Parameter identification method for engine mixed gas control system
A technology of parameter identification and control system, applied in the direction of engine control, electrical control, engine components, etc., can solve the problems of inconsistent parameters of the mixture control system, aging of parts, and poor closed-loop control effect.
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Embodiment 1
[0058] like figure 2 As shown, this embodiment provides a method for identifying parameters of an engine mixture control system, including the following steps:
[0059] S11, the open-loop response of the engine mixture system composed of the engine and the oxygen sensor to the fuel injection command is equivalent to a hysteresis link and a first-order inertia link;
[0060] S12, by changing the fuel injection quantity of the engine injector, inputting the original sine wave mixture gas signal to the engine mixture system to obtain the sine wave exhaust gas air-fuel ratio signal;
[0061] S13. Comparing the amplitude and phase of the sine wave exhaust gas air-fuel ratio signal and the original sine wave mixture gas signal to obtain the lag time T of the lag link and the filter coefficient τ of the first-order inertia link.
[0062] In practical application, such as image 3 As exemplified in , the above-mentioned steps S11-S14 can be executed by a controller, but the present...
Embodiment 2
[0079] like Figure 4 As shown, this embodiment provides a method for identifying parameters of an engine mixture control system, including the following steps:
[0080] S21, the open-loop response of the engine mixture system composed of the engine and the oxygen sensor to the fuel injection command is equivalent to a hysteresis link and a first-order inertia link;
[0081] S22, generating a square wave signal, and then passing the square wave signal through a bandpass filter to obtain the original sine wave mixture signal and inputting it to the engine mixture system to obtain a sine wave exhaust gas air-fuel ratio signal;
[0082] S23. Comparing the amplitude and phase of the sine wave exhaust gas air-fuel ratio signal and the original sine wave mixture gas signal to obtain the lag time T of the lag link and the filter coefficient τ of the first-order inertia link.
[0083] In practical application, such as Figure 5 As exemplified in , the above-mentioned steps S21-S23 c...
Embodiment 3
[0087] like Figure 6 As shown, this embodiment provides a method for identifying parameters of an engine mixture control system, including the following steps:
[0088] S31, the open-loop response of the engine mixture system composed of the engine and the oxygen sensor to the fuel injection command is equivalent to a hysteresis link and a first-order inertia link;
[0089] S32, inputting an original square-wave mixture signal to the engine mixture system to obtain a square-wave exhaust gas air-fuel ratio signal;
[0090] S33, passing the original square-wave mixture signal through a band-pass filter to obtain an original sine-wave mixture signal, and passing the square-wave exhaust air-fuel ratio signal through a band-pass filter to obtain a sine-wave exhaust air-fuel ratio signal; and,
[0091] S34. Comparing the amplitude and phase of the sine wave exhaust gas air-fuel ratio signal and the original sine wave mixture gas signal to obtain the lag time T of the lag link and ...
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