WO2005108948A2 - Manifold air flow (maf) and manifold absolute pressure (map) residual electronic throttle control (etc) security - Google Patents
Manifold air flow (maf) and manifold absolute pressure (map) residual electronic throttle control (etc) security Download PDFInfo
- Publication number
- WO2005108948A2 WO2005108948A2 PCT/US2005/014077 US2005014077W WO2005108948A2 WO 2005108948 A2 WO2005108948 A2 WO 2005108948A2 US 2005014077 W US2005014077 W US 2005014077W WO 2005108948 A2 WO2005108948 A2 WO 2005108948A2
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- maf
- map
- signal
- error
- estimated
- 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.)
- Ceased
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D11/00—Arrangements for, or adaptations to, non-automatic engine control initiation means, e.g. operator initiated
- F02D11/06—Arrangements for, or adaptations to, non-automatic engine control initiation means, e.g. operator initiated characterised by non-mechanical control linkages, e.g. fluid control linkages or by control linkages with power drive or assistance
- F02D11/10—Arrangements for, or adaptations to, non-automatic engine control initiation means, e.g. operator initiated characterised by non-mechanical control linkages, e.g. fluid control linkages or by control linkages with power drive or assistance of the electric type
- F02D11/105—Arrangements for, or adaptations to, non-automatic engine control initiation means, e.g. operator initiated characterised by non-mechanical control linkages, e.g. fluid control linkages or by control linkages with power drive or assistance of the electric type characterised by the function converting demand to actuation, e.g. a map indicating relations between an accelerator pedal position and throttle valve opening or target engine torque
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D11/00—Arrangements for, or adaptations to, non-automatic engine control initiation means, e.g. operator initiated
- F02D11/06—Arrangements for, or adaptations to, non-automatic engine control initiation means, e.g. operator initiated characterised by non-mechanical control linkages, e.g. fluid control linkages or by control linkages with power drive or assistance
- F02D11/10—Arrangements for, or adaptations to, non-automatic engine control initiation means, e.g. operator initiated characterised by non-mechanical control linkages, e.g. fluid control linkages or by control linkages with power drive or assistance of the electric type
- F02D11/107—Safety-related aspects
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01F—MEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUID LEVEL; METERING BY VOLUME
- G01F25/00—Testing or calibration of apparatus for measuring volume, volume flow or liquid level or for metering by volume
- G01F25/10—Testing or calibration of apparatus for measuring volume, volume flow or liquid level or for metering by volume of flowmeters
-
- 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
- F02D2200/04—Engine intake system parameters
- F02D2200/0402—Engine intake system parameters the parameter being determined by using a model of the engine intake or its components
-
- 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
- F02D2200/04—Engine intake system parameters
- F02D2200/0406—Intake manifold pressure
Definitions
- the present invention relates to engine control systems, and more particularly to engine control systems including an electronic throttle control (ETC) security system that is based on manifold air flow (MAF) and manifold absolute pressure (MAP) residuals.
- ETC electronic throttle control
- MAF manifold air flow
- MAP manifold absolute pressure
- Vehicles driven by internal combustion engines generally employ intake system sensors including, but not limited to, a throttle position sensor (TPS), a mass airflow (MAF) sensor and a manifold absolute pressure (MAP) sensor.
- An engine control system implements an electronic throttle control (ETC) system that regulates engine torque output based on a throttle position signal, a MAF signal and a MAP signal.
- the engine control system can also regulate engine torque output using spark advance/retard, cam phasing and/or regulating fuel supply to the cylinders.
- the engine control system executes an ETC diagnostic system that determines whether the TPS, MAF and MAP sensors are functioning properly and are providing accurate readings.
- the ETC diagnostic system uses MAP and MAF residuals or error values to determine proper sensor function.
- the MAP and MAF errors can not be calibrated to meet ETC security requirements without resulting in false failures.
- Additional system redundancy is required to ensure that the failures intended to be detected by the ETC diagnostic do not exceed the ETC security probability of occurrence metrics. The additional redundancy increases vehicle production costs and false failures increase warranty costs.
- the present invention provides an engine fault diagnostic system.
- the engine fault diagnostic system includes a diagnostic module that generates a manifold absolute pressure (MAP) error signal and that generates a mass air flow (MAF) error signal.
- a security module generates an air flow fault when the MAP error signal exceeds a MAP threshold and the MAF error signal exceeds a MAF threshold.
- the engine fault diagnostic system further includes a MAP sensor that generates a MAP signal. The MAP error signal is determined based on an estimated MAP and the MAP signal.
- the engine fault diagnostic system further includes a MAF sensor that generates a MAF signal.
- the MAF error signal is determined based on an estimated MAF and the MAF signal.
- the engine fault diagnostic system further includes a throttle position sensor that generates a throttle position signal. The security module determines the MAP threshold and the MAF threshold based on the throttle position signal.
- the engine fault diagnostic system further includes a throttle module that calculates an estimated MAF based on a MAP signal and a throttle position signal. The MAF error signal is based on the estimated MAF and the MAF signal.
- the engine fault diagnostic system further includes an intake module that calculates an estimated MAP based on a MAF signal and a throttle position signal. The MAP error signal is based on the estimated MAP and the MAP signal.
- Figure 1 is a functional block diagram of an engine fault diagnostic system according to the present invention
- Figure 2 is a functional block diagram showing further details of the engine fault diagnostic system of Figure 1
- Figure 3 is a flowchart illustrating steps performed by the engine fault diagnostic system of the present invention.
- module refers to an application specific integrated circuit (ASIC), an electronic circuit, a processor
- the diagnostic system 10 includes an intake flow rationality (IFR) diagnostic module 12 and data inputs 14.
- the IFR diagnostic module 12 includes a plurality of sub-modules used to perform the ETC security diagnostic steps, as described in further detail below.
- the engine fault diagnostic system 10 further includes an electronic throttle control (ETC) security module 23.
- the data inputs 14 include a throttle position sensor (TPS) 24, a manifold absolute pressure (MAP) sensor 26, a mass airflow (MAF) sensor 28, and other sensors (not shown). Signals generated by each sensor are provided to the IFR diagnostic module 12.
- the ETC security module 23 selectively generates an air flow fault signal based on outputs of the
- the IFR diagnostic module 12 is described in detail in commonly assigned U.S. Pat. No. 6,701 ,282, issued on March 2, 2004, the disclosure of which is expressly incorporated herein by reference.
- the rationality check is an explicit model based diagnostic system that implements three separate models for an engine intake system (not shown). The models account for variable volumetric efficiency engines due to new features such as variable cam phasing and cylinder deactivation.
- the IFR diagnostic module 12 includes a throttle module 30 that implements a throttle model.
- the throttle model describes the flow through a throttle body of the engine intake system and is used to estimate MAF based on ambient air pressure, estimated MAP, throttle position and/or intake air temperature (IAT).
- the throttle model is quasi-steady state and uses a first order lag filter to model dynamic air flow effects through the throttle body.
- the throttle model processes an effective throttle area of the throttle body, which is based on the throttle plate position.
- the IFR diagnostic module 12 also includes a first intake module 32 that implements a first intake model.
- the first intake model describes the intake manifold and is used to estimate MAP based on MAF into the intake manifold (from the throttle body and exhaust gas recirculation (EGR)) and MAF from the intake manifold caused by engine pumping.
- the intake model is quasi-steady state and accounts for manifold dynamics by integrating the effect of small step flow changes with time.
- MAF into the manifold from the throttle is based on an estimate calculated from the throttle model, as discussed in further detail below.
- An engine flow model determines volumetric efficiency and uses the intake manifold model to properly account for the effects of altitude, cam phasing and/or cylinder deactivation.
- the intake model also uses a charge temperature model to account for the effect of EGR flow on the temperature of the gas in the intake manifold.
- the control module 13 further includes a second intake module 34 that implements a second intake model and a residual module 36.
- the second intake model is identical to the first intake model described above except that the MAF sensor is used instead of the throttle model for the throttle air input.
- the residual module 36 generates inputs to the ETC security module 23 based on the sensor signals and outputs of the throttle module 30, the first intake module 32 and the second intake module 36.
- the throttle module 30 generates a mass airflow estimate (MAF E s ⁇ ) based on the input signals and the throttle model.
- the first intake module 32 generates a first manifold absolute pressure estimate (MAP E s ⁇ ) based on the input signals and the first intake model.
- the second intake module 34 generates a second manifold absolute pressure estimate (MAPEST 2 ) based on the input signals and the second intake model.
- the residual module 36 compares MAFEST, MAPESTI and MAP E s ⁇ 2 obtained from the models to the actual values indicated by the MAF and MAP sensors respectively. More specifically, the residual module 36 determines three residuals or errors including a MAF error (MAFERROR), a first MAP error (MAPERROR-I) and a second MAP error (MAPERROR2) based on MAFEST, MAPESTI and MAP E s ⁇ 2, respectively.
- the errors are each determined as the difference between the estimated values and the measured values indicated by the TPS, MAP and MAF sensor signals.
- MAFERROR and MAPERRORI are provided to the ETC security module 23.
- the ETC security module 23 arbitrates MAFERROR and MAPERRORI to determine whether there is an air flow fault. More particularly, the ETC security module 23 compares MAFERROR and MAPERRORI to threshold values, MAFTHRESH and MAP TH RESH, respectively. MAFTHRESH and MAPJHRESH are determined from look-up tables based on the throttle position. If MAFERROR exceeds MAFTHRESH, a MAF residual versus throttle position (MAFRES) fault is indicated.
- MAFRES MAF residual versus throttle position
- step 100 control determines whether enable conditions are met.
- the enable conditions include, but are not limited to, the engine speed being within a specified range (e.g., 1500 - 2300 RPM), the IAT being within a specified range and the absence of sensor faults (e.g., no open or short circuits indicated). If the enable conditions are not met, control ends. If the enable conditions are met, control starts a loop timer in step 102. [0024] In step 104, control determines a desired throttle position (PTHROT) based on the TPS signal. Control calculates MAF E s ⁇ based on the throttle model in step 106, calculates MAPESTI based on the first intake model in step 108 and calculates MAPE S T2 based on the second intake model in step 110.
- PTHROT desired throttle position
- control determines MAPERROR based on MAPESTI and the MAP signal and determines MAFERROR based on MAFEST and the MAF signal.
- the MAFERROR signal is filtered using a first order lag filter.
- control determines whether MAPERROR is below MAPTHRESH based on PTHROT- More specifically, control determines MAPTHRESH from a look-up table based on PTHROT- If MAPERROR is not below MAPTHRESH, control sets a MAPRES fault in step 116. If MAPERROR is below MAPTHRESH, control determines whether MAFERROR is below MAFTHRESH based on PTHROT in step 118.
- step 120 control sets a MAFRES fault in step 120. If MAFERROR is below MAFTHRESH, control continues in step 122. [0026] In step 122, control determines whether the loop timer has expired. If the loop timer has not expired, control loops back. If the loop timer has expired, control continues in step 124. In step 124, control determines whether both the MAPRE S fault and the MAFRES fault are set. If both faults are not set, control clears any faults (i.e., MAPRES or MAFRES faults) in step 126 and control ends. If both faults are set, control indicates an air flow failure in step 128 and control ends.
- step 122 control determines whether the loop timer has expired. If the loop timer has not expired, control loops back. If the loop timer has expired, control continues in step 124. In step 124, control determines whether both the MAPRE S fault and the MAFRES fault are set. If both faults are not set, control clears any faults (i.e
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- General Physics & Mathematics (AREA)
- Combined Controls Of Internal Combustion Engines (AREA)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/831,764 US7069773B2 (en) | 2004-04-23 | 2004-04-23 | Manifold air flow (MAF) and manifold absolute pressure (MAP) residual electronic throttle control (ETC) security |
| US10/831,764 | 2004-04-23 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| WO2005108948A2 true WO2005108948A2 (en) | 2005-11-17 |
| WO2005108948A3 WO2005108948A3 (en) | 2006-07-13 |
Family
ID=35135066
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/US2005/014077 Ceased WO2005108948A2 (en) | 2004-04-23 | 2005-04-22 | Manifold air flow (maf) and manifold absolute pressure (map) residual electronic throttle control (etc) security |
Country Status (2)
| Country | Link |
|---|---|
| US (1) | US7069773B2 (en) |
| WO (1) | WO2005108948A2 (en) |
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| US7380447B2 (en) * | 2006-06-10 | 2008-06-03 | Ford Global Technologies. Llc | Method and system for transient airflow compensation in an internal combustion engine |
| US20080155970A1 (en) * | 2006-12-27 | 2008-07-03 | Detroit Diesel Corporation | Method for verifying the functionality of the components of a diesel particulate filter system |
| JP4407711B2 (en) * | 2007-03-19 | 2010-02-03 | トヨタ自動車株式会社 | Control device for torque demand type internal combustion engine |
| US7771113B2 (en) * | 2007-06-29 | 2010-08-10 | Cummins Filtration Ip, Inc | Sensor rationality diagnostic |
| US8396680B2 (en) * | 2008-10-20 | 2013-03-12 | GM Global Technology Operations LLC | System and method for identifying issues in current and voltage measurements |
| MX2012003114A (en) | 2009-09-15 | 2012-06-19 | Kpit Cummins Infosystems Ltd | Method of converting vehicle into hybrid vehicle. |
| CN102596672B (en) | 2009-09-15 | 2015-03-04 | Kpit技术有限责任公司 | Motor assistance for a hybrid vehicle based on predicted driving range |
| US8423214B2 (en) | 2009-09-15 | 2013-04-16 | Kpit Cummins Infosystems, Ltd. | Motor assistance for a hybrid vehicle |
| JP5926182B2 (en) | 2009-09-15 | 2016-05-25 | ケーピーアイティ テクノロジーズ リミテッド | Hybrid vehicle motor assistance based on user input |
| US8706381B2 (en) * | 2011-05-31 | 2014-04-22 | GM Global Technology Operations LLC | System and method for detection failures of mass airflow sensors in a parallel intake engine |
| US9249747B2 (en) | 2012-09-10 | 2016-02-02 | GM Global Technology Operations LLC | Air mass determination for cylinder activation and deactivation control systems |
| US9222427B2 (en) | 2012-09-10 | 2015-12-29 | GM Global Technology Operations LLC | Intake port pressure prediction for cylinder activation and deactivation control systems |
| US9458778B2 (en) | 2012-08-24 | 2016-10-04 | GM Global Technology Operations LLC | Cylinder activation and deactivation control systems and methods |
| US9458780B2 (en) | 2012-09-10 | 2016-10-04 | GM Global Technology Operations LLC | Systems and methods for controlling cylinder deactivation periods and patterns |
| US9376973B2 (en) | 2012-09-10 | 2016-06-28 | GM Global Technology Operations LLC | Volumetric efficiency determination systems and methods |
| US9458779B2 (en) * | 2013-01-07 | 2016-10-04 | GM Global Technology Operations LLC | Intake runner temperature determination systems and methods |
| US9239024B2 (en) | 2012-09-10 | 2016-01-19 | GM Global Technology Operations LLC | Recursive firing pattern algorithm for variable cylinder deactivation in transient operation |
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| US9534550B2 (en) | 2012-09-10 | 2017-01-03 | GM Global Technology Operations LLC | Air per cylinder determination systems and methods |
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| US10227939B2 (en) | 2012-08-24 | 2019-03-12 | GM Global Technology Operations LLC | Cylinder deactivation pattern matching |
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| US9416743B2 (en) | 2012-10-03 | 2016-08-16 | GM Global Technology Operations LLC | Cylinder activation/deactivation sequence control systems and methods |
| US9650978B2 (en) | 2013-01-07 | 2017-05-16 | GM Global Technology Operations LLC | System and method for randomly adjusting a firing frequency of an engine to reduce vibration when cylinders of the engine are deactivated |
| US9638121B2 (en) | 2012-08-24 | 2017-05-02 | GM Global Technology Operations LLC | System and method for deactivating a cylinder of an engine and reactivating the cylinder based on an estimated trapped air mass |
| US9249749B2 (en) | 2012-10-15 | 2016-02-02 | GM Global Technology Operations LLC | System and method for controlling a firing pattern of an engine to reduce vibration when cylinders of the engine are deactivated |
| US9382853B2 (en) | 2013-01-22 | 2016-07-05 | GM Global Technology Operations LLC | Cylinder control systems and methods for discouraging resonant frequency operation |
| US9494092B2 (en) | 2013-03-13 | 2016-11-15 | GM Global Technology Operations LLC | System and method for predicting parameters associated with airflow through an engine |
| US9810171B2 (en) * | 2013-12-03 | 2017-11-07 | Ford Global Technologies, Llc | Method for determining an offset of a manifold pressure sensor |
| US9441550B2 (en) | 2014-06-10 | 2016-09-13 | GM Global Technology Operations LLC | Cylinder firing fraction determination and control systems and methods |
| US9341128B2 (en) | 2014-06-12 | 2016-05-17 | GM Global Technology Operations LLC | Fuel consumption based cylinder activation and deactivation control systems and methods |
| US9556811B2 (en) | 2014-06-20 | 2017-01-31 | GM Global Technology Operations LLC | Firing pattern management for improved transient vibration in variable cylinder deactivation mode |
| US9599047B2 (en) | 2014-11-20 | 2017-03-21 | GM Global Technology Operations LLC | Combination cylinder state and transmission gear control systems and methods |
| US9982617B2 (en) | 2014-12-04 | 2018-05-29 | Achates Power, Inc. | On-board diagnostics for an opposed-piston engine equipped with a supercharger |
| US10337441B2 (en) | 2015-06-09 | 2019-07-02 | GM Global Technology Operations LLC | Air per cylinder determination systems and methods |
| US10054070B2 (en) | 2016-09-08 | 2018-08-21 | Ford Global Technologies, Llc | Methods and system for diagnosing sensors by utilizing an evaporative emissions system |
| US10253734B2 (en) | 2017-01-18 | 2019-04-09 | Ford Global Technologies, Llc | Method for monitoring component life |
| US10598104B2 (en) | 2017-02-03 | 2020-03-24 | Achates Power, Inc. | Mass airflow sensor monitoring using supercharger airflow characteristics in an opposed-piston engine |
| CN112145325B (en) * | 2019-06-28 | 2022-04-05 | 联合汽车电子有限公司 | Engine air intake system pipeline diagnosis method |
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| US5293553A (en) * | 1991-02-12 | 1994-03-08 | General Motors Corporation | Software air-flow meter for an internal combustion engine |
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-
2004
- 2004-04-23 US US10/831,764 patent/US7069773B2/en not_active Expired - Lifetime
-
2005
- 2005-04-22 WO PCT/US2005/014077 patent/WO2005108948A2/en not_active Ceased
Also Published As
| Publication number | Publication date |
|---|---|
| US7069773B2 (en) | 2006-07-04 |
| US20050235743A1 (en) | 2005-10-27 |
| WO2005108948A3 (en) | 2006-07-13 |
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