Adaptive Fuzzy Human-in-the-Loop Control for Unmanned Surface Vehicles in Environmental Monitoring Applications

Abstract

This paper presents a human-in-the-loop (HiTL) intelligent adaptive control scheme for unmanned surface vehicles (USVs) that accounts for uncertain dynamics, with the goal of effectively monitoring marine pollutants. To tackle the challenges posed by complex aquatic monitoring environments, this approach integrates human intelligence into the navigation strategy of USVs, allowing for superior path planning through human decision-making. Additionally, a potential field-based obstacle avoidance strategy is developed to ensure the safe operation of USVs within this HiTL framework. To address issues related to system uncertainties, we propose a novel adaptive fuzzy control strategy based on convex optimization, which enhances overall control performance. Finally, stability analysis and simulation results demonstrate the effectiveness of the proposed method. The verification results show that compared with traditional adaptive fuzzy controllers, our control strategy effectively reduces control errors.

1. Introduction

In recent years, the growing disparity between social demand and resource supply has led people to focus on the exploration and utilization of marine resources. However, the increase in human activities in the ocean has resulted in severe marine pollution [1,2,3,4]. Incidents such as the Deepwater Horizon oil spill and the Ever Given blockage in the Suez Canal have highlighted the critical importance of preventing marine pollution and protecting the environment. As a result, automated detection technologies for marine pollution have become a significant area of research [5,6,7].

Intelligent USVs, which have emerged alongside advancements in artificial intelligence technologies, represent a new platform for marine monitoring [8,9,10,11,12]. Compared to traditional environmental monitoring vessels, USVs offer several advantages, including lower costs, high autonomy and flexibility, and a wider operational range. These features make them a promising next-generation technology for marine environmental monitoring. However, achieving precise control of USVs in complex marine environments remains a challenging issue. And this challenge mainly comes from the underactuated characteristics of USVs, the uncertain dynamics of the system, and unknown external disturbances. Currently, most USVs are underactuated structures, meaning their control input is less than their degrees of freedom. In [13], a distributed bearing-based formation control scheme with finite-time convergence is proposed for multiple underactuated USVs. By employing a guidance-point-based model transformation method, the dimension of the underactuated tracking error dynamics can be reduced from three to two. In [14], the trajectory tracking problem of underactuated USVs subject to input saturation, unmodeled dynamics, and marine environmental disturbances is investigated. A coordinate transformation is constructed to address the under-actuation issue of USVs, and a new event-triggered condition is introduced to significantly reduce control execution frequency and transmission load. In [15], a robust collision-avoidance formation navigation problem for multiple USVs is addressed, where USVs are modeled as underactuated nonlinear systems subject to state and input constraints. A novel distributed model predictive control (MPC)-based controller is developed to achieve collision-free formation navigation. Furthermore, a class of distributed collision-avoidance formation navigation strategies is proposed and utilized, allowing the control inputs of USVs to be determined synchronously. In [16], a prescribed performance path-following control algorithm for USVs is proposed, which employs an output-based threshold rule and a shift function to perform parallel maritime search tasks. In the guidance module, a finite-boundary-based guidance principle is developed, and a position threshold rule is adopted to avoid continuous computation of heading reference signals.

For unmodeled dynamics or external disturbance issues of USVs, adaptive control strategies or disturbance observers are often used to compensate for system uncertainties [17,18,19]. In [20], an adaptive trajectory tracking control algorithm with guaranteed transient performance is proposed for underactuated USVs. Neural networks are employed to approximate unknown external disturbances and the uncertain hydrodynamic characteristics of the USVs. In [21], the trajectory tracking control problem of underactuated USVs under state and input quantization is investigated. At the dynamic level, a fuzzy adaptive quantized control method based on an event-triggered mechanism is proposed. In [22], the trajectory tracking problem of USVs under unmeasurable velocity and unknown disturbances is investigated. By combining a fixed-time extended state observer and a fixed-time differentiator, a fixed-time sliding mode control law is proposed, in which a saturation function is employed to ensure that the terminal sliding surface avoids the singularity area. In [23], the fixed-time prescribed performance trajectory tracking control of USVs with unknown dynamics and disturbances is investigated. An improved prescribed performance function is introduced to achieve user-defined performance, including both transient and steady-state behaviors of the USVs. In [24], the distributed optimal cooperative control (DOCC) problem of USVs subject to network channel limitations and communication interruptions is investigated. To address the challenges of scarce and intermittent communication channels, an intermittent interlaced periodic event-triggered mechanism is developed in the auxiliary system.

It is important to note that while extensive research has been conducted on control systems for USVs, most existing control strategies depend on predefined trajectories or specified map information to develop corresponding controllers. This method may not be suitable for marine pollution monitoring, as such pollution incidents often occur suddenly and randomly, making their location and extent highly unpredictable. As a result, the distribution of pollutants and other essential information cannot be determined in advance. Given the complexities of the marine environment, current algorithms face significant challenges in effectively monitoring contaminated waters. To tackle the obstacles presented by complex marine environments, we have designed an HiTL control strategy for USVs. The purpose of HiTL is to enhance the system’s adaptability in complex and uncertain environments through the use of human intelligence. In [25], the HiTL control strategy is combined with an improved prescribed performance control method and applied to the cooperative control of unmanned aerial vehicle systems. In [26], the focus is on the consensus tracking control problem of an HiTL unmanned aerial vehicle attitude system subject to external disturbances. The proposed event-based adaptive neural controller ensures finite-time tracking of the attitude systems. In [27], the study, under a directed communication graph, addresses the observer-based HiTL asymptotic consensus control problem for multi-agent ship systems that are also affected by external disturbances. In [28], a human-in-the-loop framework based on deep reinforcement learning is proposed to achieve autonomous dynamic soaring for improving the endurance of fixed-wing unmanned aerial vehicles. In [29], to solve the problem of increased load on teleoperated ground vehicle operators caused by communication delay and low transparency, a human-in-the-loop experiment is conducted to evaluate the ePTGC framework. The results showed that the framework can reduce load and improve stability. Ref. [30] has designed a human-supervised task replanning system for unmanned underwater vehicles in ocean missions, and the effectiveness of the design has been verified through simulation. Ref. [31] proposes a human-in-the-loop backstepping reinforcement learning algorithm (human agent interaction) for nonlinear strict feedback multi-agent systems under unknown fault disturbances, achieving fast convergence and capture control. Ref. [32] proposes a human-in-the-loop collaborative path tracking architecture for marine vehicles with unknown disturbances (human-controlled virtual leader’s path update speed), based on the RED observer and OFCTC method to achieve finite-time path tracking. In summary, under the background of HiTL research, existing work has provided multiple approaches to solving deterministic problems. However, when applied to monitoring marine pollution, the HiTL control strategy may present potential safety issues. This approach often utilizes a joystick-like operation mode for controlling USVs. However, the human operator is usually located far from the actual environment, making it challenging to accurately perceive real-time ocean conditions. Consequently, the operator may lack precise awareness of the vessel’s orientation, velocity, and position, which can lead to operational errors. For instance, during the detection of marine pollutants, USVs are typically required to collect samples along the borders of a contaminated area instead of entering it directly. Unfortunately, because the operator in the remote control center cannot accurately discern the USV’s surrounding environment, the vessel may inadvertently drift into the polluted zone. This could potentially cause disturbances or even damage to the USV. As a result, achieving precise and safe control of USVs under the HiTL mechanism presents a significant challenge, particularly when the system is influenced by uncertain dynamic parameters.

This paper proposes a novel HiTL adaptive fuzzy control strategy for USVs with uncertain dynamics, aimed at achieving effective monitoring of marine pollutants. The effectiveness of the proposed method is validated through both theoretical analysis and simulation results. Compared with existing approaches, the main contributions of this work are as follows.

1.

This paper proposes a novel HiTL intelligent control strategy for USVs used in marine pollution monitoring. Compared with existing methods [33,34,35], the proposed approach leverages human intelligence to better address the challenges of USVs’ navigation and control in complex marine environments, thereby achieving more effective pollutant monitoring. Furthermore, based on the HiTL control framework, a potential field-based obstacle avoidance strategy is designed to achieve effective coordination between autonomous avoidance and manual control, enhancing the security performance of the USVs.

2.

Based on convex optimization theory, this paper designs an adaptive fuzzy control strategy for USVs to effectively compensate for uncertain dynamics. Moreover, a novel adaptive update mechanism is proposed to address the potential issue of excessive parameter growth under the HiTL framework. Compared with existing approaches [36,37,38], the proposed method effectively mitigates the adverse effects of uncertainties on control performance.

The structure of this paper is as follows: Section 2 presents the problem description. Section 3 focuses on the design of the navigation and control algorithms as well as the stability analysis. Section 4 provides the simulation results for validation, and Section 5 concludes the paper.

2. Model and Problem Statement

2.1. Dynamic Model

In this section, we describe in detail the three-degree-of-freedom kinematics and dynamics of the underactuated USVs. As shown in Figure 1, two coordinate frames are introduced to describe the USVs motion in planar space, where $O_E{X}_E{Y}_E$ is the earth-fixed frame and $o_b{x}_b{y}_b$ the body-fixed frame. The nonlinear mathematical model of the three-degree-of-freedom (3-DOF) of the USVs is as follows [39]:

$$\begin{array}{c}\hfill \begin{array}{c}\dot{u}={\displaystyle \frac{1}{m-X_{\dot{u}}}}[(m-Y_{\dot{v}})vr+X_{u\left|u\right|}u\left|u\right|+X_{u}u+{\tau }_x]\hfill \\ \dot{v}={\displaystyle \frac{1}{m-Y_{\dot{v}}}}[(-m+X_{\dot{u}})ur+Y_{v\left|v\right|}v\left|v\right|+Y_{v}v]\hfill \\ \dot{r}={\displaystyle \frac{1}{I_z-N_{\dot{r}}}}[(-X_{\dot{u}}+Y_{\dot{v}})vu+N_{r\left|r\right|}r\left|r\right|+N_{r}r+{\tau }_z]\hfill \\ \dot{x}=ucos\left(\psi \right)-vsin\left(\psi \right)\hfill \\ \dot{y}=usin\left(\psi \right)+vcos\left(\psi \right)\hfill \\ \dot{\psi }=r\hfill \end{array}\end{array}$$

(1)

where $(x,y)$ represents the position coordinate of the USVs, and $\psi$ represents the heading angle. u and v represent the surge velocity and sway velocity of the USVs, respectively. r is the heading angular velocity of the USVs. m is the ship mass. $X_{\dot{u}}$, $Y_{\dot{v}}$, and $N_{\dot{r}}$ represent hydrodynamic added masses. $X_u$, $Y_v$, and $N_r$ are the linear damping coefficients. $X_{\left|u\right|u},Y_{\left|v\right|v},N_{\left|r\right|r}$ represent the second-order nonlinear drag coefficients related to surge velocity, lateral drift speed, and steering speed, respectively. $I_z$ represents the moment of inertia about the vertical axis. ${\tau }_u$ and ${\tau }_r$ are the control inputs representing surge force and yaw moment, respectively. In this paper, it is assumed that all the dynamic coefficients in Equation (1) are unknown.

2.2. Control Objective

The objective of this article is to design an adaptive fuzzy control strategy that incorporates human actions for a USV system with highly uncertain and unknown dynamics. By leveraging human intelligence, the USVs can navigate to a designated monitoring area at a specified speed, effectively monitor pollutants, and avoid entering danger zones to prevent potential safety hazards.

This paper discusses the challenges associated with the HiTL adaptive intelligent control strategy in comparison to the existing literature. These challenges are primarily reflected in three key aspects. First, in HiTL control modes, human control actions are often applied suddenly. Unmanned vessels used for environmental monitoring frequently undertake multiple tasks, making it difficult to coordinate current operations with abrupt human actions. Ensuring stable vessel performance in these situations is a significant challenge. The second issue is that operators, under HiTL control, often cannot accurately perceive the vessel’s surroundings in real-time. This leads to delayed interventions, increasing the difficulty of obstacle avoidance and introducing potential safety risks. The third challenge arises from the highly nonlinear and uncertain dynamics of unmanned vessels. Since operators generally control these vessels from a distance, they struggle to fully understand the mechanical characteristics of the hull, which complicates the control process. As far as the author is aware, currently, there are still shortcomings in HiTL control strategies for USVs used for environmental monitoring when addressing certain specific challenges [25,26,27]. This gap in the literature is one of the motivations for this paper.

Assumption 1 

([39]). The left and right hull of the unmanned surface vehicle is symmetrical and the mass is even.

Assumption 2 

([20]). All the variable states in Equation (1) can be measured by using GPS and IMU modules.

Lemma 1 

([40]). Define the continuous unknown function $f\left(g\right)$ on a compact set Ω. There exists a fuzzy logic system $W^{\mathrm{T}}S\left(\mathrm{g}\right)$ that satisfies the following relation

$$\begin{array}{c}\hfill \underset{g\in \Omega }{sup}|f\left(g\right)-W^{\mathrm{T}}S\left(g\right)|\le \epsilon \end{array}$$

(2)

where $W={[w_1,\dots ,w_J]}^{\mathrm{T}}$ is the ideal constant weight vector, and $S\left(g\right)={[s_1\left(g\right),\dots ,s_J\left(g\right)]}^{\mathrm{T}}/{\sum }_{i=1}^J{s}_i\left(g\right)$ is the basis function vector of the number of fuzzy rules of $J>1$. $s_i$ is chosen as Gaussian functions, for $i=1,\dots ,J,s_i\left(g\right)=exp[-{(x-q_i)}^{\mathrm{T}}(x-q_i)/{\chi }_i^2]$, where $q_i={[q_{i1},q_{i2},\dots ,q_{ij}]}^{\mathrm{T}}$ is the center vector and the width of the Gaussian function is ${\chi }_i$.

Lemma 2 

(Young’s inequality). For $m,n\in R$, the following relationship holds:

$$\begin{array}{c}\hfill mn\le {\displaystyle \frac{z^a}{a}}{\left|m\right|}^a+{\displaystyle \frac{1}{b{z}^b}}{\left|n\right|}^b\end{array}$$

(3)

where $z>0$, $a>1$, $b>1$, and $(a-1)(b-1)=1$.

3. Human-in-Loop Control Adaptive Fuzzy Strategy

To achieve coordinated control between sudden human actions and the preset tasks of USVs, this paper proposes a strategy that separates navigation strategies from control methods. The control strategy diagram is shown in Figure 2. It implements decoupling between the control of forward velocity and heading angle for USVs using a Line-of-Sight (LOS) navigation strategy. This effectively addresses the challenge of underactuated control in unmanned vessels. The surge velocity of the USVs is set to a predefined value, while the tracking angle is determined by human actions and the LOS navigation laws. Consequently, the target angle for the USVs is given by

$$\begin{array}{c}\hfill {\psi }_d={\psi }_H+{\psi }_h\end{array}$$

(4)

where ${\psi }_H$ is defined by human input, while ${\psi }_h$ is automatically calculated based on the LOS algorithm.

4. Navigation Law Design

In this section, a navigation strategy is proposed by combining LOS guidance and APF obstacle avoidance methods, as shown in Figure 3. The LOS algorithm is a common guiding principle in the scene of a straight-line path-following mission. $P_0$ and $P_1$ are path points given in advance. $P_{los}=(x_{los},y_{los})$ is the expectation point on the line segment between the past path point $P_0$ and the current path point $P_1$. The LOS guidance law for a straight line based on the visual distance is

$$\begin{array}{cc}\hfill & {\psi }_{\mathrm{g}}={\alpha }_k+arctan\left({\displaystyle \frac{-e}{{\Delta }_{\mathrm{g}}}}\right)\hfill \end{array}$$

(5)

$$\begin{array}{cc}\hfill & e=-(y_i-y_{\mathrm{g}})sin\left({\alpha }_k\right)+(x_i-x_{\mathrm{g}})cos\left({\alpha }_k\right)\hfill \end{array}$$

(6)

$$\begin{array}{cc}\hfill & {\alpha }_k=arctan{\displaystyle \frac{x_i-x_{i-1}}{y_i-y_{i-1}}}\hfill \end{array}$$

(7)

where ${\Delta }_{\mathrm{g}}$ is the visible distance, ${\alpha }_k$ denotes the path-tangential angle, and e is the vertical distance from the USVs to the reference path. In order to track a given waypoint while avoiding contaminated areas, we have designed an APF algorithm to further modify the path of USVs.

The definition of an attractive field $U_{att}\left(p\right)$ is as follows:

$$\begin{array}{cc}\hfill & U_{att}\left(p\right)={\displaystyle \frac{k_{ap}}{2}}{\rho }_{ul}^2(p_u,p_l)\hfill \end{array}$$

(8)

$$\begin{array}{cc}\hfill & {\rho }_{ul}(p_u,p_l)=\sqrt{{(x-x_{los})}^2+{(y-y_{los})}^2}\hfill \end{array}$$

(9)

where $k_{ap}$ is positive proportional weight coefficients for the position gravitation. ${\rho }_{ul}(p_u,p_l)$ is the relative distance between USVs, and $P_{los}$. $p_u=(x,y)$ is the USV’s position, $p_l=(x_{los},y_{los})$ is the expectation point on the line segment. By computing the negative gradient of $U_{att}\left(p\right)$, we obtain

$$\begin{array}{c}\hfill F_{att}=k_{ap}{\rho }_{ul}{\overrightarrow{n}}_{ul}\end{array}$$

(10)

where $F_{att}$ is the attractive force generated by the relative position, and ${\overrightarrow{n}}_{ul}$ is the motion direction of USVs to $P_{los}$.

The definition of the repulsive field $U_{rep}\left(v\right)$ is

$$\begin{array}{c}\hfill U_{rep}\left(p\right)=\left\{\begin{array}{cc}{\displaystyle \frac{1}{2}}{k}_{rp}{\left({\displaystyle \frac{1}{{\rho }_{uo}}}-{\displaystyle \frac{1}{{\rho }_o}}\right)}^2,\hfill & {\rho }_{uo}<{\rho }_o\hfill \\ 0,\hfill & \mathrm{others}\hfill \end{array}\right.\end{array}$$

(11)

where $k_{rp}$ values are the positive control constant, ${\rho }_{uo}$ is the distance between USVs and the central point of the polluted area, and ${\rho }_o$ denotes the polluted area avoidance radius, polluted area avoidance only when ${\rho }_{pdb}\le {\rho }_d$.

The negative gradient of $U_{rep}\left(p\right)$ gives us the repulsive force $F_{rep}$:

$$\begin{array}{c}\hfill F_{rep}=-k_{rp}\left({\displaystyle \frac{1}{{\rho }_{uo}}}-{\displaystyle \frac{1}{{\rho }_o}}\right){\displaystyle \frac{1}{{\rho }_{uo}^2}}{\overrightarrow{n}}_{ou}\end{array}$$

(12)

where $F_{rep}$ represents the repulsive force arising from the relative position between USVs and the central point of the polluted area, ${\overrightarrow{n}}_{ou}$ is the unit vector from the central point of the polluted area to USVs. Therefore, we choose the resultant force as $F_{total}(x,y)=F_{att}+F_{rep}$. Combining LOS angle and obstacle avoidance angle, the target angle ${\psi }_h=arctan(F_{total\left(y\right)}/F_{total\left(x\right)})$.

4.1. Surge Velocity Controller

In this section, we present the design process of the speed controller. The dynamics of the USVs’ surge velocity is derived as follows

$$\dot{u}={\displaystyle \frac{1}{m-X_{\dot{u}}}}[(m-Y_{\dot{v}})vr+X_{u\left|u\right|}u\left|u\right|+X_{u}u+{\tau }_x]$$

(13)

Define speed error $z_u=u-u_d$. In order to design the control signal ${\tau }_z$, the Lyapunov function is given by

$$\begin{array}{c}\hfill V_1={\displaystyle \frac{1}{2}}{z_u}^2\end{array}$$

(14)

Then, differentiating $V_1$ can produce

$$\begin{array}{c}\hfill {\dot{V}}_1={\displaystyle \frac{z_u}{m-X_{\dot{u}}}}[(m-Y_{\dot{v}})vr+X_{u\left|u\right|}u\left|u\right|+X_{u}u+{\tau }_x]-z_u{\dot{u}}_d\end{array}$$

(15)

By taking advantage of the approximation property of the fuzzy logic system and combining Lemma 1, our controller is designed as

$$\begin{array}{c}\hfill {\tau }_x=-k_1{z}_u-{\theta }_u^{\mathrm{T}}{h}_u\left(X_u\right)\end{array}$$

(16)

where $k_1$ is a positive constant and ${\theta }_u^{\mathrm{T}}{h}_u\left(X\right)$ is the fuzzy logic system. ${\theta }_u$ is the weight vector and $h_u\left(X_u\right)$ is the basic vector with $X_u=[u,v,r,u_e]$.

Then, from (15) and (16), it has

$$\begin{array}{c}\hfill {\dot{z}}_u={\displaystyle \frac{1}{m-X_{\dot{u}}}}[(m-Y_{\dot{v}})vr+X_{u\left|u\right|}u\left|u\right|+X_{u}u]-{\displaystyle \frac{1}{m-X_{\dot{u}}}}{k}_1{z}_u-{\displaystyle \frac{1}{m-X_{\dot{u}}}}{\theta }_u^{\mathrm{T}}{h}_u\left(X_u\right)-{\dot{u}}_d\end{array}$$

(17)

And then, we use a command filter to evaluate the value of ${\dot{u}}_e$.

$$\begin{array}{c}\hfill {\dot{\widehat{z}}}_u=-l_1({\widehat{z}}_u-z_u)\end{array}$$

(18)

where $l_1$ is the positive constant and ${ϵ}_1={\dot{u}}_e-{\dot{\widehat{u}}}_e$ is the approximate error. Combined with (17), we can obtain

$$\begin{array}{cc}\hfill {\dot{\widehat{z}}}_u& ={\displaystyle \frac{1}{m-X_{\dot{u}}}}[(m-Y_{\dot{v}})vr+X_{u\left|u\right|}u\left|u\right|+X_{u}u]-{\displaystyle \frac{1}{m-X_{\dot{u}}}}{k}_1{z}_u-{\dot{u}}_d-{\displaystyle \frac{1}{m-X_{\dot{u}}}}{\theta }_u^{\mathrm{T}}{h}_u\left(X_u\right)-{\epsilon }_1\hfill \\ \hfill & =F_u-k_2{z}_u-{\displaystyle \frac{1}{m-X_{\dot{u}}}}{\theta }_u^{\mathrm{T}}{h}_u\left(X_u\right)\hfill \end{array}$$

(19)

where $k_2$ is a positive constant. And the dynamic function $F_u$ is

$$\begin{array}{c}\hfill F_u={\displaystyle \frac{1}{m-X_{\dot{u}}}}[(m-Y_{\dot{v}})vr+X_{u\left|u\right|}u\left|u\right|+X_{u}u]-{\displaystyle \frac{1}{m-X_{\dot{u}}}}{k}_1{z}_u-{\dot{u}}_d-{\epsilon }_1+k_2{z}_u\end{array}$$

(20)

The above equation illustrates the strong coupling relationship among adaptive parameters, tracking error, and the filter output signal. Due to the nonlinear uncertainty dynamic term $F_u$, the adaptive parameters cannot be determined by using (19). Thus, in order to overcome this issue, we introduce the following cost function

$$\begin{array}{c}\hfill J_u\left({\theta }_u\right)={\displaystyle \frac{1}{2}}{(F_u-{\displaystyle \frac{1}{m-X_{\dot{u}}}}{\theta }_u^{\mathrm{T}}{h}_u\left(X_u\right))}^2\end{array}$$

(21)

It is assumed that the cost function $J_u\left({\theta }_u\right)$ has an ideal value ${\theta }_u^{*}$, which is an “artificial” quantity required for analytical purposes, and it is defined as the value of ${\theta }_u$ that minimizes $J_u\left({\theta }_u\right)$ for all $X_u\in {\Omega }_{X_u}\subset R^n$

$$\begin{array}{c}\hfill {\theta }_u^{*}=arg\underset{{\theta }_u\in R^N}{min}\{\underset{X_u\in {\Omega }_{X_u}}{sup}|F_u-{\theta }_u^{\mathrm{T}}{h}_u\left(X_u\right)|\}\end{array}$$

(22)

where ${\Omega }_{X_u}$ is a compact set. Next, we aim to design the update law of the weight vector ${\theta }_u$ such that ${\theta }_u\to {\theta }_u^{*}$, which can be described by the following minimization problem.

$$\begin{array}{c}\hfill \underset{{\theta }_u\in R^N}{min}{J}_u\left({\theta }_u\right)\end{array}$$

(23)

The Hessian matrix of $J_u\left({\theta }_u\right)$ is derived as

$$\begin{array}{cc}\hfill {\displaystyle \frac{{\partial }^{2}J\left({\theta }_u\right)}{\partial {\theta }_u^2}}& =\left[\begin{array}{cccc}{\displaystyle \frac{{\partial }^{2}J\left({\theta }_u\right)}{\partial {{{\theta }_u}_1}^2}}& {\displaystyle \frac{{\partial }^{2}J\left({\theta }_u\right)}{\partial {{\theta }_u}_1\partial {{\theta }_u}_2}}& ...& {\displaystyle \frac{{\partial }^{2}J\left({\theta }_u\right)}{\partial {{\theta }_u}_1\partial {{\theta }_u}_N}}\\ {\displaystyle \frac{{\partial }^{2}J\left({\theta }_u\right)}{\partial {{\theta }_u}_2\partial {{\theta }_u}_1}}& {\displaystyle \frac{{\partial }^{2}J\left({\theta }_u\right)}{\partial {{{\theta }_u}_2}^2}}& ...& {\displaystyle \frac{{\partial }^{2}J\left({\theta }_u\right)}{\partial {{\theta }_u}_2\partial {{\theta }_u}_N}}\\ ⋮& ⋮& \ddots & ⋮\\ {\displaystyle \frac{{\partial }^{2}J\left({\theta }_u\right)}{\partial {{\theta }_u}_N\partial {{\theta }_u}_1}}& {\displaystyle \frac{{\partial }^{2}J\left({\theta }_u\right)}{\partial {{\theta }_u}_N\partial {{\theta }_u}_2}}& ...& {\displaystyle \frac{{\partial }^{2}J\left({\theta }_u\right)}{\partial {{{\theta }_u}_N}^2}}\end{array}\right]\hfill \\ \hfill & =h_u\left(X_u\right)h_u{\left(X_u\right)}^{\mathrm{T}}\ge 0\hfill \end{array}$$

(24)

Therefore, $J_u\left({\theta }_u\right)$ is a convex function with respect to ${\theta }_u$. Based on the principle of convex optimization, the adaptive law is designed as

$$\begin{array}{c}\hfill {\dot{\theta }}_u={\eta }_u({\dot{\widehat{z}}}_u+k_2{z}_u)h_u\left(X_u\right)\end{array}$$

(25)

where ${\eta }_u$ is the learning rate.

To avoid an excessive increase in adaptive parameters, we further limit the learning rate

$$\begin{array}{c}\hfill {\eta }_u=\left\{\begin{array}{cc}0,\hfill & |-k_1{z}_u-{\theta }_u^{\mathrm{T}}{h}_u\left(X_u\right)|>a_u)\hfill \\ a_u,\hfill & \mathrm{others}\hfill \end{array}\right.\end{array}$$

(26)

where $a_u$ is a positive constant.

4.2. Heading Angle Controller

The dynamic model of heading angle is described as

$$\begin{array}{cc}\hfill \dot{\psi }& =r\hfill \end{array}$$

(27)

$$\begin{array}{cc}\hfill \dot{r}& ={\displaystyle \frac{1}{I_z-N_{\dot{r}}}}[(-X_{\dot{u}}+Y_{\dot{v}})vu+N_{r\left|r\right|}r\left|r\right|+N_{r}r+{\tau }_z]\hfill \end{array}$$

(28)

Define the tracking error angle is ${\psi }_e=\psi -{\psi }_d$. Then, we choose the following Lyapunov function $V_2={\displaystyle \frac{1}{2}}{{\psi }_e}^2$. ${\dot{V}}_2$ is derived as

$$\begin{array}{cc}\hfill {\dot{V}}_2& =z_{\psi }{\dot{\psi }}_e=z_{\psi }(\dot{\psi }-{\dot{\psi }}_d)=z_{\psi }(z_r+{\alpha }_1-{\dot{\psi }}_d)\hfill \end{array}$$

(29)

where $z_r=r-{\alpha }_1$ is the control error and ${\alpha }_1$ is the virtual control signal. Typically, the value of ${\dot{\psi }}_d$ is determined using the LOS method, making it challenging to calculate. To solve this problem, the following command filter is introduced

$$\begin{array}{c}\hfill {\dot{\widehat{\psi }}}_d=-l_2({\widehat{\psi }}_d-{\psi }_d)\end{array}$$

(30)

where $l_1$ is a positive constant. Thus, the filtered signal ${\dot{\widehat{\psi }}}_d$ is used to approximate ${\dot{\psi }}_d$. The approximate error is designed as ${\epsilon }_2={\dot{\widehat{\psi }}}_d-{\dot{\psi }}_d$. Then ${\alpha }_1$ is given by

$$\begin{array}{c}\hfill {\alpha }_1={\dot{\widehat{\psi }}}_d-k_3{z}_{\psi }\end{array}$$

(31)

where $k_3$ is a positive constant. Thus ${\dot{V}}_1$ is rewritten as

$$\begin{array}{c}\hfill {\dot{V}}_2=-k_3{z}_{\psi }^2+z_{\psi }(z_r+{\epsilon }_2)\end{array}$$

(32)

In order to design the control signal ${\tau }_z$, the Lyapunov function is given by

$$\begin{array}{c}\hfill V_3={\displaystyle \frac{1}{2}}{z}_r^2\end{array}$$

(33)

Taking the derivative of $V_3$, we have

$$\begin{array}{c}\hfill {\dot{V}}_3={\displaystyle \frac{z_r}{I_z-N_{\dot{r}}}}[(-X_{\dot{u}}+Y_{\dot{v}})vu+N_{r\left|r\right|}r\left|r\right|+N_{r}r+{\tau }_z]-z_r{\dot{\alpha }}_1\end{array}$$

(34)

Then, the heading angle controller is given by

$$\begin{array}{c}\hfill {\tau }_z=-k_4{z}_r-{\theta }_r^{\mathrm{T}}{h}_r\left(X_r\right)\end{array}$$

(35)

where $k_4$ is a positive constant, and ${\theta }_r^{\mathrm{T}}{h}_r\left(X_r\right)$ is the fuzzy logic system. ${\theta }_r$ is the weight vector and $h_r\left(X_r\right)$ is the basic vector with $X_r=[u,v,r,{\psi }_e]$.

Thus, from (34) and (35), we obtain

$$\begin{array}{c}\hfill {\dot{z}}_r={\displaystyle \frac{1}{I_z-N_{\dot{r}}}}\left[(-X_{\dot{u}}+Y_{\dot{v}})vu+N_{r\left|r\right|}r\left|r\right|+N_{r}r\right]-{\displaystyle \frac{1}{I_z-N_{\dot{r}}}}{k}_4{z}_r-{\displaystyle \frac{1}{I_z-N_{\dot{r}}}}{\theta }_r^{\mathrm{T}}{h}_r\left(X_r\right)-{\dot{\alpha }}_1\end{array}$$

(36)

Similarly, we introduce the following command filter

$$\begin{array}{c}\hfill {\dot{\widehat{z}}}_r=-l_3({\widehat{z}}_r-z_r)\end{array}$$

(37)

where $l_3$ is the positive constant and ${ϵ}_3={\dot{r}}_e-{\dot{\widehat{r}}}_e$ is the approximate error. Combined with (36), we can obtain

$$\begin{array}{cc}\hfill {\dot{\widehat{z}}}_r+k_5{z}_r& =F_r-{\displaystyle \frac{1}{I_z-N_{\dot{r}}}}{\theta }_r^{\mathrm{T}}{h}_r\left(X_r\right)\hfill \end{array}$$

(38)

where $k_5$ is a positive constant, $F_r={\displaystyle \frac{1}{I_z-N_{\dot{r}}}}\left[(-X_{\dot{u}}+Y_{\dot{v}})vu+N_{r\left|r\right|}r\left|r\right|+N_{r}r\right]-{\displaystyle \frac{1}{I_z-N_{\dot{r}}}}{k}_2{z}_1-{\dot{\alpha }}_1-{\epsilon }_2+k_5{z}_r$.

Similarly, based on the principle of convex optimization, the adaptive law is designed as

$$\begin{array}{c}\hfill {\dot{\theta }}_r={\eta }_r({\dot{\widehat{z}}}_r+k_5{z}_r)h_r\left(X_r\right)\end{array}$$

(39)

where ${\eta }_r$ is the learning rate. To avoid excessive increase in adaptive parameters, the learning rate is designed as follows

$$\begin{array}{c}\hfill {\eta }_r=\left\{\begin{array}{cc}0,\hfill & |-k_4{z}_r-{\theta }_r^{\mathrm{T}}{h}_r\left(X_r\right)|>a_r)\hfill \\ a_r,\hfill & \mathrm{others}\hfill \end{array}\right.\end{array}$$

(40)

where $a_r$ is a positive constant.

5. System Stability Analysis

In this section, the control performance of the heading angle under our strategy is analyzed based on the Lyapunov stability theorem. Consider the following Lyapunov function

$$\begin{array}{c}\hfill V={\displaystyle \frac{1}{2}}{z}_u^2+{\displaystyle \frac{1}{2}}{z}_{\psi }^2+{\displaystyle \frac{1}{2}}{z}_r^2\end{array}$$

(41)

Taking the derivative of V, we have

$$\begin{array}{cc}\hfill \dot{V}=& {\displaystyle \frac{z_u}{m-X_{\dot{u}}}}\left[(m-Y_{\dot{v}})vr+X_{u\left|u\right|}u\left|u\right|+X_{u}u+{\tau }_x\right]-z_u{\dot{u}}_d-k_3{\psi }_e^2+{\psi }_e(z_r+{\epsilon }_2)\hfill \\ \hfill & +{\displaystyle \frac{z_r}{I_z-N_{\dot{r}}}}\left[(-X_{\dot{u}}+Y_{\dot{v}})vu+N_{r\left|r\right|}r\left|r\right|+N_{r}r+{\tau }_z\right]-z_r{\dot{\alpha }}_1\hfill \\ \hfill =& {\displaystyle \frac{z_u}{m-X_{\dot{u}}}}\left[(m-Y_{\dot{v}})vr+X_{u\left|u\right|}u\left|u\right|+X_{u}u-k_1{z}_u-{\theta }_u^{\mathrm{T}}{h}_u\left(X_u\right)\right]-z_u{\dot{u}}_d-k_3{\psi }_e^2+{\psi }_e(z_r+{\epsilon }_2)\hfill \\ \hfill & -k_3{\psi }_e^2+{\psi }_e(z_r+{\epsilon }_2)+{\displaystyle \frac{z_r}{I_z-N_{\dot{r}}}}\left[(-X_{\dot{u}}+Y_{\dot{v}})vu+N_{r\left|r\right|}r\left|r\right|+N_{r}r-k_4{z}_r-{\theta }_r^{\mathrm{T}}{h}_r\left(X_r\right)\right]-z_r{\dot{\alpha }}_1\hfill \\ \hfill =& -k_2{z}_u^2-k_3{\psi }_e^2-k_5{z}_r^2+z_u(F_u+{\epsilon }_1-{\displaystyle \frac{{\theta }_u^{\mathrm{T}}{h}_u\left(X_u\right)}{m-X_{\dot{u}}}})+{\psi }_e(z_r+{\epsilon }_2)+z_r(F_r+{\epsilon }_3-{\displaystyle \frac{{\theta }_r^{\mathrm{T}}{h}_r\left(X_r\right)}{I_z-N_{\dot{r}}}})\hfill \end{array}$$

(42)

And then, the boundedness of the term $F_u-{\displaystyle \frac{{\theta }_u^{\mathrm{T}}{h}_u\left(X_u\right)}{m-X_{\dot{u}}}}$ and $F_r-{\displaystyle \frac{{\theta }_r^{\mathrm{T}}{h}_r\left(X_r\right)}{I_z-N_{\dot{r}}}}$ will be analyzed. For the convenience of analysis, define $m_u={\displaystyle \frac{1}{m-X_{\dot{u}}}}$ and $m_r={\displaystyle \frac{1}{I_z-N_{\dot{r}}}}$ For $i=u,r$, the following first-order condition of the convex function $J_i\left({\theta }_i\right)$ holds

$$\begin{array}{c}\hfill {\displaystyle \frac{\partial J_i\left({\theta }_i\right)}{\partial {\theta }_i}}{({\theta }_i-{\theta }_i^{*})}^{\mathrm{T}}\ge 0\end{array}$$

(43)

For $i=u,r$ and $j=2,5$, it can be concluded that

$$\begin{array}{cc}\hfill {\displaystyle \frac{\partial J_i\left({\theta }_i\right)}{\partial {\theta }_i}}& =-m_i(F_i-m_i{\theta }_i^{\mathrm{T}}{h}_i\left(X_i\right))h_i\left(X_i\right)\hfill \\ \hfill & =-m_i({\dot{\widehat{z}}}_i+k_j{z}_i)h_i\left(X_i\right)\hfill \end{array}$$

(44)

Therefore, the following can be obtained:

$$\begin{array}{c}\hfill m_i({\dot{\widehat{z}}}_i+k_j{z}_i)h_i\left(X_i\right){({\theta }_i-{\theta }_i^{*})}^{\mathrm{T}}\le 0\end{array}$$

(45)

For the positive definition function $U_i={\displaystyle \frac{1}{2}}{({\theta }_i-{\theta }_i^{*})}^{\mathrm{T}}({\theta }_i-{\theta }_i^{*})$, its derivative is derived as

$$\begin{array}{cc}\hfill {\dot{U}}_i& =({\theta }_i-{\theta }_i^{*}){\dot{\theta }}_i\hfill \\ \hfill & =({\theta }_i-{\theta }_i^{*}){\eta }_i({\dot{\widehat{z}}}_i+k_j{z}_i)h_i\left(X_i\right)\hfill \end{array}$$

(46)

Using (44), we have

$$\begin{array}{c}\hfill {\dot{U}}_i\le 0\end{array}$$

(47)

Thus, the boundedness of $({\theta }_i-{\theta }_i^{*})$ is proven, which illustrates that the fuzzy logic system is able to approximate the uncertain function $F_i$. So, $F_u-{\displaystyle \frac{{\theta }_u^{\mathrm{T}}{h}_u\left(X_u\right)}{m-X_{\dot{u}}}}={\delta }_1$ and $F_r-{\displaystyle \frac{1}{I_z-N_{\dot{r}}}}{\theta }^{\mathrm{T}}h\left(X\right)={\delta }_2$, where ${\delta }_1$ and ${\delta }_2$ are bounded normal numbers. According to Lemma 2 and (42), $\dot{V}$ is rewritten as

$$\begin{array}{cc}\hfill \dot{V}& =-k_2{z}_u^2-k_3{z}_{\psi }^2-k_5{z}_r^2+z_u({\delta }_1+{\epsilon }_1)+z_{\psi }(z_r+{\epsilon }_2)+z_r({\delta }_2+{\epsilon }_3)\hfill \\ \hfill & \le -(k_2-1)z_u^2-(k_3-1)z_{\psi }^2-(k_5-{\displaystyle \frac{3}{2}})z_r^2+{\displaystyle \frac{1}{2}}{\epsilon }_1^2+{\displaystyle \frac{1}{2}}{\epsilon }_2^2+{\displaystyle \frac{1}{2}}{\epsilon }_3^2+{\displaystyle \frac{1}{2}}{\delta }_1^2+{\displaystyle \frac{1}{2}}{\delta }_2^2\hfill \\ \hfill & \le -aV+b\hfill \end{array}$$

(48)

In (48), $a=min\{2k_2-2,2k_3-1,2k_5-3\}$, $b={\displaystyle \frac{1}{2}}{\epsilon }_1^2+{\displaystyle \frac{1}{2}}{\epsilon }_2^2+{\displaystyle \frac{1}{2}}{\epsilon }_3^2+{\displaystyle \frac{1}{2}}{\delta }_1^2+{\displaystyle \frac{1}{2}}{\delta }_2^2$. In order to ensure the positive definiteness of a, the control parameters need to meet the following conditions: $k_2>1,k_3>1,k_5>{\displaystyle \frac{3}{2}}$. Thus, one can obtain

$$\begin{array}{c}\hfill V\left(t\right)\le {\displaystyle \frac{b}{a}}+\left(V\left(0\right)-{\displaystyle \frac{b}{a}}\right)e^{-at},t\ge 0\end{array}$$

(49)

According to (49), $V\left(t\right)$ is bounded by $li{m}_{t\to +\infty }V={\displaystyle \frac{b}{a}}$. Therefore, all the error variables in the system are ultimately bounded.

Remark 1. 

It is important to note that in this article, human actions do not directly control the USVs’ movements, specifically the torque. Instead, human control is achieved by adjusting the desired heading angle of the USVs. This approach aligns more closely with human operational habits compared to existing methods [32]. Additionally, we implement a LOS navigation strategy based on the potential field method, which helps mitigate potential safety risks associated with human actions.

Remark 2. 

The formula presented introduces an adaptive learning strategy that is based on input saturation. Under this control strategy, if the control torque exceeds a specified saturation value, our adaptive method ceases training the fuzzy system. This strategy effectively minimizes the negative impact of excessive control inputs on performance, in contrast to what is found in the existing literature [41,42]. Furthermore, we develop the adaptive law for the fuzzy system using convex optimization rather than the Lyapunov method, which reduces the coupling within the entire controller. Compared to other adaptive intelligent control strategies [43,44,45], the separate design approach outlined in this paper simplifies the controller’s complexity and facilitates easier parameter tuning.

6. Method Validation and Analysis

In this section, we conduct simulation experiments to verify the feasibility of the proposed adaptive fuzzy control strategy. The USV model chosen for this test is based on the work of [46]. The model parameters are shown in

Table 1. Model parameters of USVs.

Parameter	Value	Unit	Parameter	Value	Unit
m	23.8000	kg	$Y_v$	$-0.8612$	kg/s
$I_z$	1.7600	kg·m2	$Y_{\left|v\right|v}$	$-36.2823$	kg/m
$x_g$	0.0460	m	$Y_r$	0.1079	kg·m/s
$X_u$	$-0.7225$	kg/s	$N_v$	0.1052	kg·m/s
$X_{\left|u\right|u}$	$-1.3274$	kg/m	$N_{\left|v\right|v}$	5.0437	kg·m
$X_{uuuu}$	$-5.8664$	kg/m3	$X_{\dot{u}}$	$-2.0$	kg
$Y_{\dot{v}}$	$-10.0$	kg	$Y_{\dot{r}}$	0.0	kg·m
$N_{\dot{v}}$	0.0	kg·m	$N_{\dot{r}}$	$-1.0$	kg·m2

. The expected speed of the USV is set to 0.5 m/s, with an initial position of (1, −1) and an initial speed of 0. The waypoints for the reference path are set at (0, 0) and (80, 80). We have designated a blue danger zone with a radius of 5 m, centered around the coordinates (28, 50), and a circular green pollution zone that extends 5 m beyond the danger zone. The fuzzy system nodes for both the velocity and heading angle subsystems consist of 11 nodes, with the center points of the Gaussian functions evenly distributed within the range of $[-3,3]$ and a width of 0.5. The initial fuzzy weights are all 0. The control parameters are $k_1=50$, $k_2=4$, $k_3=10$, $k_4=10$, $k_5=30$, $l_1=10$, $l_2=10$, $l_3=0.1$, ${\eta }_u=2$, ${\eta }_r=20$, $k_{ap}=1$, $k_{rp}=1$, $a_u=50$, $a_r=50$.

To validate the performance of our algorithm, we conduct simulation experiments across various scenarios. Firstly, we present the performance curve of the unmanned ship control system with the participation of human intelligence The validation results are illustrated in Figure 4, Figure 5, Figure 6, Figure 7, Figure 8 and Figure 9. Figure 4 displays the global path diagram, while Figure 5 and Figure 6 present the dynamic curves for the heading angle and surge velocity, respectively. Figure 7 shows the control input curve of the USVs and Figure 8 and Figure 9 depict the fuzzy weight curves for the velocity and heading angle subsystems. As illustrated in Figure 4, human intervention occurs at 75 s to enable the USVs to enter the contaminated area for environmental monitoring. At this point, there is a significant shift in the expected heading angle, prompting the controller to quickly adjust and guide the USVs to track the desired heading angle. Figure 5 and Figure 6 demonstrate that effective tracking of both speed and angle is still maintained following human intervention. As shown in Figure 5, when human intervention occurs at t = 75 s, the heading angle controller exhibits excellent tracking performance. Quantitative analysis shows that the rise time of the system is 2.1 s, the adjustment time is 4.5 s, and the overshoot is only 3.8%. At about 108 s, the USVs enter the contaminated area and detect obstacles. Thanks to the APF algorithm, the USV is able to navigate around these obstacles autonomously, ensuring the safe continuation of the detection task without human intervention. After exiting the contaminated area, the USVs resume their original path without further human interference. During the obstacle avoidance process, Figure 8 and Figure 9 illustrate that the adaptive fuzzy strategy continuously learns to adapt to changing angles. Our adaptive law only relies on the system information at the current moment; therefore, it has the advantage of low computational complexity. On a PC equipped with an i5-8500 processor (Lenovo Group Co., Ltd., Beijing, China), the running time of our controller in MATLAB (version R2023b) is less than 0.01 s. Additionally, it is observed in Figure 7 and Figure 9 that the adaptive strategy ceased updating at both 52 s and 152 s. This occurs because our proposed adaptive strategy effectively prevents excessive parameter growth, which helps mitigate the negative effects of overly adaptive parameters on the system under the human-in-the-loop control strategy.

To further analyze the performance of the controller during obstacle avoidance, we select two critical moments in the obstacle avoidance process for detailed examination. In Figure 10, we observe that as the USV enters the avoidance radius of the polluted area, the obstacle avoidance maneuver is automatically initiated through the APF algorithm. The sudden change in the heading angle command results in a smooth but significant adjustment in the USV’s trajectory, demonstrating the rapid response capability of our control system. In Figure 11, we can see that when the USV has successfully navigated around the core hazardous zone, it begins to return toward the original desired path while maintaining a safe distance from the polluted area. These two figures collectively illustrate that the guidance algorithm has successfully executed the obstacle avoidance function, while the control algorithm effectively tracks the abrupt angle changes that occur during this process, thereby verifying the effectiveness of our proposed APF-based navigation strategy.

Under the same control parameters, we simulate the tracking of the expected path without human intervention. The experimental results are presented in Figure 12, Figure 13, Figure 14, Figure 15, Figure 16 and Figure 17. Figure 12 illustrates the tracking path of the unmanned surface vehicles, demonstrating their effective tracking of the expected route. Figure 13 and Figure 14 depict the tracking of the heading angle and surge velocity. Notably, there are significant tracking errors during the initial stage. However, as adaptive parameters are trained, the tracking error decreases rapidly. Figure 15 shows the curve of the control input signal. Meanwhile, Figure 16 and Figure 17 illustrate the changes in fuzzy weights. It is evident that as the tracking error diminishes, both the velocity weight and heading angle weight remain within a specific range. By comparing the two results above, it is clear that human intelligence can enhance the performance of unmanned ships in functions like ocean environment monitoring. Additionally, our design approach, which separates navigation from control, effectively minimizes the impact of human actions on the stability of these unmanned vessels. The verification results demonstrate that the control strategy proposed in this paper ensures the stability of unmanned ships, whether human actions are introduced or removed.

To demonstrate the advantages of our control strategy, we compare our controller with the traditional adaptive fuzzy control strategy in reference [47]. The control parameters used in reference [47] are the same as those in our controller. The comparison results are shown in Figure 18, Figure 19 and Figure 20, and the system performance metrics are shown in

Table 2. Comparison of tracking performance between two strategies.

Indexes	Proposed Method	Comparison Method
MAE ($u_e$)	$4.1\times {10}^{-5}$	$1.8\times {10}^{-3}$
MAE (${\psi }_e$)	$1.1\times {10}^{-5}$	$4.4\times {10}^{-4}$

. Our method outperforms the compared methods in both speed control and angle control. For speed control, the value of MAE in our controller is only $4.1\times {10}^{-5}$, while the one in the comparison method is $1.8\times {10}^{-3}$. In the angle control subsystem, our proposed method reduces the value of MAE from $4.4\times {10}^{-4}$ to $1.1\times {10}^{-5}$ when compared to traditional methods.

To comprehensively evaluate the performance of the proposed control strategy,

Table 3. Comparison Performance Benchmark Table of Control Methods.

Control Strategy	Model Dependency	Environments Adaptability	Obstacle Avoidance	Computational Complexity
Our Method	Low	High	High	Low
Model Predictive Control [33]	High	Low	Low	High
HiTL Continuous Twisting Control [32]	Medium	High	Low	Medium
Adaptive Fuzzy Control [47]	Low	Medium	Low	Medium

compares and analyzes this method with other mainstream control strategies from four key dimensions. From Table 3, it can be seen that this comparison highlights the good balance achieved by our method between model independence, environmental adaptability, safety, and real-time performance, verifying its practical value and comprehensive advantages in complex marine environment monitoring tasks.

7. Conclusions

A new type of adaptive fuzzy control strategy based on human-in-the-loop is proposed to solve the navigation and control problems of USVs for environmental monitoring in complex sea conditions. An intelligent control strategy based on convex optimization is proposed to solve uncertain dynamic problems in USVs, and the potential field method is introduced into the HiTL control strategy to ensure the safe operation of USVs. The verification results indicate that with the help of human intelligence, the proposed control strategy can effectively complete the monitoring of marine pollution and overcome the impact of uncertain dynamic problems on control performance. It is important to note that this article did not address the issues of ocean pollutant movement and communication delays, which could result in potential performance degradation. In the future, we aim to develop an HiTL control framework that is resilient to communication delays in order to tackle the obstacle avoidance control problem faced by unmanned ships when encountering moving obstacles.