CN112327627B - Nonlinear switching system self-adaptive sliding mode control method based on composite learning - Google Patents
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Abstract
本发明涉及一种基于复合学习的非线性切换系统自适应滑模控制方法,用于解决现有非线性切换系统控制方法实用性差的技术问题。考虑非线性切换系统存在外界干扰和输入非线性,得到切换系统输入死区模型;使用神经网络和切换扰动观测器分别对系统未知非线性函数和复合干扰进行估计,基于平行估计模型构造表征学习性能好坏的预测误差,通过预测误差对神经网络权重更新律和扰动观测器进行调节;基于动态逆技术框架和复合学习策略设计自适应滑模切换控制器;利用预测误差构建滑模时变增益函数,减小了滑模切换抖振的幅度,提升了滑模控制的性能;本发明结合非线性切换系统控制特点,通过设计基于复合学习的自适应滑模控制器有效提升了控制性能。
The invention relates to an adaptive sliding mode control method for a nonlinear switching system based on compound learning, which is used to solve the technical problem of poor practicability of the existing nonlinear switching system control method. Considering the existence of external disturbance and input nonlinearity in the nonlinear switched system, the input dead zone model of the switched system is obtained; the neural network and the switched disturbance observer are used to estimate the unknown nonlinear function and compound disturbance of the system respectively, and the representation learning performance is constructed based on the parallel estimation model. The prediction error is good or bad, and the weight update law of the neural network and the disturbance observer are adjusted by the prediction error; the adaptive sliding mode switching controller is designed based on the dynamic inverse technology framework and compound learning strategy; the sliding mode time-varying gain function is constructed by using the prediction error , reducing the amplitude of the sliding mode switching chattering and improving the performance of the sliding mode control; the invention combines the control characteristics of the nonlinear switching system, and effectively improves the control performance by designing an adaptive sliding mode controller based on compound learning.
Description
技术领域technical field
本发明涉及一种非线性切换系统控制方法,特别是涉及一种基于复合学习的非线性切换系统自适应滑模控制方法,属于飞行控制领域。The invention relates to a control method of a nonlinear switching system, in particular to an adaptive sliding mode control method of a nonlinear switching system based on compound learning, which belongs to the field of flight control.
背景技术Background technique
在实际工程中,许多控制对象如变体飞行器、变频电机以及机器人等都可以用非线性切换系统来描述,因此非线性切换系统控制技术引起了广泛关注,在汽车、电力、化工等许多行业都得到了研究与应用。In practical engineering, many control objects such as variant aircraft, variable frequency motors, and robots can be described by nonlinear switching systems. Therefore, the control technology of nonlinear switching systems has attracted extensive attention. researched and applied.
非线性切换系统自身具有较强的不确定性,同时易受到外部干扰和输入死区的影响,现有的控制方法多采用神经网络或模糊逻辑等智能系统逼近不确定性,采用扰动观测器估计外部干扰。这些控制方法只考虑了智能系统的逼近作用,忽视了智能学习策略的本质,没有对不确定性学习性能进行有效评价,且智能逼近系统和扰动观测器之间没有信息交互,鲁棒性性较差,不利于工程实现。因此研究面向学习性能提升的先进控制方法对于非线性切换系统控制研究意义重大且有着迫切需求。The nonlinear switching system itself has strong uncertainty, and is easily affected by external disturbance and input dead zone. The existing control methods mostly use intelligent systems such as neural network or fuzzy logic to approximate the uncertainty, and use disturbance observer to estimate the uncertainty. external interference. These control methods only consider the approximation effect of the intelligent system, ignore the essence of the intelligent learning strategy, do not effectively evaluate the uncertainty learning performance, and there is no information interaction between the intelligent approximation system and the disturbance observer, and the robustness is relatively low. Poor, not conducive to the realization of the project. Therefore, the study of advanced control methods for learning performance improvement is of great significance and urgent need for nonlinear switching system control research.
发明内容SUMMARY OF THE INVENTION
要解决的技术问题technical problem to be solved
为了克服现有非线性切换系统控制方法实用性差的不足,本发明提供一种基于复合学习的非线性切换系统自适应滑模控制方法。该方法考虑非线性切换系统存在不确定性、外界干扰和输入非线性,通过模型转换获取输入死区模型。同时采用神经网络和扰动观测器分别对非线性函数和复合干扰进行估计,通过构造预测误差对学习效果进行评价,进而调节神经网络权重自适应更新律和切换扰动观测器。基于动态逆技术框架和复合学习策略设计了自适应滑模切换控制器,时变的滑模增益函数提升了控制器鲁棒性,便于工程实现。In order to overcome the shortcomings of poor practicability of the existing nonlinear switching system control methods, the present invention provides an adaptive sliding mode control method for nonlinear switching systems based on compound learning. The method considers the existence of uncertainty, external disturbance and input nonlinearity in the nonlinear switching system, and obtains the input dead zone model through model conversion. At the same time, the neural network and the disturbance observer are used to estimate the nonlinear function and the compound disturbance respectively, and the learning effect is evaluated by constructing the prediction error, and then the adaptive update law of the neural network weight and the switching disturbance observer are adjusted. An adaptive sliding mode switching controller is designed based on the dynamic inverse technology framework and compound learning strategy. The time-varying sliding mode gain function improves the robustness of the controller and facilitates engineering implementation.
技术方案Technical solutions
一种基于复合学习的非线性切换系统自适应滑模控制方法,其特征在于以下步骤:A composite learning-based adaptive sliding mode control method for nonlinear switching systems, characterized by the following steps:
步骤1:考虑一类单输入单输出非线性能控标准型切换系统Step 1: Consider a class of single-input single-output nonlinear controllable standard switching systems
其中,是系统状态向量;uσ(t)∈R是系统输入,y∈R是系统输出;函数σ(t):[0,∞)→M={1,2,…,m}是切换信号,且σ(t)=k时表示第k个子系统是激活的;是关于的未知平滑函数,是关于的未知非零平滑函数;dσ(t)(t)是外部未知干扰;in, is the system state vector; u σ(t) ∈ R is the system input, y∈R is the system output; the function σ(t):[0,∞)→M={1,2,…,m} is the switching signal, And when σ(t)=k, it means that the kth subsystem is activated; its about The unknown smoothing function of , its about The unknown non-zero smooth function of ; d σ(t) (t) is the external unknown disturbance;
步骤2:将系统输入非线性描述为Step 2: Describe the system input nonlinearity as
其中,uv,k∈R是带死区的输入,br,k和bl,k是未知的正常数;where u v,k ∈ R is the input with dead zone, b r,k and b l,k are unknown positive constants;
可将(2)进一步描述为(2) can be further described as
其中in
信号uk存在如下关系The signal u k has the following relationship
其中是uv,k的上界值;in is the upper bound value of u v,k ;
则系统(1)可进一步写为Then system (1) can be further written as
其中, in,
步骤3:针对未知函数和用神经网络来逼近Step 3: For unknown functions and Approximate with a neural network
其中,和是神经网络最优权重向量,和是神经网络基函数向量,εf,k和εG,k是神经网络残差且存在和和是正常数;in, and is the optimal weight vector of the neural network, and is the neural network basis function vector, ε f,k and ε G,k are the neural network residuals and exist and and is a normal number;
则和的估计值可写为but and The estimated value of can be written as
其中,和是神经网络最优权重向量估计值;in, and is the estimated value of the optimal weight vector of the neural network;
定义Δuk=uv,k-uc,k,则xn的导数可写为Define Δu k =u v,k -u c,k , then the derivative of x n can be written as
其中, in,
步骤4:针对非线性切换系统(1),基于复合学习策略设计自适应滑模控制器;Step 4: Design an adaptive sliding mode controller based on a composite learning strategy for the nonlinear switching system (1);
定义输出跟踪误差其中e=x1-yd,yd是控制参考指令;Define Output Tracking Error Where e=x 1 -y d , y d is the control reference command;
设计滑模面为The sliding surface is designed as
s=[ΛT 1]E (11)s=[Λ T 1]E (11)
其中,Λ=[τn-1,(n-1)τn-2,…,(n-1)τ]T,τ>0;Among them, Λ=[τ n-1 ,(n-1)τ n-2 ,...,(n-1)τ] T , τ>0;
滑模面s的导数为The derivative of the sliding surface s is
其中, in,
设计控制器为Design the controller as
其中in
其中,是Dk(t)的估计值,βk是正的设计参数,mk是滑模增益函数;in, is the estimated value of D k (t), β k is a positive design parameter, and m k is the sliding mode gain function;
构造预测误差znNN为The prediction error z nNN is constructed as
其中,可由如下的平行估计模型得到in, It can be obtained by the following parallel estimation model
其中,λn,k是正的设计参数;in, λ n,k is a positive design parameter;
设计滑模增益函数为The sliding mode gain function is designed as
mk=-γz,kλkznNN (19)m k = -γ z,k λ k z nNN (19)
其中,γz,k是正的设计参数;where γz,k is a positive design parameter;
设计神经网络权重更新律为The weight update law of the designed neural network is
其中,γf,k,γG,k,δf,k和δG,k是正的设计参数;where γ f,k , γ G,k , δ f,k and δ G,k are positive design parameters;
设计切换扰动观测器为The switching disturbance observer is designed as
其中,ξn是中间变量,Lk是正的设计参数;where ξ n is an intermediate variable and L k is a positive design parameter;
步骤4:根据步骤3中(13)得到的控制量uc,k,返回到系统模型(1),对系统输出y进行跟踪控制。Step 4: According to the control variable uc ,k obtained in (13) in step 3, return to the system model (1), and perform tracking control on the system output y.
有益效果beneficial effect
本发明提出的一种基于复合学习的非线性切换系统自适应滑模控制方法。该方法考虑非线性切换系统存在不确定性、外界干扰和输入非线性,通过模型转换获取输入死区模型。同时采用神经网络和扰动观测器分别对非线性函数和复合干扰进行估计,通过构造预测误差对学习效果进行评价,进而调节神经网络权重自适应更新律和切换扰动观测器。基于动态逆技术框架和复合学习策略设计了自适应滑模切换控制器,时变的滑模增益函数提升了控制器鲁棒性,便于工程实现。有益效果如下:The invention proposes an adaptive sliding mode control method for nonlinear switching systems based on compound learning. The method considers the existence of uncertainty, external disturbance and input nonlinearity in the nonlinear switching system, and obtains the input dead zone model through model conversion. At the same time, the neural network and the disturbance observer are used to estimate the nonlinear function and the compound disturbance respectively, and the learning effect is evaluated by constructing the prediction error, and then the adaptive update law of the neural network weight and the switching disturbance observer are adjusted. An adaptive sliding mode switching controller is designed based on the dynamic inverse technology framework and compound learning strategy. The time-varying sliding mode gain function improves the robustness of the controller and facilitates engineering implementation. The beneficial effects are as follows:
(1)基于平行估计模型构造了预测误差,基于该误差设计神经网络权重更新律,提高不确定性学习精度,便于工程应用;(1) The prediction error is constructed based on the parallel estimation model, and the weight update law of the neural network is designed based on the error to improve the uncertainty learning accuracy and facilitate engineering applications;
(2)设计非线性切换扰动观测器,对外界时变干扰和输入未知死区带来的不利影响进行了有效的估计补偿;(2) The nonlinear switching disturbance observer is designed to effectively estimate and compensate the adverse effects of external time-varying disturbances and input unknown dead zone;
(3)基于预测误差,采用一种改进的时变增益滑模进行控制器设计,减小了控制切换时的抖振;(3) Based on the prediction error, an improved time-varying gain sliding mode is used to design the controller, which reduces the chattering during control switching;
(4)将滑模面信号引入到神经网络和扰动观测器设计中,通过两者的交互协同实现对未知非线性函数和外界时变干扰的有效估计。(4) The sliding mode surface signal is introduced into the design of the neural network and the disturbance observer, and the effective estimation of the unknown nonlinear function and the external time-varying disturbance is realized through the interaction and synergy of the two.
附图说明Description of drawings
图1为本发明实施流程图。FIG. 1 is a flow chart of the implementation of the present invention.
具体实施方式Detailed ways
现结合实施例、附图对本发明作进一步描述:The present invention will now be further described in conjunction with the embodiments and accompanying drawings:
参照图1,本发明基于复合学习的非线性切换系统自适应滑模控制方法具体步骤如下:1, the specific steps of the adaptive sliding mode control method of the nonlinear switching system based on compound learning of the present invention are as follows:
步骤1:考虑变体飞行器机翼摇滚模型Step 1: Consider the variant aircraft wing rock model
其中,φ、和分别是滚转角、滚转角速率和滚转角加速度,u是控制输入;Among them, φ, and are the roll angle, roll angular rate and roll angular acceleration, respectively, and u is the control input;
模型中各种系数定义为The various coefficients in the model are defined as
其中,a1到a5是和攻角相关的变量,c1和c2是由后掠角决定的常数;Among them, a 1 to a 5 are variables related to the angle of attack, and c 1 and c 2 are constants determined by the sweep angle;
定义状态量x(t)=[x1,x2]T∈R2,其中x1=φ,以后掠角作为切换信号,可将变体飞行器机翼摇滚模型转化为2阶单输入单输出非线性切换系统Define the state quantity x(t)=[x 1 ,x 2 ] T ∈ R 2 , where x 1 =φ, Using the sweep angle as the switching signal, the wing rock model of the variant aircraft can be transformed into a second-order single-input single-output nonlinear switching system
其中,是系统状态向量;uσ(t)∈R是系统输入,y∈R是系统输出;函数σ(t)∈{1,2}是切换信号;是未知非线性函数;d1(t)=0.1cos(t2),d2(t)=0.1sin(t)是引入的外部干扰;in, is the system state vector; u σ(t) ∈ R is the system input, y ∈ R is the system output; the function σ(t) ∈ {1,2} is the switching signal; is the unknown nonlinear function; d 1 (t)=0.1cos(t 2 ), d 2 (t)=0.1 sin(t) is the external disturbance introduced;
步骤2:将系统输入非线性描述为Step 2: Describe the system input nonlinearity as
其中,uv,k∈R是带死区的输入,bl,1=0.5,br,1=0.1,bl,2=0.8,br,2=0.3;where u v,k ∈ R is the input with dead zone, b l,1 = 0.5, b r,1 = 0.1, b l,2 = 0.8, b r,2 = 0.3;
可将(2)进一步描述为(2) can be further described as
其中in
信号uk存在如下关系The signal u k has the following relationship
其中是uv,k的上界值;in is the upper bound value of u v,k ;
则系统(1)可进一步写为Then system (1) can be further written as
步骤3:针对未知函数用神经网络来逼近Step 3: For unknown functions Approximate with a neural network
其中,是神经网络最优权重向量,是神经网络基函数向量,εf,k是神经网络残差且存在是正常数;in, is the optimal weight vector of the neural network, is the neural network basis function vector, ε f,k is the neural network residual and exists is a normal number;
则的估计值可写为but The estimated value of can be written as
其中,和是神经网络最优权重向量估计值;in, and is the estimated value of the optimal weight vector of the neural network;
定义Δuk=uv,k-uc,k,则x2的导数可写为Define Δu k =u v,k -u c,k , then the derivative of x 2 can be written as
其中,步骤4:针对非线性切换系统(1),基于复合学习策略设计自适应滑模控制器;in, Step 4: Design an adaptive sliding mode controller based on a composite learning strategy for the nonlinear switching system (1);
定义输出跟踪误差其中e=x1-yd,yd是控制参考指令;Define Output Tracking Error Where e=x 1 -y d , y d is the control reference command;
设计滑模面为The sliding surface is designed as
s=[ΛT 1]E (10)s=[Λ T 1]E (10)
其中,Λ=τ,τ>0;Among them, Λ=τ, τ>0;
滑模面s的导数为The derivative of the sliding surface s is
其中, in,
设计控制器为Design the controller as
其中in
其中,是Dk(t)的估计值,βk是正的设计参数,mk是滑模增益函数;in, is the estimated value of D k (t), β k is a positive design parameter, and m k is the sliding mode gain function;
构造预测误差z2NN为Constructing the prediction error z 2NN as
其中,可由如下的平行估计模型得到in, It can be obtained by the following parallel estimation model
其中,λk是正的设计参数;in, λk is a positive design parameter;
设计滑模增益函数为The sliding mode gain function is designed as
mk=-γz,kλkz2NN (18)m k = -γ z,k λ k z 2NN (18)
其中,γz,k是正的设计参数;where γz,k is a positive design parameter;
设计神经网络权重更新律为The weight update law of the designed neural network is
其中,γf,k和δf,k是正的设计参数;where γ f,k and δ f,k are positive design parameters;
设计切换扰动观测器为The switching disturbance observer is designed as
其中,ξ2是中间变量,Lk是正的设计参数;where ξ 2 is an intermediate variable, and L k is a positive design parameter;
步骤4:根据步骤3中(12)得到的控制量uc,k,返回到变体飞行器机翼摇滚模型(1),对滚转角φ进行跟踪控制。Step 4: According to the control amount uc ,k obtained in (12) in step 3, return to the rock model (1) of the variant aircraft wing, and perform tracking control on the roll angle φ.
本发明未详细说明部分属于领域技术人员公知常识。The parts of the present invention that are not described in detail belong to the common knowledge of those skilled in the art.
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CN113268023B (en) * | 2021-05-13 | 2022-07-22 | 哈尔滨工程大学青岛船舶科技有限公司 | Sliding Mode Predictive Congestion Control System for Satellite Spatial Information Transmission Network |
CN113377013B (en) * | 2021-06-10 | 2022-10-18 | 江南大学 | A Continuous Disturbance Trigger Control Method for Saturated Nonlinear Systems |
CN113608438B (en) * | 2021-07-22 | 2024-02-20 | 浙江中烟工业有限责任公司 | A fan system and its control method |
CN114114925B (en) * | 2021-11-29 | 2023-09-08 | 江南大学 | Data-driven collaborative self-adaptive sliding mode constraint control method and system |
CN114371623B (en) * | 2022-01-10 | 2022-12-23 | 南京工业大学 | A Fractional Order Global Sliding Mode Control Method for Neural Network Observer in Structural Thermal Test |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105867134A (en) * | 2016-04-27 | 2016-08-17 | 南京航空航天大学 | Control method for continuous switching movement of double-framework airplane skin detection robot |
CN107450323A (en) * | 2017-09-05 | 2017-12-08 | 西北工业大学 | Hypersonic aircraft reentry stage neutral net Hybrid Learning control method |
CN108828957A (en) * | 2018-08-20 | 2018-11-16 | 西北工业大学 | Aircraft overall situation finite time neural network control method based on handover mechanism |
CN109062234A (en) * | 2018-08-20 | 2018-12-21 | 西北工业大学 | A kind of non-minimum phase aircraft Hybrid Learning sliding-mode control |
CN110376887A (en) * | 2019-07-11 | 2019-10-25 | 西北工业大学 | Aircraft discrete sliding mode intelligent control method based on time-varying sliding formwork gain |
-
2020
- 2020-11-14 CN CN202011274007.4A patent/CN112327627B/en active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105867134A (en) * | 2016-04-27 | 2016-08-17 | 南京航空航天大学 | Control method for continuous switching movement of double-framework airplane skin detection robot |
CN107450323A (en) * | 2017-09-05 | 2017-12-08 | 西北工业大学 | Hypersonic aircraft reentry stage neutral net Hybrid Learning control method |
CN108828957A (en) * | 2018-08-20 | 2018-11-16 | 西北工业大学 | Aircraft overall situation finite time neural network control method based on handover mechanism |
CN109062234A (en) * | 2018-08-20 | 2018-12-21 | 西北工业大学 | A kind of non-minimum phase aircraft Hybrid Learning sliding-mode control |
CN110376887A (en) * | 2019-07-11 | 2019-10-25 | 西北工业大学 | Aircraft discrete sliding mode intelligent control method based on time-varying sliding formwork gain |
Non-Patent Citations (2)
Title |
---|
HOSM observer based robust adaptive hypersonic flight control using composite learning;Yixin Cheng 等;《Neurocomputing》;20180315;第295卷;第98-107页 * |
一类切换非线性系统的自适应反步滑模控制;王素珍 等;《济南大学学报(自然科学版)》;20200630;第34卷(第3期);第267-274页 * |
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