CN114580106A - Engine torque model and construction method thereof - Google Patents
Engine torque model and construction method thereof Download PDFInfo
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Abstract
本发明提供了一种发动机扭矩模型的构建方法及发动机扭矩模型,涉及模型构建方法技术领域。本发明的发动机扭矩模型的构建方法通过根据预设点火角效率曲线搭建初始点火角效率模型,向初始点火角效率模型输入实际点火角和最优点火角的差值,以输出点火角效率,将多组数组代入初始点火角效率模型,以得到与所多组数组对应的多个点火角效率模型过程可以使得搭建的发动机扭矩模型精度高,从而提高发动机输出扭矩的精度,并且使得扭矩的偏差在一定范围内,提高了发动机的NVH特性。
The invention provides a construction method of an engine torque model and an engine torque model, and relates to the technical field of model construction methods. The construction method of the engine torque model of the present invention builds an initial ignition angle efficiency model according to a preset ignition angle efficiency curve, and inputs the difference between the actual ignition angle and the optimal ignition angle into the initial ignition angle efficiency model, so as to output the ignition angle efficiency. Substitute multiple sets of arrays into the initial ignition angle efficiency model to obtain multiple ignition angle efficiency models corresponding to all the multiple sets of arrays. The process can make the built engine torque model with high accuracy, thereby improving the accuracy of the engine output torque, and making the torque deviation within Within a certain range, the NVH characteristics of the engine are improved.
Description
技术领域technical field
本发明涉及模型构建方法技术领域,特别是涉及一种发动机扭矩模型的构建方法及发动机扭矩模型。The present invention relates to the technical field of model building methods, in particular to a method for building an engine torque model and an engine torque model.
背景技术Background technique
点火角效率又称为点火损失率,即在其他控制参数不变下,点火角输出变化对扭矩变化的关系;点火角效率是发动机扭矩模型标定的核心内容,点火角效率标定的准确直接决定了扭矩控制的精度,扭矩精度对整车换挡品质及整车驾驶性都有直接影响,对发动机排放和油耗表现也有间接影响;Ignition angle efficiency is also called ignition loss rate, that is, the relationship between ignition angle output change and torque change when other control parameters remain unchanged; ignition angle efficiency is the core content of engine torque model calibration, and the accuracy of ignition angle efficiency calibration directly determines The accuracy of torque control has a direct impact on the shifting quality and drivability of the entire vehicle, and also has an indirect impact on engine emissions and fuel consumption performance;
目前现有的点火角效率确认方法是多项式拟合:The current existing method for confirming the ignition angle efficiency is polynomial fitting:
通过对不同工况下如发动机转速和负荷,对不同点火角下扭矩数据采集,通过对采集后数据进行筛选处理,通过多组数据拟合出一条点火角效率曲线。上述介绍的点火角效率确认方法有以下不足:1).扭矩模型精度不足:2).最优点火角(MBT)代表输出最大扭矩对应的点火角,正常不应当出现最优点火角小于基础点火角的情况,使得最优点火角输出不合理。Through the acquisition of torque data at different ignition angles under different operating conditions such as engine speed and load, and by filtering the collected data, an ignition angle efficiency curve is fitted through multiple sets of data. The ignition angle efficiency confirmation method introduced above has the following shortcomings: 1). The torque model is not accurate enough: 2). The optimal ignition angle (MBT) represents the ignition angle corresponding to the output maximum torque. Normally, the optimal ignition angle should not be smaller than the basic ignition angle. angle, making the optimal ignition angle output unreasonable.
发明内容SUMMARY OF THE INVENTION
本发明的第一方面的一个目的是要提供一种发动机扭矩模型的构建方法,解决现有技术中扭矩模型精度不足的问题。An object of the first aspect of the present invention is to provide a method for constructing an engine torque model, which solves the problem of insufficient accuracy of the torque model in the prior art.
本发明的第一方面的另一个目的是解决现有扭矩模型的最优点火角输出不合理的问题。Another object of the first aspect of the present invention is to solve the problem that the optimal ignition angle output of the existing torque model is unreasonable.
本发明的第二方面的一个目的是要提供一种发动机扭矩模型的构建方法。An object of the second aspect of the present invention is to provide a method of constructing an engine torque model.
特别地,本发明还提供一种发动机扭矩模型的构建方法,所述发动机扭矩模型包括用以输出目标点火角效率曲线的点火角效率模型,所述点火角效率模型的构建方法包括如下步骤:In particular, the present invention also provides a method for constructing an engine torque model, wherein the engine torque model includes an ignition angle efficiency model for outputting a target ignition angle efficiency curve, and the method for constructing the ignition angle efficiency model includes the following steps:
根据预设点火角效率曲线搭建初始点火角效率模型,所述初始点火角效率模型为与正弦函数相关的包含多个未知系数的数学函数;Build an initial firing angle efficiency model according to a preset firing angle efficiency curve, where the initial firing angle efficiency model is a mathematical function related to a sine function that includes a plurality of unknown coefficients;
向所述初始点火角效率模型输入实际点火角和最优点火角的差值,以输出点火角效率,并进行多次输入和输出循环,以计算获得包含有所有未知系数的数值的多组数组,所述最优点火角根据转速和负荷计算获得;Input the difference between the actual ignition angle and the optimal ignition angle into the initial ignition angle efficiency model to output the ignition angle efficiency, and perform multiple input and output cycles to calculate and obtain multiple sets of arrays containing the values of all unknown coefficients , the optimal ignition angle is calculated and obtained according to the rotational speed and load;
将所述多组数组代入所述初始点火角效率模型,以得到与所多组数组对应的多个点火角效率模型。Substitute the multiple groups of arrays into the initial ignition angle efficiency model to obtain multiple ignition angle efficiency models corresponding to the multiple groups of arrays.
可选地,根据预设点火角效率曲线搭建初始点火角效率模型的步骤中,所述初始点火角效率模型的数学关系式为:Optionally, in the step of building an initial ignition angle efficiency model according to a preset ignition angle efficiency curve, the mathematical relationship of the initial ignition angle efficiency model is:
y=asin(bx+c)+dsin(ex+f)y=asin(bx+c)+dsin(ex+f)
其中,y为点火角效率,x为最优点火角与实际点火角的差值,a、b、c、d、e、f均为所述未知系数。Among them, y is the ignition angle efficiency, x is the difference between the optimal ignition angle and the actual ignition angle, and a, b, c, d, e, and f are all the unknown coefficients.
可选地,所述初始点火角效率模型的数学关系式为:Optionally, the mathematical relationship of the initial ignition angle efficiency model is:
y=(acos(b)sin(cx+d)-ccos(d)sin(ax+b))/(acos(b)sin(d)-ccos(d)sin(b))。y=(acos(b)sin(cx+d)-ccos(d)sin(ax+b))/(acos(b)sin(d)-ccos(d)sin(b)).
可选地,向所述初始点火角效率模型输入实际点火角和最优点火角的差值的步骤中,所述最优点火角是通过最优点火角模型计算获得的,所述最优点火角模型的构建方法包括如下步骤:Optionally, in the step of inputting the difference between the actual ignition angle and the optimal ignition angle into the initial ignition angle efficiency model, the optimal ignition angle is obtained by calculating the optimal ignition angle model, and the optimal ignition angle is obtained by calculating the optimal ignition angle. The construction method of the corner model includes the following steps:
将基础点火角加上点火角偏移值得到所述最优点火角的关系式构建为初始最优点火角模型,所述基础点火角根据转速和负荷计算获得;The relational expression of the optimal ignition angle obtained by adding the basic ignition angle to the ignition angle offset value is constructed as an initial optimal ignition angle model, and the basic ignition angle is calculated and obtained according to the rotational speed and the load;
向所述初始最优点火角模型输入所述转速和所述负荷;inputting the rotational speed and the load to the initial optimum firing angle model;
将所述初始最优点火角模型中的所述点火角偏移值约束为正值;Constraining the ignition angle offset value in the initial optimal ignition angle model to a positive value;
在所述初始最优点火角模型与所述初始点火角效率模型合并时进行整个所述发动机扭矩模型的输入输出循环,以获得多个不同的转速和负荷下对应的目标最优点火角模型。When the initial optimal ignition angle model and the initial ignition angle efficiency model are combined, an input-output cycle of the entire engine torque model is performed to obtain a plurality of target optimal ignition angle models corresponding to different rotational speeds and loads.
可选地,将所述初始最优点火角模型与所述初始点火角效率模型合并,并进行输入输出循环,还获得多组所述未知系数的值。Optionally, the initial optimal ignition angle model and the initial ignition angle efficiency model are combined, and an input and output cycle is performed, and a plurality of sets of values of the unknown coefficients are also obtained.
可选地,在获得多组所述未知系数的值后还包括:Optionally, after obtaining multiple sets of values of the unknown coefficients, the method further includes:
将任意一组所述未知系数的值带入所述初始点火角效率模型得到与该所述未知系数对应的所述转速和所述负荷对应的目标点火角效率模型。Bringing the value of any set of the unknown coefficients into the initial ignition angle efficiency model to obtain a target ignition angle efficiency model corresponding to the rotational speed and the load corresponding to the unknown coefficients.
可选地,将所述目标最优点火角模型与所述目标点火角效率模型合并,并进行输入输出循环,还获得多组不同的转速和负荷下对应的基础点火角数组、点火角偏移值数组和点火角效率曲线。Optionally, the target optimal ignition angle model and the target ignition angle efficiency model are combined, and an input and output cycle is performed, and multiple sets of basic ignition angle arrays and ignition angle offsets corresponding to different rotational speeds and loads are also obtained. Array of values and firing angle efficiency curve.
特别地,本发明还提供一种发动机扭矩模型,由上面所述的发动机扭矩模型的构建方法得到。In particular, the present invention also provides an engine torque model obtained by the above-mentioned construction method of the engine torque model.
可选地,包括:Optionally, include:
点火角效率模型,由包含多个未知数的初始点火角效率模型经过各种输入输出得到所述多个未知数的值后再带入所述初始点火角效率模型中得到;The ignition angle efficiency model is obtained from an initial ignition angle efficiency model containing multiple unknowns through various inputs and outputs, and then the values of the multiple unknowns are obtained and then brought into the initial ignition angle efficiency model;
最优点火角模型,由初始最优点火角模型和所述初始点火角效率模型经过多次输入和输出后得到最优点火角模型。The optimal ignition angle model is obtained from the initial optimal ignition angle model and the initial ignition angle efficiency model after multiple inputs and outputs.
可选地,所述初始点火角效率模型为与正弦函数相关的包含多个未知系数的数学函数;Optionally, the initial firing angle efficiency model is a mathematical function related to a sine function that includes a plurality of unknown coefficients;
所述数学函数为y=asin(bx+c)+dsin(ex+f),x为最优点火角与实际点火角的差值,y为点火角效率,a、b、c、d、e、f为所述未知参数;The mathematical function is y=asin(bx+c)+dsin(ex+f), x is the difference between the optimal ignition angle and the actual ignition angle, y is the ignition angle efficiency, a, b, c, d, e , f is the unknown parameter;
其中,已知以x=0为输入,以y=1为输出,以及以x=0为输入,以y′=0为输出,求解得到初始点火角效率模型,所述初始点火角效率模型为y=(acos(b)sin(cx+d)-ccos(d)sin(ax+b))/(acos(b)sin(d)-ccos(d)sin(b))。Among them, it is known that x=0 is used as input, y=1 is output, and x=0 is used as input, and y′=0 is used as output, and the initial ignition angle efficiency model is obtained by solving, and the initial ignition angle efficiency model is y=(acos(b)sin(cx+d)-ccos(d)sin(ax+b))/(acos(b)sin(d)-ccos(d)sin(b)).
本申请中,通过根据预设点火角效率曲线搭建初始点火角效率模型,向初始点火角效率模型输入实际点火角和最优点火角的差值,以输出点火角效率,将多组数组代入初始点火角效率模型,以得到与所多组数组对应的多个点火角效率模型过程可以使得搭建的发动机扭矩模型精度高,从而提高发动机输出扭矩的精度,并且使得扭矩的偏差在一定范围内,提高了发动机的NVH特性。In this application, an initial ignition angle efficiency model is built according to a preset ignition angle efficiency curve, and the difference between the actual ignition angle and the optimal ignition angle is input into the initial ignition angle efficiency model to output the ignition angle efficiency, and multiple groups of arrays are substituted into the initial ignition angle efficiency model. The ignition angle efficiency model is used to obtain multiple ignition angle efficiency models corresponding to the multiple groups of arrays. The process can make the built engine torque model with high accuracy, thereby improving the accuracy of the engine output torque, and making the torque deviation within a certain range. the NVH characteristics of the engine.
进一步地,本申请中还通过将基础点火角加上点火角偏移值得到最优点火角的关系式构建为初始最优点火角模型,基础点火角根据转速和负荷计算获得,将初始最优点火角模型中的点火角偏移值约束为正值等过程得到最优点火角模型,可以实时最优点火角大于基础点火角,从而使得最优点火角的输出合理,完善输出的点火效率曲线。Further, in this application, the relational expression of the optimal ignition angle obtained by adding the basic ignition angle to the ignition angle offset value is also constructed as the initial optimal ignition angle model. The optimal ignition angle model can be obtained through the process of constraining the ignition angle offset value in the ignition angle model to a positive value, and the real-time optimal ignition angle can be larger than the basic ignition angle, so that the output of the optimal ignition angle is reasonable and the output ignition efficiency curve is improved. .
根据下文结合附图对本发明具体实施例的详细描述,本领域技术人员将会更加明了本发明的上述以及其他目的、优点和特征。The above and other objects, advantages and features of the present invention will be more apparent to those skilled in the art from the following detailed description of the specific embodiments of the present invention in conjunction with the accompanying drawings.
附图说明Description of drawings
后文将参照附图以示例性而非限制性的方式详细描述本发明的一些具体实施例。附图中相同的附图标记标示了相同或类似的部件或部分。本领域技术人员应该理解,这些附图未必是按比例绘制的。附图中:Hereinafter, some specific embodiments of the present invention will be described in detail by way of example and not limitation with reference to the accompanying drawings. The same reference numbers in the figures designate the same or similar parts or parts. It will be understood by those skilled in the art that the drawings are not necessarily to scale. In the attached picture:
图1是根据本发明的一个具体的实施例的发动机扭矩模型的构建方法的示意性流程图;1 is a schematic flowchart of a method for constructing an engine torque model according to a specific embodiment of the present invention;
图2是根据本发明的另一个具体的实施例的发动机扭矩模型的构建方法的示意性流程图;2 is a schematic flowchart of a method for constructing an engine torque model according to another specific embodiment of the present invention;
图3是根据本发明的另一个具体的实施例的发动机扭矩模型的构建方法的示意性流程图;3 is a schematic flowchart of a method for constructing an engine torque model according to another specific embodiment of the present invention;
图4是根据本发明的一个具体的实施例的发动机扭矩模型的示意性结构框图;4 is a schematic structural block diagram of an engine torque model according to a specific embodiment of the present invention;
图5是根据本发明的一个具体的实施例的发动机扭矩模型输出的点火角效率曲线图;5 is a graph of ignition angle efficiency output by an engine torque model according to a specific embodiment of the present invention;
图6是根据本发明的一个具体的实施例的发动机扭矩模型的偏差示意图。FIG. 6 is a schematic diagram of the deviation of the engine torque model according to a specific embodiment of the present invention.
具体实施方式Detailed ways
图1是根据本发明的一个具体的实施例的发动机扭矩模型的构建方法的示意性流程图。作为本发明一个具体的实施例,本实施例提供一种发动机扭矩模型的构建方法。发动机扭矩模型可以包括用以输出目标点火角效率曲线的点火角效率模型,点火角效率模型的构建方法可以包括如下步骤:FIG. 1 is a schematic flowchart of a method for constructing an engine torque model according to a specific embodiment of the present invention. As a specific embodiment of the present invention, this embodiment provides a method for constructing an engine torque model. The engine torque model may include an ignition angle efficiency model for outputting a target ignition angle efficiency curve, and the construction method of the ignition angle efficiency model may include the following steps:
步骤S100,根据预设点火角效率曲线搭建初始点火角效率模型,初始点火角效率模型为与正弦函数相关的包含多个未知系数的数学函数;Step S100, building an initial firing angle efficiency model according to a preset firing angle efficiency curve, where the initial firing angle efficiency model is a mathematical function related to a sine function and including a plurality of unknown coefficients;
步骤S200,向初始点火角效率模型输入实际点火角和最优点火角的差值,以输出点火角效率,并进行多次输入和输出循环,以计算获得包含有所有未知系数的数值的多组数组,最优点火角根据转速和负荷计算获得;Step S200, input the difference between the actual ignition angle and the optimal ignition angle into the initial ignition angle efficiency model to output the ignition angle efficiency, and perform multiple input and output cycles to calculate and obtain multiple sets of values including all unknown coefficients. Array, the optimal ignition angle is calculated according to the speed and load;
步骤S300,将多组数组代入初始点火角效率模型,以得到与所多组数组对应的多个点火角效率模型。Step S300, substituting multiple groups of arrays into the initial ignition angle efficiency model to obtain multiple ignition angle efficiency models corresponding to all the multiple groups of arrays.
具体地,在搭建初始点火角效率模型前,发明人获得大量的点火角效率的曲线,其曲线形状大体与正弦函数相似。因此,在构建初始点火角效率模型时,将初始点火角效率模型搭建为正弦函数模型。具体可以是初始点火角效率模型y=asin(bx+c)+dsin(ex+f),其中,y为点火角效率,x为最优点火角与实际点火角的差值,a、b、c、d、e、f均为未知系数。Specifically, before building the initial ignition angle efficiency model, the inventors obtained a large number of ignition angle efficiency curves, the shape of which is generally similar to a sine function. Therefore, when constructing the initial ignition angle efficiency model, the initial ignition angle efficiency model is constructed as a sine function model. Specifically, the initial ignition angle efficiency model y=asin(bx+c)+dsin(ex+f), where y is the ignition angle efficiency, x is the difference between the optimal ignition angle and the actual ignition angle, a, b, c, d, e, and f are all unknown coefficients.
由于在发动机实际使用过程中,已知x=0时,y=1,x=0时,y′=0。将其带入到上面的关系式中转化后可以得到初始点火角效率模型为y=(acos(b)sin(cx+d)-ccos(d)sin(ax+b))/(acos(b)sin(d)-ccos(d)sin(b))。In the actual use of the engine, it is known that when x=0, y=1, and when x=0, y'=0. Bringing it into the above relationship and transforming it, the initial ignition angle efficiency model can be obtained as y=(acos(b)sin(cx+d)-ccos(d)sin(ax+b))/(acos(b) )sin(d)-ccos(d)sin(b)).
步骤S200中,向该模型中输入实际点火角和最优点火角的差值,以输出点火角效率,经过多次的输入和输出后可以得到多组点火角效率模型。In step S200, the difference between the actual ignition angle and the optimal ignition angle is input into the model to output the ignition angle efficiency. After many times of input and output, multiple sets of ignition angle efficiency models can be obtained.
通过上述方式搭建的模型,可以得到以精度高的点火角效率模型,从而提高发动机输出扭矩的精度,并且使得扭矩精度的偏差在一定范围内,提高了发动机的扭矩特性。Through the model built in the above manner, a high-precision ignition angle efficiency model can be obtained, thereby improving the accuracy of the output torque of the engine, and making the deviation of the torque accuracy within a certain range, improving the torque characteristics of the engine.
图2是根据本发明的另一个具体的实施例的发动机扭矩模型的构建方法的示意性流程图;作为本发明一个具体的实施例,本实施例向初始点火角效率模型输入实际点火角和最优点火角的差值的步骤中,最优点火角是通过最优点火角模型计算获得的,最优点火角模型的构建方法包括如下步骤:2 is a schematic flowchart of a method for constructing an engine torque model according to another specific embodiment of the present invention; as a specific embodiment of the present invention, the present embodiment inputs the actual ignition angle and the maximum ignition angle into the initial ignition angle efficiency model. In the step of calculating the difference of the advantage fire angle, the optimal ignition angle is obtained by calculating the optimal ignition angle model, and the construction method of the optimal ignition angle model includes the following steps:
步骤S400,将基础点火角加上点火角偏移值得到最优点火角的关系式构建为初始最优点火角模型,基础点火角根据转速和负荷计算获得;Step S400, constructing the relational expression of the optimal ignition angle obtained by adding the basic ignition angle to the ignition angle offset value as an initial optimal ignition angle model, and the basic ignition angle is calculated and obtained according to the rotational speed and the load;
步骤S500,向初始最优点火角模型输入转速和负荷;Step S500, input the rotational speed and load to the initial optimal ignition angle model;
步骤S600,将初始最优点火角模型中的点火角偏移值约束为正值;Step S600, constrain the ignition angle offset value in the initial optimal ignition angle model to be a positive value;
步骤S700,在初始最优点火角模型与初始点火角效率模型合并时进行整个发动机扭矩模型的输入输出循环,以获得多个不同的转速和负荷下对应的目标最优点火角模型。Step S700, when the initial optimal ignition angle model and the initial ignition angle efficiency model are combined, the input and output cycle of the entire engine torque model is performed to obtain multiple target optimal ignition angle models corresponding to different rotational speeds and loads.
本实施例中,初始点火角模组中可以通过输入转速和负荷得到基础点火角,基础点火角与点火角偏移值相加得到最优点火角,而在实际的情况中,最优点火角要大于基础点火角,因此需要约束点火角偏移值为正值。In this embodiment, in the initial ignition angle module, the basic ignition angle can be obtained by inputting the rotational speed and load, and the optimal ignition angle is obtained by adding the basic ignition angle and the ignition angle offset value. To be larger than the base firing angle, it is necessary to constrain the firing angle offset to a positive value.
本实施例中,由于将点火角偏移值约束为正值,则可以实时最优点火角大于基础点火角,从而使得最优点火角的输出合理,完善点火效率曲线输出。In this embodiment, since the ignition angle offset value is constrained to be a positive value, the real-time optimal ignition angle can be larger than the basic ignition angle, thereby making the output of the optimal ignition angle reasonable and improving the output of the ignition efficiency curve.
图3是根据本发明的另一个具体的实施例的发动机扭矩模型的构建方法的示意性流程图。作为本发明一个具体地实施例,本实施例的发动机扭矩模型的构建方法还包括步骤S800,将初始最优点火角模型与初始点火角效率模型合并,并进行输入输出循环,还获得多组未知系数的值。FIG. 3 is a schematic flowchart of a method for constructing an engine torque model according to another specific embodiment of the present invention. As a specific embodiment of the present invention, the method for constructing an engine torque model in this embodiment further includes step S800, merging the initial optimal ignition angle model and the initial ignition angle efficiency model, and performing an input and output cycle, and obtaining multiple sets of unknown the value of the coefficient.
一般而言,在初始最优点火角模型中位置系数的值的数量的多少决定了输出和输出的循环次数至少大要与该数量,才能得到位置系数的值。当输入和输出循环的次数越多时,则得到后续的值越多,越精确。Generally speaking, the number of the value of the position coefficient in the initial optimal ignition angle model determines the output and the number of cycles of the output is at least as large as this number before the value of the position coefficient can be obtained. When the number of input and output loops is more, the more subsequent values are obtained, the more accurate.
在获得多组未知系数的值后还包括:After obtaining the values of multiple sets of unknown coefficients, it also includes:
步骤S900,将任意一组未知系数的值带入初始点火角效率模型得到与该未知系数对应的转速和负荷对应的目标点火角效率模型。Step S900, bringing the value of any group of unknown coefficients into the initial ignition angle efficiency model to obtain a target ignition angle efficiency model corresponding to the rotational speed and load corresponding to the unknown coefficients.
将目标最优点火角模型与目标点火角效率模型合并,并进行输入输出循环,还获得多组不同的转速和负荷下对应的基础点火角数组、点火角偏移值数组和点火角效率曲线。The target optimal ignition angle model and the target ignition angle efficiency model are combined, and the input and output cycle is performed, and multiple sets of basic ignition angle arrays, ignition angle offset value arrays and ignition angle efficiency curves corresponding to different rotational speeds and loads are obtained.
因此若输入一组转速和负荷无法得到输出的数据,需要输出多个转速和负荷,经过模型的处理后可以得到多组转速和负荷对应的基础点火角数组、点火角偏移值数组和点火角效率曲线。Therefore, if a set of speed and load cannot be outputted, it is necessary to output multiple speeds and loads. After processing the model, the basic ignition angle array, ignition angle offset value array and ignition angle corresponding to multiple sets of speeds and loads can be obtained. efficiency curve.
图5是根据本发明的一个具体的实施例的发动机扭矩模型输出的点火角效率曲线图。由图5可以看出,按照本申请的方法得到的发动机扭矩模型最终输出的点火角效率曲线与实际相符。FIG. 5 is a graph of ignition angle efficiency output by an engine torque model according to a specific embodiment of the present invention. It can be seen from FIG. 5 that the ignition angle efficiency curve finally output by the engine torque model obtained by the method of the present application is consistent with the actual situation.
图6是根据本发明的一个具体的实施例的发动机扭矩模型的偏差示意图。本实施例中整个过程都是借助Matlab的MBC工具箱对模型进行优化。如图6所示,本实施例的发动机扭矩模型精度在全工况下都满足200Nm以内±5Nm偏差,200Nm以上±扭矩乘以2.5%偏差范围内,可以变化的点火角范围内也可以保证上面标准;同时最优点火角输出合理,即最优点火角大于等于基础点火角。FIG. 6 is a schematic diagram of the deviation of the engine torque model according to a specific embodiment of the present invention. In this embodiment, the entire process is to optimize the model by means of the MBC toolbox of Matlab. As shown in FIG. 6 , the accuracy of the engine torque model of this embodiment satisfies the deviation of ±5Nm within 200Nm under all operating conditions, and within the range of ±torque multiplied by 2.5% deviation above 200Nm, the above can also be guaranteed within the variable ignition angle range. At the same time, the optimal ignition angle output is reasonable, that is, the optimal ignition angle is greater than or equal to the basic ignition angle.
具体地,作为本发明一个具体的实施例,本实施例还提供一种发动机扭矩模型,该发动机扭矩模型可以由上面的发动机扭矩模型的构建方法得到。Specifically, as a specific embodiment of the present invention, the embodiment further provides an engine torque model, and the engine torque model can be obtained by the above construction method of the engine torque model.
本实施例的发动机扭矩模型可以包括点火角效率模型和最优点火角模型。其中,该点火角效率模型和最优点火角模型首先与目前车辆的整体扭矩模型进行结合,可以在输入发动机转速和负荷后输出扭矩。经过每一次的转速和负荷检测到扭矩的数据,将其输入到上述的模型中,即可按照上面的方式得到发动机扭矩模型。The engine torque model of the present embodiment may include an ignition angle efficiency model and an optimal ignition angle model. Among them, the ignition angle efficiency model and the optimal ignition angle model are first combined with the overall torque model of the current vehicle, and the torque can be output after inputting the engine speed and load. After each rotation speed and load detection torque data, input it into the above model, the engine torque model can be obtained according to the above method.
本实施例中点火角效率模型则由包含多个未知数的初始点火角效率模型经过各种输入输出得到多个未知数的值后再带入初始点火角效率模型中得到。最优点火角模型则由初始最优点火角模型和初始点火角效率模型经过多次输入和输出后得到最优点火角模型。初始点火角效率模型为与正弦函数相关的包含多个未知系数的数学函数。In this embodiment, the ignition angle efficiency model is obtained from an initial ignition angle efficiency model containing multiple unknowns through various inputs and outputs to obtain the values of the multiple unknowns and then brought into the initial ignition angle efficiency model. The optimal ignition angle model is obtained from the initial optimal ignition angle model and the initial ignition angle efficiency model after multiple inputs and outputs. The initial firing angle efficiency model is a mathematical function with a number of unknown coefficients related to a sine function.
数学函数为y=asin(bx+c)+dsin(ex+f),x为最优点火角与实际点火角的差值,y为点火角效率,a、b、c、d、e、f为未知参数;The mathematical function is y=asin(bx+c)+dsin(ex+f), x is the difference between the optimal ignition angle and the actual ignition angle, y is the ignition angle efficiency, a, b, c, d, e, f is an unknown parameter;
其中,已知以x=0为输入,以y=1为输出,以及以x=0为输入,以y′=0为输出,求解得到初始点火角效率模型,初始点火角效率模型为y=(acos(b)sin(cx+d)-ccos(d)sin(ax+b))/(acos(b)sin(d)-ccos(d)sin(b))。Among them, it is known that with x=0 as input, y=1 as output, and with x=0 as input, y′=0 as output, the initial ignition angle efficiency model is obtained by solving, and the initial ignition angle efficiency model is y= (acos(b)sin(cx+d)-ccos(d)sin(ax+b))/(acos(b)sin(d)-ccos(d)sin(b)).
本实施例中按照上述方法得到的发动机扭矩模型的精度在全工况下都满足200Nm以内±5Nm偏差,200Nm以上±扭矩乘以2.5%偏差范围内,可以变化的点火角范围内也可以保证标准,同时,使得最优点火角输出合理,即最优点火角大于等于基础点火角。In this embodiment, the accuracy of the engine torque model obtained by the above method satisfies the deviation of ±5Nm within 200Nm under all operating conditions, and within the range of ±torque multiplied by 2.5% above 200Nm, and the standard can also be guaranteed within the range of the variable ignition angle. , and at the same time, make the optimal ignition angle output reasonable, that is, the optimal ignition angle is greater than or equal to the basic ignition angle.
至此,本领域技术人员应认识到,虽然本文已详尽示出和描述了本发明的多个示例性实施例,但是,在不脱离本发明精神和范围的情况下,仍可根据本发明公开的内容直接确定或推导出符合本发明原理的许多其他变型或修改。因此,本发明的范围应被理解和认定为覆盖了所有这些其他变型或修改。By now, those skilled in the art will recognize that, although various exemplary embodiments of the present invention have been illustrated and described in detail herein, the present invention may still be implemented in accordance with the present disclosure without departing from the spirit and scope of the present invention. The content directly determines or derives many other variations or modifications consistent with the principles of the invention. Accordingly, the scope of the present invention should be understood and deemed to cover all such other variations or modifications.
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