transfer function by -Δ2. Thus the act of adapting the transfer function means in this case moving the transfer function curve up or down by the amount indicated by the primary output (or derivative thereof).Simultaneously the middle part of fig. 4 shows that the next value of the primary output (or a derivative number as mentioned above) is received, and has the value -Δ2. During the time period that is known to have affected the generation of this primary output, the input / to the secondary controller had some other, relatively large value, for which reason the circled-cross symbol of the newly received primary output (or derivative number) ) appears in the right-hand part of the input / output diagram. The following response of the secondary controller in adapting the transfer function is shown in the right part of FIG. 4: This time the secondary controller responds by augmenting all the outputs of the transfer function by -Δ2. Thus the act of adapting the transfer function means in this case moving the transfer function curve up or down by the amount indicated by the primary output (or derivative paragraph).
Since each step of adapting the transfer function according to the model shown in fig. 4 moves the whole transfer function curve, it is preferable that the value on which the adapting is based is some filtered version of the primary output value, like a mean or median value over a relatively long time window. Also, this kind of approach to adapting the transfer function is most suitable for cases in which we may be reasonably sure about the form of the transfer function, but non-measurable disturbances that are discrete by appearance and take place relatively seldom constitute a basis for the adaptation. An example of such a non-measurable disturbance could be a change in the exact constitution of fuel. When a nearly empty fuel tank is filled to the top from a different source than earlier, the exact constitution of fuel that is available to the engine may change relatively abruptly, but stays more or less the same after that, until the next fill-up.Since each step of adapting the transfer function according to the model shown in FIG. 4 moves the whole transfer function curve, it is preferable to the value on which the adaptation is based on some filtered version of the primary output value, like a mean or median value over a relatively long time window. Also, this kind of approach to adapting the transfer function is most suitable for cases in which we can reasonably be sure about the form of the transfer function, but non-measurable disturbances that are discrete by appearance and take place relatively seldom constitute a basis for the adaptation. An example of such a non-measurable disturbance could be a change in the exact Constitution of fuel. When a nearly empty fuel tank is filled to the top from a different source than before, the exact Constitution of fuel that is available to the engine may change relatively abruptly, but stays more or less the same after that, until the next fill-up .
In fig. 5 the leftmost part illustrates the same starting point as above in fig. 4: the initial form of the transfer function is a relatively smooth curve, and a primary output value (or derivative thereof) is found to have the magnitude Δχ during a period of time when a characteristic input to the second controller was i±. However, in this case the secondary controller does not start moving the whole transfer function curve. Rather, it associates said primary output (or derivative thereof) with a particular sub-range of input values Δί, which includes the input ti that was characteristic for a period of time over which said primary output (or derivative thereof) was obtained. The secondary controller adapts locally the transfer function so that outputs that the previous form of the transfer function gives for inputs within said sub-range are augmented with values proportional to said primary output (or derivative thereof).In FIG. 5 the leftmost part illustrates the same starting point as above in fig. 4: The initial form of the transfer function is a relatively smooth curve, and the primary output value (or derivative equation) is found to have magnitude Δχ during the period of time when the characteristic input to the second controller was i ±. However, in this case the secondary controller does not start moving the whole transfer function curve. Rather, it associates received a primary output (or derivative) with a particular sub-range of input values Δί, which includes the input that was characteristic of the time over which the primary output (or derivative) was obtained. The secondary controller adapts locally the transfer function so that the outputs that the previous form of the transfer function gives for the inputs within said sub-range are augmented with values proportional to said primary output (or derivative number).
The middle part of fig. 5 shows one example of such local adapting. Within the sub-range of input values Δί, the transfer function curve is stretched so that it reaches the point that was above the original transfer function curve by Δχ. In order not to create discontinuities in the transfer function curve, the effect of the adaptation is inversely proportional to the difference between the respective input and the characteristic input mentioned above. Another possibility would have been to cut a piece of the original transfer function curve within the sub-range of input values Δί, and to move that piece translationally upwards by Δ1; but that would naturally result in a discontinuity in the transfer function curve at both ends of the sub-range Δί.The middle part of fig. 5 shows one example of such local adapting. Within the sub-range of input values Δί, the transfer function curve is stretched so that it reaches the point that was above the original transfer function curve by Δχ. In order not to create discontinuities in the transfer function curve, the effect of adaptation is inversely proportional to the difference between the corresponding input and the characteristic input mentioned above. Another possibility would have been to cut a piece of the original transfer function curve within the sub-range of input values Δί, and to move that piece translationally upwards by Δ1; but that would naturally result in a discontinuity in the transfer function curve at both ends of the sub-range Δί.
Mathematically the adapted transfer function could be expressed asMathematically, the adapted transfer function could be expressed as
when ί E Δί elsewhere where t(i) is an augmentation function that is defined within the sub-range of input values M. The middle part of fig. 5 also shows that the next received primary output (or derivative thereof) is associated with a significantly larger concurrent input value, and is below the (original!) transfer function curve by Δ2. The rightmost part of fig. 5 shows how also in that case the transfer function has been adapted locally so that outputs that the previous form of the transfer function gives for inputs within the appropriate sub-range (not separately shown) are augmented with values proportional to said primary output (or derivative thereof). Again, graphically the result seems like stretching the transfer function curve so that one part of it reaches the point at which the circled-cross symbol appeared.when ί E Δί elsewhere where t (i) is an augmentation function that is defined within the sub-range of input values M. The middle part of fig. 5 also shows that the next received primary output (or derivative) is associated with a significantly larger concurrent input value, and is below the (original!) Transfer function curve by Δ2. The rightmost part of fig. 5 shows how the transfer function has been adapted locally so that the outputs that the previous form of the transfer function gives for inputs within the appropriate sub-range (not shown separately) are augmented with values proportional to said primary output (or derivative paragraph). Again, graphically the result seems like stretching the transfer function curve so that one part of it reaches the point at which the circled-cross symbol appeared.
Repeated adaptations of the transfer function in this way will eventually adapt the transfer function curve so that in its adapted form it goes through all points in the input/output plane for which a corresponding primary output (or derivative thereof) has been received. Such an approach to adapting is well suited for cases in which it would be difficult to define exactly the most optimal transfer function on the basis of pre-existing information only.Repeated adaptations of the transfer function in this way will eventually adapt the transfer function to the curve so that it adapts through all points in the input / output plan for which corresponding primary output (or derivative paragraph) has been received. Such an approach to adapting is well suited for cases in which it would be difficult to define exactly the most optimal transfer function on the basis of pre-existing information only.
Fig. 6 illustrates yet another example of adapting a transfer function. In this case the secondary controller has the nature of a self-organizing map or neural network, and it is coupled to receive two different and mutually independent types of input values. In this schematic illustration we assume that each possible pair of received values (INPUT 1, INPUT 2) makes the secondary controller produce a secondary output, the value of which is represented by the phase angle (angle in relation to the horizontal direction to the right) of the corresponding arrow in the drawing. The transfer function is equal to the unambiguous mapping from each possible pair of input values to the corresponding output value.Figure 6 illustrates yet another example of adapting a transfer function. In this case, the secondary controller has the nature of a self-organizing map or neural network, and it is coupled to receive two different and mutually independent types of input values. In this schematic illustration, we assume that each possible pair of received values (INPUT 1, INPUT 2) makes the secondary controller produce a secondary output, the value represented by the phase angle (angle in relation to the horizontal direction to the right ) of the corresponding arrow in the drawing. The transfer function is equal to the unambiguous mapping from each possible pair of input values to the corresponding output value.
On the left in fig. 6 we assume that a primary output (or derivative thereof) is received in the secondary controller, and said primary output concerns a time period during which a particular characteristic pair of values (INPUT 1, INPUT 2) is received by the secondary controller as represented by point 601. We also assume that the secondary output value that was previously associated with this pair of input values was the one represented with a dashed line to the upper right from the point 601. The received primary output (or derivative thereof) defines the new secondary output value 603 in a way that is analo gous to that applied above in figs. 4 and 5: it is assumed that if the secondary output had already had the value 603, the corresponding primary output would have had a neutral value. A further assumption in the left-hand part of fig. 6 is that the concept "subrange of input values" that was used in association with fig. 5 has a corresponding two-dimensional form in the self-organizing map or neural network. In other words, the effect of changing the output value associated with point 601 will "bleed" into its immediate surroundings, and cause similar (yet smaller) changes in the output values associated with neighboring points. The points that will be affected are those that fit in the elliptical region 604. The right-hand side of fig. 6 shows the self-organizing map or neural network after the whole adaptation round has been made. Dashed lines illustrate the previous output values associated with those points for which a new output value was defined as a part of adapting the transfer function (note that the previous value for the actual point 601 is not shown any more on the right, because it was already shown in the left-hand part).On the left in fig. 6 We assume that the primary output (or derivative sign) is received in the secondary controller, and you have received the primary output during the time period which has a particular characteristic pair (INPUT 1, INPUT 2) by point 601. We also assume that the secondary output value that was previously associated with this pair of input values was the one represented with a dashed line to the upper right from point 601. the received primary output (or derivative paragraph) defines the new secondary output value 603 in a way that is analogous to that applied above in figs. 4 and 5: it is assumed that if the secondary output had a value of 603, the corresponding primary output would have had a neutral value. A further Assumption in the left-hand part of FIG. 6 is that concept "subrange of input values" that was used in association with fig. 5 has a corresponding two-dimensional form in a self-organizing map or neural network. In other words, the effect of changing the output value associated with point 601 will "bleed" into its immediate surroundings, and cause similar (yet smaller) changes in the output values associated with adjacent points. The points that will be affected are those that fit in the Elliptical region 604. The right-hand side of fig. 6 shows the self-organizing map or neural network after the whole adaptation round has been made. Dashed lines illustrate the previous output values associated with those points for which the new output value was defined as part of the adaptation of the transfer function (note that the previous value for the actual point 601 is not shown any more because it was already shown in the left-hand part).
The mapping from two inputs to one (secondary) output in fig. 6 can be generalized so that the secondary controller may have any number of mutually depending and/or mutually independent inputs, as long the transfer function is unequivocally defined as a mapping from each possible combination of input values to a corresponding secondary output value.The mapping from two inputs to one (secondary) output in fig. 6 can be generalized so that the secondary controller can have any number of mutually dependent and / or mutually independent inputs, as long the transfer function is unequivocally defined as mapping from each possible combination of input values to the corresponding secondary output value.
Fig. 7 illustrates one possible practical application of a control system described above in an internal combustion engine, such as a large diesel engine of the common rail type. On the lower right in the drawing are a fuel delivery line 701 and one or more injectors 702 for injecting fuel coming from the fuel delivery line 701 into cylinders (not shown) of the internal combustion engine. The dynamic quantity to be measured is the fuel pressure in the fuel delivery line 701. A sensor 103 is configured to measure the fuel pressure and to provide a feedback value to the primary controller 301, which feedback value is an indicator of the measured fuel pressure. The actuator 104 is a flow control apparatus that is configured to regulate the flow of fuel 703 into the fuel delivery line 701.Figure 7 illustrates one possible practical application of a control system described above in an internal combustion engine, such as a large diesel engine of the common rail type. On the lower right in the drawing are a fuel supply line 701 and one or more injectors 702 for injecting fuel coming from the fuel supply line 701 into cylinders (not shown) of the internal combustion engine. The dynamic quantity to be measured is the fuel pressure in the fuel delivery line 701. The sensor 103 is configured to measure the fuel pressure and provide a feedback value to the primary controller 301, which feedback value is an indicator of the measured fuel pressure. . The actuator 104 is a flow control apparatus that is configured to regulate the flow of fuel 703 into the fuel delivery line 701.
The input value to the secondary controller 302 is an indicator of the injection duration of one or more of the injectors 702. A deliberate increase in injection duration aims at increasing the output power of the engine, and requires a corresponding increase in the flow of fuel into the fuel delivery line 701. Thus when the secondary controller 302 receives an input that indicates an increase in injection duration, it produces a secondary output that goes through the combiner 303 to the actuator 104 and increases the fuel flow.The input value to the secondary controller 302 is an indicator of the injection duration of one or more of the injectors 702. The deliberate increase in injection duration aims at increasing the output power of the engine, and requires a corresponding increase in the flow of fuel. into the fuel delivery line 701. Thus, when the secondary controller 302 receives an input that indicates an increase in injection duration, it produces a secondary output that passes through the combiner 303 to the actuator 104 and increases the fuel flow.
Non-measurable disturbances include all such factors that make this increase in fuel flow inaccurate for reasons that would be difficult or impossible to predict. For example if the flow control apparatus is worn, a particular movement of the actuator 104 may increase the fuel flow too much or too little. Feedback control through the loop including the sensor 103 and primary controller 301 corrects the fuel pressure, and the secondary controller 302 receives knowledge about the appeared need for correction in the form of the primary output that the primary controller 301 produced. If the initial increase in fuel flow was too small, the primary controller 301 produced a primary output that moved the actuator 104 a little bit further. The secondary controller 302 notices this, so it becomes aware that next time when a similar increase in injection duration is made, the secondary controller 302 should already in the first place move the actuator 104 a little more than previously.Non-measurable disturbances include all such factors that make this increase in fuel flow inaccurate for reasons that would be difficult or impossible to predict. For example, if the flow control apparatus is worn, a particular movement of the actuator 104 may increase the fuel flow too much or too little. Feedback control through the loop including the sensor 103 and the primary controller 301 corrects the fuel pressure, and the secondary controller 302 receives the knowledge about the need for correction in the form of the primary output that the primary controller 301 produced. If the initial increase in fuel flow was too small, the primary controller 301 produced a primary output that moved the actuator 104 a little bit further. The secondary controller 302 notices this, so it becomes aware that the next time a similar increase in injection duration is made, the secondary controller 302 should already be in the first place to move the actuator 104 a little more than before.
Similar principles can be applied to the controlling of various processes in an internal combustion engine. In order to ensure the applicability of the description given above, it is advantageous that if a more proactive input signal and a more reactive input signal are available, the more proactive one is used as the input to the secondary controller while the more reactive one is used a feedback value fed to the primary controller. For example, if pilot fuel injection is used in a dual-fuel engine (or pilot gas injection in a solely gas-fuelled engine), the pilot fuel pressure (or pilot gas pressure) could be controlled so that information about pilot duration is used as an input to the secondary controller and a measured pressure in the pilot delivery line as a feedback value to the primary controller. Also in a dual-fuelled or gas-fuelled engine the main gas pressure control could come into question, so that the main gas duration is used as an input value to the secondary controller and the main gas pressure as a feedback value to the primary controller.Similar principles can be applied to controlling various processes in an internal combustion engine. In order to ensure the applicability of the description given above, it is advantageous that if a more proactive input signal and a more reactive input signal are available, the more proactive one is used as the input to the secondary controller while the more reactive one is used a feedback value fed to the primary controller. For example, if a pilot fuel injection is used in a dual fuel engine (or pilot gas injection), the pilot fuel pressure (or pilot gas pressure) could be controlled so that information about pilot duration is used as an input to the secondary controller and a measured pressure in the pilot delivery line as a feedback value to the primary controller. Also in a dual-fuelled or gas-fuelled engine the main gas pressure control could come into question, so that the main gas duration is used as an input value to the secondary controller and the main gas pressure as a feedback value to the primary controller .
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KR1020167021041A KR102067868B1 (en) | 2014-01-03 | 2014-12-17 | Control system and control method for an internal combustion engine, and an internal combustion engine |
CN201480072006.8A CN105934575B (en) | 2014-01-03 | 2014-12-17 | Control system and control method and internal combustion engine for internal combustion engine |
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