CN107145074A - A kind of high-speed trimaran pitching stabilization control method based on sliding moding structure convergence law - Google Patents

A kind of high-speed trimaran pitching stabilization control method based on sliding moding structure convergence law Download PDF

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CN107145074A
CN107145074A CN201710501665.4A CN201710501665A CN107145074A CN 107145074 A CN107145074 A CN 107145074A CN 201710501665 A CN201710501665 A CN 201710501665A CN 107145074 A CN107145074 A CN 107145074A
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原新
张欣
王靖淇
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Harbin Engineering University
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Abstract

本发明提供的是一种基于滑模变结构趋近律法的高速三体船减纵摇控制方法。该方法设计不同级别的随机海浪模型;使用ANSYS平台分析获得三体船水动力系数,建立三体船纵向运动数学模型,得到纵向运动响应垂荡高度和纵摇角度;以垂荡高度和纵摇角度为输入,设计基于趋近律的滑模变结构控制律,得到输出迎流角度改变量;建立减摇附体T型翼和压浪板的纵向运动模型,将减摇附体迎流角度改变量作为减摇附体控制系统输入,输出为减摇附体为三体船提供的纵向力和力矩,反馈作用在高速三体船纵向运动系统。该方法可应用于军用及民用多体船的稳定性控制方面,能够有效地减弱海浪对于三体船运动稳定性的影响,提高乘客舒适度。

The invention provides a method for pitch reduction control of a high-speed trimaran based on sliding mode variable structure approach law. This method designs random wave models of different levels; uses the ANSYS platform to analyze and obtain the hydrodynamic coefficient of the trimaran, establishes the mathematical model of the longitudinal motion of the trimaran, and obtains the heave height and pitch angle in response to the longitudinal motion; Angle is the input, and a sliding mode variable structure control law based on reaching law is designed to obtain the change in the output flow angle; the longitudinal motion model of the T-shaped wing of the anti-rolling appendage and the wave control plate is established, and the change of the incoming flow angle of the anti-rolling appendage is The quantity is used as the input of the anti-rolling appendage control system, and the output is the longitudinal force and moment provided by the anti-rolling appendage for the trimaran, and the feedback acts on the longitudinal motion system of the high-speed trimaran. The method can be applied to the stability control of military and civilian multihull ships, and can effectively reduce the influence of waves on the motion stability of the trimaran and improve passenger comfort.

Description

一种基于滑模变结构趋近律法的高速三体船减纵摇控制方法A Pitching Control Method for High Speed Trimaran Based on Sliding Mode Variable Structure Approach Law

技术领域technical field

本发明属于高速三体船纵向运动减摇控制领域,特别涉及一种基于滑模变结构趋近律法的高速三体船减纵摇控制方法。The invention belongs to the field of anti-rolling control of high-speed trimaran longitudinal motion, in particular to a method for anti-rolling control of high-speed trimaran based on sliding mode variable structure approach law.

背景技术Background technique

经典控制理论和现代控制理论都是需要被控对象拥有清晰的数学模型,但实际的控制对象并不理想,系统的机构可能很复杂,规模很庞大,变量很多,参数多变且耦合,或系统有非线性,不确定性,时变性,滞后性的情况,传统控制理论很难用数学进行分析,并建立合乎运动规律的数学模型。通常建模时要对非线性采用线性化,分布参数要采用集中参数,时变系数需要采用定常系数,建模和实际可能会有很大出入,因此在实际控制时传统控制算法很难奏效。在三体船纵向减摇控制系统中采用传统控制方法如PID控制器,虽然算法简单,但是却只适用于被控对象参数不变,非线性不严重的系统,无法做到在三体船快速航行中实现动态控制,而且根据实验结果其控制效果也远远不能达到需求。LQR控制方法的最优控制效果取决于加权阵Q和R的选取,这样会产生很大的工作量并且误差很大。Both classical control theory and modern control theory require the controlled object to have a clear mathematical model, but the actual controlled object is not ideal. The system mechanism may be complex, large in scale, with many variables, variable and coupled parameters, or the system In the case of nonlinearity, uncertainty, time-varying, and hysteresis, traditional control theory is difficult to use mathematics to analyze and establish a mathematical model that conforms to the law of motion. Usually, linearization should be used for nonlinear modeling, lumped parameters should be used for distribution parameters, and constant coefficients should be used for time-varying coefficients. There may be great discrepancies between modeling and reality, so traditional control algorithms are difficult to work in actual control. The traditional control method such as PID controller is used in the trimaran longitudinal anti-rolling control system. Although the algorithm is simple, it is only suitable for the system with constant parameters of the controlled object and non-serious nonlinearity. Dynamic control is realized during navigation, and according to the experimental results, its control effect is far from meeting the requirements. The optimal control effect of the LQR control method depends on the selection of the weighting matrix Q and R, which will produce a large workload and a large error.

滑模变结构控制方法优点是可进行设计并与对象参数和扰动无关,且可快速响应、抗扰动能力强、物理实现简单等。针对高速三体船减摇控制,传统的PID控制方法已经不能满足在复杂无规则海况中实现快速、非线性的实时控制了,而滑模变结构由于其具有的以上特点可以更好地适应这些复杂情况,而目前对于滑模方法应用于新兴高速三体船减纵摇方面目前还没有明确的设计。The advantage of the sliding mode variable structure control method is that it can be designed and has nothing to do with the object parameters and disturbances, and it can respond quickly, has strong anti-disturbance ability, and is simple in physical implementation. For the anti-rolling control of high-speed trimaran, the traditional PID control method can no longer satisfy the fast and nonlinear real-time control in complex and irregular sea conditions, and the sliding mode variable structure can better adapt to these conditions due to its above characteristics. However, there is no clear design for the application of the sliding mode method to the pitch reduction of emerging high-speed trimarans.

发明内容Contents of the invention

本发明的目的在于提供一种可以更好地改善高速、细长的三体船纵向运动稳定性的基于滑模变结构趋近律法的高速三体船减纵摇控制方法。The object of the present invention is to provide a high-speed trimaran pitch reduction control method based on sliding mode variable structure approach law that can better improve the longitudinal motion stability of a high-speed, slender trimaran.

本发明一种基于滑模变结构趋近律法的高速三体船减纵摇控制方法包括如下步骤:A kind of pitch reduction control method of a high-speed trimaran based on sliding mode variable structure approach law of the present invention comprises the following steps:

步骤一:根据国际气象局海浪标准设计不同级别的随机海浪模型;Step 1: Design random wave models of different levels according to the wave standard of the International Meteorological Bureau;

步骤二:利用随机海浪模型,使用ANSYS平台分析获得三体船水动力系数,再根据水动力系数建立高速三体船纵向运动数学模型,得到高速三体船纵向运动响应垂荡高度和纵摇角度;Step 2: Using the random wave model, use the ANSYS platform to analyze and obtain the hydrodynamic coefficient of the trimaran, and then establish a mathematical model of the longitudinal motion of the high-speed trimaran according to the hydrodynamic coefficient, and obtain the heave height and pitch angle of the longitudinal motion of the high-speed trimaran ;

步骤三:利用上述高速三体船纵向运动响应垂荡高度和纵摇角度,设计基于趋近律的滑模变结构控制律,得到控制输出迎流角度改变量;Step 3: Using the longitudinal motion of the above-mentioned high-speed trimaran to respond to the heave height and pitch angle, design a sliding mode variable structure control law based on the reaching law, and obtain the change in the control output head angle;

步骤四:建立减摇附体T型翼和压浪板的升力和力矩计算模型,利用减摇附体迎流角度改变量得到减摇附体为三体船提供的纵向力和力矩,反馈作用在高速三体船纵向运动系统。Step 4: Establish the lift and moment calculation model of the T-shaped wing of the anti-rolling appendage and the wave suppression plate, and use the change of the oncoming angle of the anti-rolling appendage to obtain the longitudinal force and moment provided by the anti-rolling appendage for the trimaran, and the feedback acts on Longitudinal motion system of high-speed trimaran.

步骤一所述的随机海浪模型具体为:The random sea wave model described in step 1 is specifically:

(1)根据国际气象学组织规定的不同级别海浪对应的不同有效波高H和频段,使用MATLAB编程实现不同级别的随机海浪模型的建立;(1) According to the different significant wave heights H and frequency bands corresponding to different levels of waves specified by the International Meteorological Organization, use MATLAB programming to realize the establishment of different levels of random wave models;

(2)模型建立基于有理谱法,设计的有理谱定义如下所示:(2) The model is established based on the rational spectrum method, and the designed rational spectrum is defined as follows:

其中,Sx(ω)是所涉及实平稳随机过程X(t)的功率谱密度函数,P(ω)和Q(ω)则是ω实系数多项式且分母阶次必须要高于分子;Among them, S x (ω) is the power spectral density function of the involved real stationary random process X(t), P(ω) and Q(ω) are ω real coefficient polynomials and the order of the denominator must be higher than that of the numerator;

海浪最终模型为:The final model of the wave is:

εi代表构成海浪波的相位角,认为是在(0,2π)区间内的随机变量,即εi=rand(0,2π),S(wi)海浪在圆频率wi处的功率谱密度,N为样本数;ε i represents the phase angle of the ocean wave, which is considered as a random variable in the interval (0, 2π), that is, ε i =rand(0,2π), the power spectrum of S(w i ) ocean wave at the circular frequency w i Density, N is the number of samples;

(3)海浪模块的输入为时钟,将输出作为后面模块的输入。(3) The input of the wave module is the clock, and the output is used as the input of the following modules.

步骤二所述的三体船纵向运动模型具体为:The trimaran longitudinal motion model described in step 2 is specifically:

(1)使用ANSYS平台分析得到不同航速下三体船水动力系数;(1) Using the ANSYS platform to analyze and obtain the hydrodynamic coefficient of the trimaran at different speeds;

(2)根据三体船在海中的航速、海浪模型以及遭遇频率,使用MATLAB平台“ss2tf”函数进行实现对三体船纵向运动模型的具体解耦和求解。(2) According to the speed of the trimaran in the sea, the wave model and the encounter frequency, the "ss2tf" function of the MATLAB platform is used to realize the specific decoupling and solution of the longitudinal motion model of the trimaran.

步骤三所述的基于趋近律的滑模变结构控制律具体为:The sliding mode variable structure control law based on reaching law described in step three is specifically:

(1)建立三体船的纵向运动控制系统变结构控制:(1) Establish the variable structure control of the longitudinal motion control system of the trimaran:

指数趋近律设计为:The exponential reaching law is designed as:

其中:为指数趋近项;in: is the exponent approach term;

得到变结构控制:Get variable structure control:

(2)对控制律进行柔化处理:(2) Soften the control law:

其中,ξ为一个自主选定的小整数;Among them, ξ is a small integer selected independently;

最终得到的基于趋近律的滑模变结构控制律为:The final sliding mode variable structure control law based on reaching law is:

其中,参数ε决定系统的鲁棒性能,值越大鲁棒性能越好;参数q决定控制系统逐渐靠近超平面的速度,q越大,系统趋近的速度越快,A、B为系统状态矩阵,C为待求的控制矩阵,可通过使用MATLAB编译平台,利用极点配置法求得,ξ为一个自主选定的小整数。Among them, the parameter ε determines the robust performance of the system, the larger the value, the better the robust performance; the parameter q determines the speed at which the control system gradually approaches the hyperplane, the larger the q, the faster the system approaches, and A and B are the system states Matrix, C is the control matrix to be sought, which can be obtained by using the MATLAB compilation platform and using the pole allocation method, and ξ is a small integer selected independently.

步骤四所述的减摇附体T型翼和压浪板的升力和力矩计算模型:The lift and moment calculation model of the anti-roll T-wing attached to the body and the wave control plate described in step 4:

迎流角度改变量与对应该角度为三体船纵向提供的力之间为一个非线性关系,同时得到了该力对应的力矩:There is a nonlinear relationship between the amount of change in the incoming flow angle and the force provided for the longitudinal direction of the trimaran corresponding to this angle, and the moment corresponding to the force is obtained at the same time:

MT/F=da·FT/F M T/F = d a F T/F

式中:ρ为海水密度,1.025×103kg/m3;A为T型翼或压浪板的投影面积,V为船速;α为减摇附体迎流攻角改变量;CL(α)为减摇附体的升力系数,在攻角α很小时一般可以视为常量,da为T型翼安装位置和重心之间的垂直距离;Ft、Ff和Mt、Mf分别表示T型翼和压浪板提供的升力和力矩。In the formula: ρ is the seawater density, 1.025×10 3 kg/m 3 ; A is the projected area of T-shaped wing or wave breaker, V is the speed of the ship; α is the change in the angle of attack of the anti-rolling appendage; C L ( α) is the lift coefficient of the anti-rolling appendage, which can generally be regarded as a constant when the angle of attack α is small; d a is the vertical distance between the installation position of the T-shaped wing and the center of gravity; F t , F f and M t , M f represent the lift and moment provided by the T-shaped wing and the breaker, respectively.

本发明设计的控制方法针对目前最常用的高速三体船在海中航行时的纵向减摇,明显的降低了运动中的船体垂荡和纵摇。实现了将滑模控制方法用于高速三体船纵向减摇功能,适用于海况复杂、高船速的海上航行环境,可应用于军用及民用多体船的稳定性控制方面,能够有效地减弱海浪对于三体船运动稳定性的影响,提高乘客舒适度。The control method designed by the invention is aimed at the longitudinal antirolling of the currently most commonly used high-speed trimaran when navigating in the sea, and obviously reduces the heave and pitch of the hull in motion. The sliding mode control method has been applied to the longitudinal anti-rolling function of the high-speed trimaran, which is suitable for the sea navigation environment with complex sea conditions and high speed, and can be applied to the stability control of military and civilian multi-hull ships, and can effectively reduce the The impact of waves on the motion stability of the trimaran improves the comfort of passengers.

附图说明Description of drawings

图1(a)是本发明中设计的国际气候局规定的SSN5级随机海浪三维模型;Fig. 1 (a) is the SSN5 level random ocean wave three-dimensional model that the International Meteorological Bureau of Design stipulates in the present invention;

图1(b)是本发明中设计的国际气候局规定的SSN6级随机海浪三维模型;Fig. 1 (b) is the SSN6 grade random ocean wave three-dimensional model that the International Meteorological Bureau of Design stipulates in the present invention;

图2是本发明设计的控制系统结构框图;Fig. 2 is the structural block diagram of the control system that the present invention designs;

图3是本发明控制方法流程图;Fig. 3 is a flowchart of the control method of the present invention;

图4是本发明三体船纵向运动模型结构图。Fig. 4 is a structural diagram of a trimaran longitudinal motion model of the present invention.

具体实施方式detailed description

下面结合附图对本发明进行详细说明。The present invention will be described in detail below in conjunction with the accompanying drawings.

基于滑模变结构趋近律法的高速三体船减纵摇控制方法流程图如图3所示,具体流程如下:The flow chart of the high-speed trimaran pitch reduction control method based on the sliding mode variable structure approach law is shown in Figure 3, and the specific process is as follows:

(1)随机海浪模型的建立:(1) Establishment of random wave model:

海浪可视为是由一系列波幅,波长以及初相位均不同的余弦波叠加组成的,海浪瞬时波高可以表示为:Ocean waves can be considered to be composed of a series of cosine waves with different amplitudes, wavelengths, and initial phases. The instantaneous wave height of ocean waves can be expressed as:

其中,H为海面的平均潮高,ζi是组成波的波幅,ki是波数,θi是组成波传播方向与x轴的角度,ωi是组成波的角频率,εi是组成波的相位角,可以认为是在(0,2π)区间内的随机变量,x为瞬时海浪沿x轴方向的宽度,z为瞬时海浪沿z轴方向的高度。Among them, H is the average tidal height of the sea surface, ζ i is the amplitude of the component wave, ki is the wave number, θ i is the angle between the propagation direction of the component wave and the x-axis, ω i is the angular frequency of the component wave, and ε i is the component wave The phase angle of can be considered as a random variable in the interval (0,2π), x is the width of the instantaneous wave along the x-axis direction, and z is the height of the instantaneous wave along the z-axis direction.

实验中令海平面平均波高H=0,且固定,可简化海浪模型为:In the experiment, the average sea level wave height H=0 and fixed, the wave model can be simplified as:

采用有理谱法进行离散化:Discretization using the rational spectral method:

有理谱定义如下所示:A rational spectrum is defined as follows:

其中,Sx(ω)是所涉及实平稳随机过程X(t)的功率谱密度函数,P(ω)和Q(ω)则是ω实系数多项式且分母阶次必须要高于分子。Among them, S x (ω) is the power spectral density function of the involved real stationary random process X(t), P(ω) and Q(ω) are polynomials with real coefficients of ω and the order of the denominator must be higher than that of the numerator.

设有理海浪的逼近谱形式如下:The approximation spectrum form of the unreasonable ocean wave is as follows:

令s=jω,则:Let s=jω, then:

由参数估计理论可知:According to the parameter estimation theory, we know that:

S(ωi)=Sxi) (6)S(ω i )=S xi ) (6)

其中,i=1,2,···,N,(N>2n)且S(ω)为海浪的功率谱密度:Wherein, i=1, 2,..., N, (N>2n) and S(ω) is the power spectral density of the ocean wave:

其中,A=8.10×10-3g2是有义波高,ω是波浪圆频率。Among them, A=8.10×10 -3 g 2 , is the significant wave height, and ω is the wave circular frequency.

将上式代入(2)得到海浪最终模型为:Substituting the above formula into (2) to obtain the final model of the ocean wave is:

其中,εi代表构成海浪波的相位角,认为是在(0,2π)区间内的随机变量,即εi=rand(0,2π),S(wi)是海浪在圆频率wi处的功率谱密度,N为样本数。Among them, ε i represents the phase angle of the ocean wave, which is considered as a random variable in the interval (0, 2π), that is, ε i =rand(0,2π), S(w i ) is the wave at the circular frequency w i The power spectral density of , N is the number of samples.

给出SSN5和SSN6级随机海浪模型三维图像示例见图1(a)和图1(b)。Examples of 3D images of SSN5 and SSN6 stochastic wave models are shown in Fig. 1(a) and Fig. 1(b).

海浪模块的输入为时钟,将输出作为后面模块的输入。The input of the wave module is the clock, and the output is used as the input of the following modules.

(2)三体船纵向运动模型设计:(2) Trimaran longitudinal motion model design:

首先使用ANSYS Workbench平台的AQWA软件模块进行实验,经过移动模型调节吃水,又由于实体在AQWA中不能进行计算,所以接下来对于模型进行抽壳,得到外表面的一层厚度设置为0的壳;再进行对于高速三体船进行切水线、构造船舶整体结构。接着插入质心后设置回转半径:Kxx=0.163m,Kyy=0.807m,Kzz=0.807m。最后设置圆频率:实验中使用40节航速下的圆频率分别是:0.42249rad/s,0.56275rad/s,0.69203rad/s,0.81299rad/s,0.92691rad/s,1.03491rad/s,1.18757rad/s,1.42196rad/s,1.63671rad/s。在仿真得到的文件夹中找到生成.DAT文件,经过Aqwa16.0处理后得到三体船的水动力系数aii、bii、ciiFirst, use the AQWA software module of the ANSYS Workbench platform to conduct experiments, adjust the draft by moving the model, and because the entity cannot be calculated in AQWA, the model is then shelled to obtain a shell whose outer surface thickness is set to 0; Carry out waterline cutting for the high-speed trimaran and construct the overall structure of the ship. Then set the radius of gyration after inserting the center of mass: K xx =0.163m, K yy =0.807m, K zz =0.807m. Finally, set the circular frequency: the circular frequencies used in the experiment at a speed of 40 knots are: 0.42249rad/s, 0.56275rad/s, 0.69203rad/s, 0.81299rad/s, 0.92691rad/s, 1.03491rad/s, 1.18757rad /s, 1.42196rad/s, 1.63671rad/s. Find the generated .DAT file in the folder obtained by simulation, and get the hydrodynamic coefficients a ii , b ii , c ii of the trimaran after being processed by Aqwa16.0.

由图4可知,该系统设计分为海浪-力的转化部分以及力-角度的转化部分,最终输出的是三体船纵向的垂荡高度和纵摇角度。It can be seen from Fig. 4 that the system design is divided into the wave-force conversion part and the force-angle conversion part, and the final output is the longitudinal heave height and pitch angle of the trimaran.

由达朗贝尔理论可得高速船纵摇和升沉耦合方程:According to d'Alembert's theory, the coupled equation of pitch and heave of high-speed ship can be obtained:

等式左边是船的动态模型,右边是海浪与力的关系,由等式左边可以推导出船在力作用下的运动模型,右边可以推导出船在海浪作用下的受力模型。式中m33是船质量,aij是海水对船的附加质量,x3是升沉量,bij是阻尼系数,cij是恢复系数,x5是纵摇量,m55是纵摇惯性力矩,这些水动力系数是在ANSYS平台上根据不同三体船的尺寸参数仿真得到的。Ft、Ff和Mt、Mf分别表示T型翼和压浪板提供的升力和力矩,Fwave和Mwave分别为海浪作用在三体船上的垂荡扰动力和纵摇干扰力矩。The left side of the equation is the dynamic model of the ship, and the right side is the relationship between waves and forces. The motion model of the ship under the action of force can be deduced from the left side of the equation, and the force model of the ship under the action of waves can be deduced from the right side. In the formula, m 33 is the mass of the ship, a ij is the additional mass of seawater to the ship, x 3 is the heave, b ij is the damping coefficient, c ij is the restitution coefficient, x 5 is the pitching amount, m 55 is the pitching inertia These hydrodynamic coefficients are simulated on the ANSYS platform according to the size parameters of different trimarans. F t , F f and M t , M f represent the lift and moment provided by the T-shaped wing and the wave suppressor, respectively, and F wave and M wave are the heave disturbance force and pitch disturbance moment of the waves acting on the trimaran, respectively.

在三体船处于不同航行速度、不同遭遇频率时根据方程(10)可以得到不同的海浪-力、力-角度的传递函数方程。当选择航速为40节,海浪为SSN5级,遭遇频率为1.5rad/s时,可得到的传递函数方程如下:When the trimaran is at different sailing speeds and different encounter frequencies, different wave-force and force-angle transfer function equations can be obtained according to equation (10). When the selected speed is 40 knots, the sea wave is SSN5, and the encounter frequency is 1.5rad/s, the transfer function equation that can be obtained is as follows:

力-垂荡: Force-heave:

力矩-垂荡: Moment-heave:

力-纵摇: Force-Pitch:

力矩-纵摇: Moment-Pitch:

(3)滑模变结构模块的设计(3) Design of sliding mode variable structure module

三体船的纵向运动线性微分方程的状态空间方程表示为:The state space equation of the longitudinal motion linear differential equation of the trimaran is expressed as:

式中:是控制向量,其中x3为垂荡位移和垂荡速度,x5是纵摇角度和纵摇角速度。In the formula: is the control vector, where x 3 and is the heave displacement and heave velocity, x 5 and are the pitch angle and pitch angular velocity.

据此选取线性切换函数:Choose the linear switching function accordingly:

S(x)=Cx(t) (14)S(x)=Cx(t) (14)

设计滑模面:根据滑模变结构控制理论知,在滑动超平面上有:Design sliding mode surface: According to the sliding mode variable structure control theory, there are:

s(x)=Cx=C1x1+C2x2=0 (15)s(x)=Cx=C 1 x 1 +C 2 x 2 =0 (15)

由上式可以导出在超平面上:The above formula can be derived on the hyperplane:

得到系统滑动方程为:The sliding equation of the system is obtained as:

对于三体船的纵向运动控制系统建立变结构控制:Establish variable structure control for the longitudinal motion control system of the trimaran:

采用应用最广泛的指数趋近律:Using the most widely used exponential reaching law:

其中:为指数趋近项,则有系统状态空间方程可得到:in: is an exponential approach term, then the system state space equation can be obtained:

引入指数趋近律后即可得到以纵向运动系统状态空间方程中的A、B、C、D矩阵为参数的滑模控制律,其中未知项只有C矩阵,使用MATLAB编译平台,利用极点配置法求出C矩阵;After introducing the exponential reaching law, the sliding mode control law with the A, B, C, and D matrices in the state space equation of the longitudinal motion system as parameters can be obtained. Among them, the unknown item is only the C matrix, using the MATLAB compilation platform, and using the pole allocation method Find the C matrix;

可得到变结构控制:Variable structure control is available:

其中:参数q的大小决定了趋近切换超平面速度的快慢,其值越大,速度越快,但如果过大又会引起震荡;参数ε的大小决定着系统的鲁棒性能,其值越大,鲁棒性越好,但抖振幅值也越大并且影响系统的稳态精度。Among them: the size of the parameter q determines the speed of approaching the switching hyperplane, the larger the value, the faster the speed, but if it is too large, it will cause shocks; the size of the parameter ε determines the robustness of the system, the larger the value The larger the value, the better the robustness, but the larger the chattering amplitude will be and affect the steady-state accuracy of the system.

对控制律进行柔化处理来防止抖振现象:Soften the control law to prevent chattering:

所以得到最终的滑模控制律为:So the final sliding mode control law is:

唯一需要确定的是矩阵C,而C的求取都可以使用极点配置法通过MATLAB编程进行实现,在三体船处于不同航速,且遭遇频率不同时,会得到不同的滑模变结构的切换函数矩阵C。The only thing that needs to be determined is the matrix C, and the calculation of C can be realized by using the pole configuration method through MATLAB programming. When the trimaran is at different speeds and the encounter frequency is different, different switching functions of the sliding mode variable structure will be obtained Matrix C.

将这些切换函数矩阵C代入滑模控制律式(23)中,即可得到对应的滑模变结构三体船纵向运动减摇控制方法,从而实现三体船纵向运动减摇的非线性动态控制。Substituting these switching function matrices C into the sliding mode control law formula (23), the corresponding sliding mode variable structure trimaran longitudinal motion anti-rolling control method can be obtained, so as to realize the nonlinear dynamic control of trimaran longitudinal motion anti-rolling .

(4)减摇附体控制模块设计(4) Design of anti-rolling attachment control module

使用ANSYS 16.0进行参数化求解,航速固定为40节/小时,实验中对于T型翼和压浪板来说都令迎流攻角改变量作为参数,二者的输入是经过滑模控制器处理纵向响应后得到的调整角度,这个角度为需要的角度与现在的迎流角度的差值,所以二者由滑模控制律提供的角度变化所改变的升力和力矩的计算模型均为:ANSYS 16.0 is used for parametric solution, and the speed is fixed at 40 knots/hour. In the experiment, both the T-shaped wing and the wave breaker use the change of the angle of attack as a parameter, and the input of the two is processed by the sliding mode controller. The adjustment angle obtained after the response, this angle is the difference between the required angle and the current on-flow angle, so the calculation models of the lift and moment changed by the angle change provided by the sliding mode control law are:

Mt/f=da·Ft/f (25)M t/f = d a F t/f (25)

其中:ρ为海水密度,1.025×103kg/m3;A为T型翼的表面积,m2;V为船速,m/s;α为减摇附体迎流攻角改变量(注:T型翼在实际工况中的有效迎流攻角由三部分组成,T型翼的转角,船的纵摇角,以及纵向运动产生的附加角,且高速船的纵摇角对T型翼的减摇效果有减弱效果,附加角对T型翼的减摇效果有增强效果)。CL(α)为升力系数,攻角α很小时可以视为常量,da为减摇附体安装位置和重心之间的垂直距离。在SIMULINK中对于上述描述的实现只需利用简单的逻辑运算模块进行组合实现上面公式即可。Where: ρ is the seawater density, 1.025×10 3 kg/m 3 ; A is the surface area of the T-shaped wing, m 2 ; V is the speed of the ship, m/s; : The effective oncoming attack angle of the T-shaped wing in the actual working condition is composed of three parts, the rotation angle of the T-shaped wing, the pitch angle of the ship, and the additional angle generated by the longitudinal motion, and the pitch angle of the high-speed ship has a significant effect on the T-shaped The anti-rolling effect of the wing has a weakening effect, and the additional angle has a strengthening effect on the anti-rolling effect of the T-shaped wing). C L (α) is the lift coefficient, which can be regarded as a constant when the angle of attack α is small, and d a is the vertical distance between the installation position of the anti-rolling appendage and the center of gravity. In SIMULINK, the realization of the above description only needs to be combined with simple logic operation modules to realize the above formula.

将上述得到的由减摇附体提供的调整力和力矩反馈到三体船纵向运动控制系统中叠加在原有的力上,从而实现减摇闭环系统的实现。The adjustment force and moment provided by the anti-rolling appendage obtained above are fed back to the trimaran longitudinal motion control system and superimposed on the original force, so as to realize the realization of the anti-rolling closed-loop system.

(5)基于滑模的高速三体船纵向运动模型在MATLAB中实现的具体步骤:(5) The specific steps to realize the longitudinal motion model of high-speed trimaran based on sliding mode in MATLAB:

具体实现见图2。选择高速三体船航速为40节,在SSN5级海浪ξ(t)作为输入时,经过海浪-力/力矩模块处理后得到垂荡力F3和纵摇力F5,将其作为三体船纵向运动模型力-垂荡/纵摇模块的输入,得到垂荡x3和纵摇x5以及它们的变化加速度将这四个量作为滑模控制器的输入,经过基于趋近律滑模控制方法的处理后得到减摇附体T型翼和压浪板迎流攻角需要的改变量α,将这个改变量作为输入经减摇附体运动模块后得到两种减摇附体为三体船提供的纵向力和力矩分别为Ft、Ff和Mt、Mf,并将其作为反馈量作用到力-垂荡/纵摇模块前,实现高速三体船纵向运动稳定控制。See Figure 2 for the specific implementation. The speed of the high-speed trimaran is selected as 40 knots. When the SSN5 level wave ξ(t) is used as input, the heave force F 3 and the pitch force F 5 are obtained after processing by the wave-force/moment module, which is used as the trimaran Longitudinal motion model force - input of heave/pitch module, get heave x 3 and pitch x 5 and their change acceleration with These four quantities are used as the input of the sliding mode controller, and after processing based on the approach law sliding mode control method, the required change amount α of the T-shaped wing attached to the anti-rolling body and the oncoming attack angle of the wave control plate is obtained, and the change amount As input, the longitudinal forces and moments provided by the two anti-rolling appendages for the trimaran are F t , F f and M t , M f respectively after being passed through the motion module of the anti-rolling appendage, and they are used as feedback to act on the force -In front of the heave/pitch module, the longitudinal motion stability control of the high-speed trimaran is realized.

Claims (5)

1.一种基于滑模变结构趋近律法的高速三体船减纵摇控制方法,其特征是:包括如下步骤:1. a high-speed trimaran anti-pitch control method based on sliding mode variable structure approach law, is characterized in that: comprise the steps: 步骤一:根据国际气象局海浪标准设计不同级别的随机海浪模型;Step 1: Design random wave models of different levels according to the wave standard of the International Meteorological Bureau; 步骤二:利用随机海浪模型,使用ANSYS平台分析获得三体船水动力系数,再根据水动力系数建立高速三体船纵向运动数学模型,得到高速三体船纵向运动响应垂荡高度和纵摇角度;Step 2: Using the random wave model, use the ANSYS platform to analyze and obtain the hydrodynamic coefficient of the trimaran, and then establish a mathematical model of the longitudinal motion of the high-speed trimaran according to the hydrodynamic coefficient, and obtain the heave height and pitch angle of the longitudinal motion of the high-speed trimaran ; 步骤三:利用上述高速三体船纵向运动响应垂荡高度和纵摇角度,设计基于趋近律的滑模变结构控制律,得到控制输出迎流角度改变量;Step 3: Using the longitudinal motion of the above-mentioned high-speed trimaran to respond to the heave height and pitch angle, design a sliding mode variable structure control law based on the reaching law, and obtain the change in the control output head angle; 步骤四:建立减摇附体T型翼和压浪板的升力和力矩计算模型,利用减摇附体迎流角度改变量得到减摇附体为三体船提供的纵向力和力矩,反馈作用在高速三体船纵向运动系统。Step 4: Establish the lift and moment calculation model of the T-shaped wing of the anti-rolling appendage and the wave suppression plate, and use the change of the oncoming angle of the anti-rolling appendage to obtain the longitudinal force and moment provided by the anti-rolling appendage for the trimaran, and the feedback acts on Longitudinal motion system of high-speed trimaran. 2.根据权利要求1所述的基于滑模变结构趋近律法的高速三体船减纵摇控制方法,其特征在于:2. the high-speed trimaran anti-rolling control method based on sliding mode variable structure approach law according to claim 1, is characterized in that: 步骤一所述的随机海浪模型具体为:The random sea wave model described in step 1 is specifically: (1)根据国际气象学组织规定的不同级别海浪对应的不同有效波高H和频段,使用MATLAB编程实现不同级别的随机海浪模型的建立;(1) According to the different significant wave heights H and frequency bands corresponding to different levels of waves specified by the International Meteorological Organization, use MATLAB programming to realize the establishment of different levels of random wave models; (2)模型建立基于有理谱法,设计的有理谱定义如下所示:(2) The model is established based on the rational spectrum method, and the designed rational spectrum is defined as follows: <mrow> <msub> <mi>S</mi> <mi>x</mi> </msub> <mrow> <mo>(</mo> <mi>&amp;omega;</mi> <mo>)</mo> </mrow> <mo>=</mo> <mfrac> <mrow> <mi>P</mi> <mrow> <mo>(</mo> <mi>&amp;omega;</mi> <mo>)</mo> </mrow> </mrow> <mrow> <mi>Q</mi> <mrow> <mo>(</mo> <mi>&amp;omega;</mi> <mo>)</mo> </mrow> </mrow> </mfrac> </mrow> <mrow> <msub> <mi>S</mi> <mi>x</mi> </msub> <mrow> <mo>(</mo> <mi>&amp;omega;</mi> <mo>)</mo> </mrow> <mo>=</mo> <mfrac> <mrow> <mi>P</mi> <mrow> <mo>(</mo> <mi>&amp;omega;</mi> <mo>)</mo> </mrow> </mrow> <mrow> <mi>Q</mi> <mrow> <mo>(</mo> <mi>&amp;omega;</mi> <mo>)</mo> </mrow> </mrow> </mfrac> </mrow> 其中,Sx(ω)是所涉及实平稳随机过程X(t)的功率谱密度函数,P(ω)和Q(ω)则是ω实系数多项式且分母阶次必须要高于分子;Among them, S x (ω) is the power spectral density function of the involved real stationary random process X(t), P(ω) and Q(ω) are ω real coefficient polynomials and the order of the denominator must be higher than that of the numerator; 海浪最终模型为:The final model of the wave is: <mrow> <mi>&amp;zeta;</mi> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>=</mo> <munderover> <mo>&amp;Sigma;</mo> <mrow> <mi>i</mi> <mo>=</mo> <mn>1</mn> </mrow> <mrow> <mi>N</mi> <mo>-</mo> <mn>1</mn> </mrow> </munderover> <msqrt> <mrow> <mn>2</mn> <mi>S</mi> <mrow> <mo>(</mo> <msub> <mi>&amp;omega;</mi> <mi>i</mi> </msub> <mo>)</mo> </mrow> <msub> <mi>&amp;Delta;&amp;omega;</mi> <mi>i</mi> </msub> </mrow> </msqrt> <mi>c</mi> <mi>o</mi> <mi>s</mi> <mrow> <mo>(</mo> <msub> <mi>&amp;omega;</mi> <mi>i</mi> </msub> <mi>t</mi> <mo>+</mo> <msub> <mi>&amp;epsiv;</mi> <mi>i</mi> </msub> <mo>)</mo> </mrow> </mrow> <mrow> <mi>&amp;zeta;</mi> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> <mo>=</mo> <munderover> <mo>&amp;Sigma;</mo> <mrow> <mi>i</mi> <mo>=</mo> <mn>1</mn> </mrow> <mrow> <mi>N</mi> <mo>-</mo> <mn>1</mn> </mrow> </munderover> <msqrt> <mrow> <mn>2</mn> <mi>S</mi> <mrow> <mo>(</mo> <msub> <mi>&amp;omega;</mi> <mi>i</mi> </msub> <mo>)</mo> </mrow> <msub> <mi>&amp;Delta;&amp;omega;</mi> <mi>i</mi> </msub> </mrow> </msqrt> <mi>c</mi> <mi>o</mi> <mi>s</mi> <mrow> <mo>(</mo> <msub> <mi>&amp;omega;</mi> <mi>i</mi> </msub> <mi>t</mi> <mo>+</mo> <msub> <mi>&amp;epsiv;</mi> <mi>i</mi> </msub> <mo>)</mo> </mrow> </mrow> εi代表构成海浪波的相位角,认为是在(0,2π)区间内的随机变量,即εi=rand(0,2π),S(wi)海浪在圆频率wi处的功率谱密度,N为样本数;ε i represents the phase angle of the ocean wave, which is considered as a random variable in the interval (0, 2π), that is, ε i =rand(0,2π), the power spectrum of S(w i ) ocean wave at the circular frequency w i Density, N is the number of samples; (3)海浪模块的输入为时钟,将输出作为后面模块的输入。(3) The input of the wave module is the clock, and the output is used as the input of the following modules. 3.根据权利要求1所述的基于滑模变结构趋近律法的高速三体船减纵摇控制方法,其特征在于:3. the high-speed trimaran anti-rolling control method based on sliding mode variable structure approach law according to claim 1, is characterized in that: 步骤二所述的三体船纵向运动模型具体为:The trimaran longitudinal motion model described in step 2 is specifically: (1)使用ANSYS平台分析得到不同航速下三体船水动力系数;(1) Using the ANSYS platform to analyze and obtain the hydrodynamic coefficient of the trimaran at different speeds; (2)根据三体船在海中的航速、海浪模型以及遭遇频率,使用MATLAB平台“ss2tf”函数进行实现对三体船纵向运动模型的具体解耦和求解。(2) According to the speed of the trimaran in the sea, the wave model and the encounter frequency, the "ss2tf" function of the MATLAB platform is used to realize the specific decoupling and solution of the longitudinal motion model of the trimaran. 4.根据权利要求1所述的基于滑模变结构趋近律法的高速三体船减纵摇控制方法,其特征在于:4. the high-speed trimaran anti-rolling control method based on sliding mode variable structure approach law according to claim 1, is characterized in that: 步骤三所述的基于趋近律的滑模变结构控制律具体为:The sliding mode variable structure control law based on reaching law described in step three is specifically: (1)建立三体船的纵向运动控制系统变结构控制:(1) Establish the variable structure control of the longitudinal motion control system of the trimaran: <mrow> <mi>u</mi> <mo>=</mo> <mfenced open = "{" close = ""> <mtable> <mtr> <mtd> <msup> <mi>u</mi> <mo>+</mo> </msup> <mo>,</mo> <mi>s</mi> <mo>&gt;</mo> <mn>0</mn> </mtd> </mtr> <mtr> <mtd> <msup> <mi>u</mi> <mo>-</mo> </msup> <mo>,</mo> <mi>s</mi> <mo>&lt;</mo> <mn>0</mn> </mtd> </mtr> </mtable> </mfenced> </mrow> <mrow> <mi>u</mi> <mo>=</mo> <mfenced open = "{" close = ""> <mtable> <mtr> <mtd> <msup> <mi>u</mi> <mo>+</mo> </msup> <mo>,</mo> <mi>s</mi> <mo>&gt;</mo> <mn>0</mn> </mtd> </mtr> <mtr> <mtd> <msup> <mi>u</mi> <mo>-</mo> </msup> <mo>,</mo> <mi>s</mi> <mo>&lt;</mo> <mn>0</mn> </mtd> </mtr> </mtable> </mfenced> </mrow> 指数趋近律设计为:The exponential reaching law is designed as: 其中:为指数趋近项;in: is the exponent approach term; 得到变结构控制:Get variable structure control: (2)对控制律进行柔化处理:(2) Soften the control law: <mrow> <mi>&amp;theta;</mi> <mrow> <mo>(</mo> <mi>s</mi> <mo>)</mo> </mrow> <mo>=</mo> <mfrac> <mi>s</mi> <mrow> <mo>|</mo> <mi>s</mi> <mo>|</mo> <mo>+</mo> <mi>&amp;xi;</mi> </mrow> </mfrac> </mrow> <mrow> <mi>&amp;theta;</mi> <mrow> <mo>(</mo> <mi>s</mi> <mo>)</mo> </mrow> <mo>=</mo> <mfrac> <mi>s</mi> <mrow> <mo>|</mo> <mi>s</mi> <mo>|</mo> <mo>+</mo> <mi>&amp;xi;</mi> </mrow> </mfrac> </mrow> 其中,ξ为一个自主选定的小整数;Among them, ξ is a small integer selected independently; 最终得到的基于趋近律的滑模变结构控制律为:The final sliding mode variable structure control law based on reaching law is: 其中,参数ε决定系统的鲁棒性能,值越大鲁棒性能越好;参数q决定控制系统逐渐靠近超平面的速度,q越大,系统趋近的速度越快,A、B为系统状态矩阵,C为待求的控制矩阵,可通过使用MATLAB编译平台,利用极点配置法求得,ξ为一个自主选定的小整数。Among them, the parameter ε determines the robust performance of the system, the larger the value, the better the robust performance; the parameter q determines the speed at which the control system gradually approaches the hyperplane, the larger the q, the faster the system approaches, and A and B are the system states Matrix, C is the control matrix to be sought, which can be obtained by using the MATLAB compilation platform and using the pole allocation method, and ξ is a small integer selected independently. 5.根据权利要求1所述的基于滑模变结构趋近律法的高速三体船减纵摇控制方法,其特征在于:5. the high-speed trimaran anti-rolling control method based on sliding mode variable structure approach law according to claim 1, is characterized in that: 步骤四所述的减摇附体T型翼和压浪板的升力和力矩计算模型:The lift and moment calculation model of the anti-roll T-wing attached to the body and the wave control plate described in step 4: 迎流角度改变量与对应该角度为三体船纵向提供的力之间为一个非线性关系,同时得到了该力对应的力矩:There is a nonlinear relationship between the amount of change in the incoming flow angle and the longitudinal force provided by the trimaran corresponding to this angle, and the moment corresponding to the force is obtained at the same time: MT/F=da·FT/F M T/F = d a F T/F 式中:ρ为海水密度,1.025×103kg/m3;A为T型翼或压浪板的投影面积,V为船速;α为减摇附体迎流攻角改变量;CL(α)为减摇附体的升力系数,在攻角α很小时一般可以视为常量,da为T型翼安装位置和重心之间的垂直距离;Ft、Ff和Mt、Mf分别表示T型翼和压浪板提供的升力和力矩。In the formula: ρ is the seawater density, 1.025×10 3 kg/m 3 ; A is the projected area of T-shaped wing or wave breaker, V is the speed of the ship; α is the change in the angle of attack of the anti-rolling appendage; C L ( α) is the lift coefficient of the anti-rolling appendage, which can generally be regarded as a constant when the angle of attack α is small; d a is the vertical distance between the installation position of the T-shaped wing and the center of gravity; F t , F f and M t , M f represent the lift and moment provided by the T-shaped wing and the breaker, respectively.
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