Complexity

Volume 2019, Article ID 1507051, 9 pages

https://doi.org/10.1155/2019/1507051

## Neural Terminal Sliding-Mode Control for Uncertain Systems with Building Structure Vibration

^{1}The School of Mechanical and Electric Engineering, Guangzhou University, Guangzhou 510006, China^{2}The School of Automation, Guangdong University of Technology, Guangzhou 510320, China

Correspondence should be addressed to Wenqiang Wu; nc.ude.uhzg@qww_zg and Chunliang Zhang; moc.361@lczhn

Received 29 October 2018; Revised 8 March 2019; Accepted 26 March 2019; Published 10 April 2019

Academic Editor: Yan-Ling Wei

Copyright © 2019 Jianhui Wang et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

#### Abstract

Building structures occasionally suffer from unpredictable earthquakes, which can cause severe damage and can threaten human lives. Thus, effective control methods are needed to protect against structural vibration in buildings, and rapid finite-time convergence is a key performance indicator for vibration control systems. Rapid convergence can be ensured by applying a sliding-mode control method. However, this method would result in chattering issue, which would weaken the feasibility of the physical implementation. To address this problem, a neural terminal sliding-mode control method is proposed. The proposed method is combined with a terminal sliding-mode and a hyperbolic tangent function to ensure that the considered system can be stabilized in finite-time without chattering. Finally, the control effect of the proposed method is compared with that of LQR (linear quadratic regulator) control and switching function control. The simulation results showed that the proposed method can ensure rapid convergence while the chattering issue can be eliminated effectively. And the structural building vibration can be suppressed effectively too.

#### 1. Introduction

Earthquakes are a natural phenomenon that can cause severe damage to building structures and can threaten human lives.Today, it remains difficult to predict when an earthquake may occur, and seismic waves are uncertain. Both factors pose challenges for building structure controllers during design. Thus, it is worth researching advanced antiseismic technology to protect building structures from vibration.

During the past few decades, many modern control methods, including linear quadratic regulator (LQR) control [1–3], sliding-mode control [4–6], and semiactive control [7–10], have proven active and effective measures in the area of structural vibration. These methods can stabilize the system. However, building structure vibrations cannot be effectively suppressed in finite-time, which might cause severe damage to the building structure.

To guarantee the rapid convergence of the system, sliding-mode control is applied for structural vibration control. According to the current deviation of the system and various derivative values, the vibration control method can change by jumping in the transient process. Therefore, the system can enter the sliding plane and obtain sliding-mode motion quickly, which ensures the rapid convergence of the system [11–14]. Meanwhile, the application of sliding-mode control is always accompanied by chattering, which may weaken the physical implementation rate.

By applying the hyperbolic tangent function, direct switching of the control input can be avoided, and chattering can be eliminated. This approach allows the system to respond to the outside world in a timely manner and facilitates physical implementation. However, most control methods use Lyapunov stability, which belongs to the field of asymptotic stability research; in this field, the stable time goes toward infinity, which is meaningless for the control of structural vibrations [15–19].

As research on the combination of Lyapunov stability theory and the theorem of homogeneity has developed, finite-time stable control methods have progressed. Finite-time stable control has been widely applied, for example, in the position control of synchronous permanent magnet motors and in high-precision guidance laws [20–23]. However, the finite-time stable control method is rarely applied to structural vibrations.

However, uncertainties that could affect system stability exist in practical systems. The guarantee of finite-time stability when considering a system with uncertainty is an outstanding research area. Neural networks can be used to approximate any nonlinear function with generalization. Thus, a Radial Basis Function (RBF) neural network is adopted to address this problem; see [24–28].

The neural terminal sliding-mode control method is proposed in this work to address an uncertain system with structural vibrations. An RBF neural network is combined with a terminal sliding-mode and the hyperbolic tangent function to handle an uncertain system with structural vibrations. The finite-time stabilization method is used to stabilize the building structural system in finite-time. As shown below, the main compensatory mechanism and contributions of the proposed schemes are summarized as follows.

Most traditional control methods were researched without considering uncertainty and rapid convergence performance, which may result in serious damage to building structures [3–5]. Rapid convergence can be ensured by applying a sliding-mode control method; however, uncertainty affects rapid convergence, which poses a considerable challenge regarding controller design. Thus, a combination of a RBF neural network and terminal sliding-mode control is proposed to solve the uncertainty issues and ensure rapid convergence.

In practice, chattering weakens the feasibility of physical implementation, which means that stable timeliness cannot be guaranteed and substantial structural damage may occur [8–10]; therefore, the feasibility of physical applications is important to determine. In this paper, finite-time control is combined with a hyperbolic tangent function to eliminate chattering and prevent structural building vibrations in finite time.

The remainder of this paper is organized as follows. In Section 2, models and a problem formulation are proposed. Then, the neural terminal sliding-mode control method is proposed to address the uncertain system with structural vibrations. In Section 3, the control effect of the proposed method is compared with the LQR control method and switching function control. The simulation results showed that the proposed method can effectively eliminate chattering, ensure rapid convergence, and effectively suppress structural building vibration. Finally, conclusions are given in Section 4.

#### 2. Modeling and Analysis of Building Structures

##### 2.1. Modeling Building Structures under Earthquake Conditions

A building structure optimized for interlaminar shear is used for modeling. Thus, the n-layer building structure can be simplified as a building structure with n degrees of freedom. Under earthquake conditions, the dynamic equation can be described as follows:where is the displacement vector of the structure, is the displacement of the* i*th floor (relative to the ground) of the building structure, is the stiffness matrix, is the mass matrix, is the transformation matrix of the ground seismic acceleration, where is the unit column of , is the damping matrix, is the ground seismic acceleration, is a matrix denoting the location of the actuators, and is the control input.

Defining a state-space vectorwhere and . Equation (1) is rewritten as follows:where .

According to the rank criterion, the controllability of the building structure under earthquake conditions can be certified. Thus, structural vibration can be restrained by designing a control variable setting as follows: where is a variable derived from (2) and (3) as follows:

Setting , the system is composed of a mutually independent subsystem, which is described as follows:

The seismic wave is uncertain. Thus, further analysis is difficult. Neural finite-time stable control is used to handle this problem.

##### 2.2. Approximation System Research

Analyzing the system above, seismic wave is assumed to be known. The RBF neural network is chosen to approximate because it can effectively approximate the unknown variable [29]. The network algorithm is designed as follows:where is an input of the network, is the* j*th joint of the hidden-layer of the network, , and is the desirable permission of the network, is the approximate error of the network, and . According to the above analysis, the model can be described as follows:

Because function is unknown, to offset the effect of function on the system, the RBF neural network is used to approximate the function, which allows (4) to be rewritten as follows:

##### 2.3. Terminal Sliding-Mode Controller Design

is the* i*th controller, and denotes the displacement of the* i*th floor (relative to the ground) of the building structure. Thus, the structural building model with uncertain earthquakes can be described as follows:

*Remark 1. * is the actual seismic wave, and is the estimated value approximated by RBF; therefore, is the error of the actual value and the estimated value. Thus, .

The sliding-mode function is designed as follows:where , , , and . Thus, we can obtainwhere must satisfy the Hurwitz condition ().

*Remark 2. *For of the system to track desired state within appointed time , [30] proposes a method of constructing terminal function . The method is designed as follows.

To achieve global robustness, , i.e., . To achieve the convergence of appointed time , . Therefore, the terminal function can be described as follows: where is a coefficient that can be obtained by solving the equation.

The derivative of (13) can be obtained as follows:If , then

*Remark 3. *The hyperbolic tangent function is as follows:where and the speed of the inflection point of the hyperbolic tangent smooth function depends on the value of .

The controller is designed as follows:where is a positive design parameter.

Derived from (16) and (18):A Lyapunov function is defined as follows: Then, the derivative of (20) can be obtained as follows:

##### 2.4. Stability Analysis

Derived from (21):

Lemma 4 (see [31]). *For any given , and there is an inequality: **The explanation for Lemma 4 is as follows.**According to the definition of the hyperbolic tangent function, we have the following:**Thus, it can be said that**Hence,**Then,**Thus, the consequence can be achieved such that which completes the proof.*

Setting , so :

From the above discussion, system stability can be proven.

From the expression of function , when , and (i.e., ). Hence, the initial system state is already on the sliding surface, which eliminates the arrival phase of the sliding film and ensures the global robustness and stability of the closed-loop system.

*Remark 5. *Because the system has global robustness, i.e., , design function can be used to ensure that so that the tracking error converges to zero within finite time .

To achieve convergence for a specified time , it is necessary to ensure that when , , and , where meets the requirements of (14). Therefore, when , function and its derivative can be written as follows:The derivative of (30) is as follows:The derivative of (31) is as follows:When , we can obtain . Thus,The necessary conditions for the establishment of are as follows: Similarly, when , the necessary condition for is as follows:Three ternary equations can be sorted by the above equations:According to , to express the ternary equations, the above three equations can be written as the following three forms:The solution to the above equations is as follows:Moreover, through further solutions:where is defined as a finite function set.

*Remark 6. *From (30), we know , which means that Lyapunov function must be nonincreasing with respect to the time variable. Because the initial value is finite, it follows that . Thus, is bounded, which allows us to obtain the following:Derived from (21), it is determined that and are bounded.

Because and the closed-loop system enters the sliding stage at the initial moment, we can determine that , i.e., . Because is bounded and is a constant, can converge within finite time , and can converge within finite time . Therefore, according to the preset terminal function , the output error can be guaranteed to converge to zero within a finite time to ensure the system can be stabilized within a finite time.

#### 3. Control Method Analysis

In this section, three control methods were simulated: LQR control, switching function control, and neural terminal sliding-mode finite-time stable control. Based on a three-layer building structure, the system is subjected to an El earthquake wave. The maximum earthquake acceleration is . The parameters of the proposed control are set as, , and . The mass matrix, damping matrix, stiffness matrix, and the position of the examples are set as follows:

*Example 1. *No control, LQR control, and proposed control for the three-layer building structure are simulated. The contrast simulation curves of displacement, velocity, acceleration response, and control force are shown in Figures 1–4.

According to Table 1, the LQR control compared with no control, the maximum displacement of the first, second, and third floors decreased by 59.9%, 67.6%, and 71.9%, respectively. And the maximum velocity decreased by 34.3%, 46%, and 46.4%, respectively. Meanwhile, the proposed control method compared with no control, the maximum displacement of the first, second, and third floors decreased by 97.1%, 98.4%, and 98.7%, respectively. And the maximum velocity decreased by 92.6%, 94.8%, and 94.6%, and maximum acceleration decreased by 64.7%, 56.5%, and 54.5%, respectively.