Method for operating a system in which a manipulated variable of an actuator element can be controlled
10851716 ยท 2020-12-01
Assignee
Inventors
Cpc classification
F02B37/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B39/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D11/107
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D41/0007
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02T10/40
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F02M26/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/24
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F02D11/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B39/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A method (10) is described for operating a system (12), for example a hydraulic or pneumatic system (12), in which a manipulated variable of an actuator element (16) can be controlled, and in which at least one variable (26) which is dependent on the manipulated variable of the actuator element (16) can be determined, wherein the manipulated variable of the actuator element (16) is modulated with a first periodic signal (22), and wherein a measurement signal (30) which characterizes the at least one variable (26) is evaluated using at least one second periodic signal (47).
Claims
1. A method (10) for operating an electronic control device (32) of a system (12) of an internal combustion engine in which a through-flow cross section of a valve is modified by an actuator element (16), and in which at least one variable (26) which is dependent on the through-flow cross section of the actuator element (16) is sensed via a sensor, the method comprising: modulating, with a first periodic signal (22), the through-flow cross section of the valve; generating, based on a measurement of the sensor, a measurement signal (30) which characterizes the at least one variable (26); generating a second periodic signal (47) derived from the measurement signal (30) by means of a phase locked loop (49), the second periodic signal (47) having been modified to have a phase difference of zero from the measurement signal (30); providing the measurement signal (30) and the second periodic signal (47) to a multiplier which multiplies the measurement signal (30) and the at least one second periodic signal (47) and outputs a product (50) of the measurement signal (30) and the at least one second periodic signal (47); and detecting, via the evaluation unit, that there is a fault within the actuator element (16) based on an evaluation of the product (50).
2. The method (10) according to claim 1, characterized in that the system (12) is a hydraulic system (12).
3. The method (10) according to claim 1, characterized in that the system (12) is a pneumatic system (12).
4. The method (10) according to claim 1, characterized in that the system (12) is an air system and/or an exhaust system of an internal combustion engine (15) of a motor vehicle.
5. The method (10) according to claim 1, characterized in that the valve is an exhaust gas recirculation valve.
6. The method (10) according to claim 1, characterized in that the actuator element (16) is a charge pressure actuator of a turbocharger.
7. The method (10) according to claim 6, characterized in that the charge pressure actuator of the turbocharger is a VTG actuator or a waste gate actuator.
8. The method (10) according to claim 1, characterized in that the valve is a throttle valve for controlling an air mass flow.
9. The method (10) according to claim 1, characterized in that the first periodic signal (22) is a square-wave signal or a sinusoidal signal.
10. The method (10) according to claim 1, characterized in that a phase locked loop (49) receives the first periodic signal (22) and the measurement signal (30) and generates a reference signal (36) which is used to generate the second periodic signal (47).
11. The method (10) according to claim 1, characterized in that the product (50) is filtered and compared with a threshold value (46).
12. The method (10) according to claim 1, characterized in that the second periodic signal (47) is derived from the first periodic signal (22), wherein the second periodic signal (47) has a first phase in relation to the first periodic signal (22), and in that a third periodic signal (57) is derived from the first or second periodic signal (22; 47), wherein the third periodic signal (57) has a second phase in relation to the second periodic signal (47).
13. The method (10) according to claim 1, characterized in that the second periodic signal (47) is derived from the measurement signal (30) by a phase locked loop (49), wherein the second periodic signal (47) has a first phase in relation to the measurement signal (30), and in that a third periodic signal (57) is derived from the second periodic signal (47) or the measurement signal (30), wherein the third periodic signal (57) has a second phase in relation to the second periodic signal (47).
14. The method (10) according to claim 12, characterized in that the second phase is approximately 90.
15. The method (10) according to claim 12, characterized in that the third periodic signal (57) is multiplied by the measurement signal (30), producing a second product (58), and wherein the product (50) and the second product (58) are each squared and added together creating a sum, and in that the sum is compared with a threshold value (46).
16. The method (10) according to claim 4, characterized in that a frequency of the first periodic signal (22) is selected as a function of a rotational speed of the internal combustion engine (15) of the motor vehicle.
17. The method (10) according to claim 16, characterized in that the frequency and the rotational speed have a nonintegral relationship with one another.
18. The method (10) according to claim 1, characterized in that said method is carried out at least partially by means of a computer program.
19. A control device for an internal combustion engine (15) of a motor vehicle having an internal combustion engine in which a through-flow cross section of a valve is modified by an actuator element (16), and in which at least one variable (26) which is dependent on the through-flow cross section of the actuator element (16) is sensed via a sensor, the control device configured to: modulate, with a first periodic signal (22), the through-flow cross section of the valve; generate, based on a measurement of the sensor, a measurement signal (30) which characterizes the at least one variable (26); generate a second periodic signal (47) derived from the measurement signal (30) by means of a phase locked loop (49), the second periodic signal (47) having been modified to have a phase difference of zero from the measurement signal (30); provide the measurement signal (30) and the second periodic signal (47) to a multiplier which multiplies the measurement signal (30) and the at least one second periodic signal (47) and outputs a product (50) of the measurement signal (30) and the at least one second periodic signal (47); and detect, via the evaluation unit, that there is a fault within the actuator element (16) based on an evaluation of the product (50).
20. The control device according to claim 19, wherein the control device is an open-loop control device.
21. The control device according to claim 19, wherein the control device is a closed-loop control device.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) In addition, important features for the invention can be found in the following drawings, wherein the features may be important for the invention either in isolation or in different combinations, without reference being made once more explicitly to this.
(2) Advantageous embodiments of the invention are explained below with reference to the drawing, in which:
(3)
(4)
(5)
(6)
(7)
DETAILED DESCRIPTION
(8) The same reference symbols are used for functionally equivalent elements and variables in all the figures, even for different embodiments.
(9)
(10) A generator 20 generates a first periodic signal 22 by means of which the through-flow cross section of the actuator element 16 can be controlled by means of an actuator (not illustrated). As a result, modulation of the through-flow cross section or of the quantity of exhaust gas flowing through the actuator element 16 is achieved here. At the top right of the drawing, a sensor 24 is arranged in the exhaust train of the motor vehicle in the pneumatic system 12. The sensor 24 comprises, for example, an exhaust gas probe (not illustrated). A variable 26 which is determined in the sensor 24 is dependent on the through-flow cross section of the actuator element 16. A block 28 generates a measurement signal 30 from a signal which characterizes the variable 26.
(11) An evaluation device for evaluating the measurement signal 30 is arranged in the lower region of the drawing in
(12) As an alternative to the senor 24 arranged in the exhaust train, the variable 26 can also be determined by means of another sensor of the system 12 if the variable 26 is dependent on the manipulated variable of the actuator element 16. For example, the variable 26 can be a charge pressure or an air mass flow in the fresh air feedline 17, and the sensor 24 can be, for example, a hot film air mass meter. However, this is not illustrated in
(13) The method 10 according to the invention is carried out by modulating the through-flow cross section of the actuator element 16 at least temporarily by the first periodic signal 22. Here, an amplitude of this modulation is set in such a way that satisfactory operation of the pneumatic system 12 or of the motor vehicle is not adversely affected. In particular, the amplitude can be set in such a way that the influence thereof on the air system and/or the exhaust system is approximately linear. The effect of the modulation according to the invention is therefore averaged out and therefore remains essentially neutral in relation to the production of soot or nitrogen oxides (NOx).
(14) The variable 26 which is determined by the sensor 24 has periodic fluctuations during satisfactory behavior of the actuator element 16, which fluctuations are dependent on the modulation carried out by means of the first periodic signal 22. The measurement signal 30 has fluctuations which correspond thereto. For example, the generator 20 is a sinusoidal generator and correspondingly the measurement signal 30 has an at least approximately sinusoidal profile. The closed-loop control device 32 continuously compares the phase of the measurement signal 30 with the phase of the reference signal 36 and adjusts the frequency of the generator 34 in accordance with the frequency and phase of the measurement signal 30. This is also known as what is referred to as a phase locked loop 49 (PLL). The phase control takes place in such a way that the phases of the input signals which are applied to the closed-loop control device 32 have a phase offset of 90 with respect to one another. Correspondingly, the phase of the reference signal 36 in the phase rotational element 38 is shifted by a value of 90, with the result that the two input signals of the multiplier 40 essentially have a phase difference of 0 with respect to one another.
(15) The multiplier 40 generates a product 50 which corresponds essentially to the square of a sinusoidal function. The product 50 is subsequently filtered in the filter 42 in such a way that essentially low-pass filtering is performed. As a result, possible interference signals which have frequencies outside the spectrum generated by the generator 20 are effectively suppressed. For example, the output signal of the filter 42 corresponds to a comparatively slow variable direct voltage signal. This signal is subsequently compared with the threshold value 46 in the comparator 44. The output signal 48 therefore contains the information indicating whether the threshold value 46 is exceeded or undershot at a particular time. This information can be used subsequently to evaluate the state or the functional capability of the actuator element 16.
(16) It is particularly advantageous if a frequency of the first periodic signal 22 is selected as a function of a rotational speed of the internal combustion engine 15 of the motor vehicle, in particular if the frequency and the rotational speed have a nonintegral relationship with respect to one another. As a result, interference components of the measurement signal 30 which happen to have the frequency of the second periodic signal 47 can be kept out of the frequency range which is essential for the method 10.
(17) Of course, the pneumatic system 12 (shown in
(18)
(19) In
(20)
(21) During operation, the respective second input signals of the multiplier 40 and of the multiplier 56 have a phase offset of 90 with respect to one another. As a result, the following mathematical approach can be established:
Y.sub.LockInOut1A.Math.cos()
Y.sub.LockInOut2A.Math.cos(90) or Y.sub.LockInOut2A.Math.sin()
S=(Y.sub.LockInOut1.sup.2+Y.sub.LockInOut2.sup.2)
sin.sup.2(x)+cos.sup.2(x)=1; where
(22) Y.sub.LockInOut1=product 50 of the second periodic signal 47 with the measurement signal 30,
(23) Y.sub.LockInOut2=product 58 of the third periodic signal 57 with the measurement signal 30,
(24) A=amplitude of the measurement signal 30 corresponding to the modulation carried out by the first periodic signal 22,
(25) =phase difference between the second periodic signal 47 and the measurement signal 30; and
(26) S=root of the sum of the squares of Y.sub.LockInOut1 and Y.sub.LockInOut2.
(27) It is apparent that the variable S or the sum signal 66 depends essentially on the amplitude A of the measurement signal 30 and not on the phase difference . As a result it is irrelevant whether the second and the third periodic signals 47 and 57 have a specific phase relationship with the measurement signal 30 or not.
(28) Just as in
(29) Alternatively, the second and third periodic signals 47 and 57 can also be derived from the measurement signal 30 by using a phase locked loop 49, similarly to as was described in
(30)
(31) In the block 74 of the left-hand branch, the through-flow cross section of the actuator element 16 is modulated with the first periodic signal 22. In a following block 76, at least one variable of the pneumatic system 12, for example an air mass flow or a charge pressure, is determined. This is done, for example, by using a sensor 24 which is, for example, a charge pressure sensor or an air mass meter. A signal 78 of the block 76, which characterizes the variable 26, is subjected to signal pre-processing in the following block 28, on the basis of which the measurement signal 30 is formed. The signal pre-processing comprises, for example, the formation of a sliding average value and subsequent subtraction of this average value from the signal 78.
(32) In a first block 80 of the right-hand branch in the drawing in
(33) The output signal of the block 83 is used in the block 84 to generate the second periodic signal 47. The left-hand branch and the right-hand branch in the drawing in
(34)
(35) Blocks 70, 72, 74 and 76 and 28 of
(36) The second periodic signal 47 is formed on the basis of the output signal of the block 72, that is to say the first periodic signal 22, in a block 90. The second periodic signal 47 corresponds essentially to the first periodic signal 22; however, if appropriate, it has a different phase. The second periodic signal 47 is rotated through 90 in its phase in the following block 92, which corresponds essentially to the phase rotation element 38. This results in the third periodic signal 57.
(37) A subsequent first multiplier 40 (first lock-in amplifier) is actuated at its first input by the measurement signal 30 and at its second input by the second periodic signal 47. A second multiplier 56 (second lock-in amplifier) is actuated at its first input by the measurement signal 30 and at its second input by the third periodic signal 57. In a subsequent block 94, the geometric sum is calculated from the two output signals of the multipliers 40 and 56, similarly to as is illustrated in
(38) The method 10 according to the flow diagram in