Numerical Research on Hull–Propeller–Rudder–Ice Interaction of Full-Scale Polar Transport Ship in Brash Ice Channel by Jinlong Zhang, Jianing Zhang, Lei Zhang, Weimin Chen, Qingshan Zhang

“…The interactions between the full-scale polar transport ship, propeller, rudder, and brash ice are effectively simulated. First, the hydrodynamic performance of an open-water propeller is tested, and it is found that the numerical errors of efficiency and the experimental result are less than 8%. …”
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Modeling and Analysis of Actuators in Multi-Pump Waterjet Propulsion Systems by Shuli Jia, Yinuo Guo, Yuxue Liu, Dali Wei, Chong Qu, Liyong Ma

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Experimental dataset of a model-scale ship in calm water and wavesUniversity of Southampton Institutional Repository by Saeed Hosseinzadeh, Stephen Turnock, Haesol Lee, Rodolfo Olvera

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Fault-Tolerant Model Predictive Control for Autonomous Underwater Vehicles Considering Unknown Disturbances by Yimin Chen, Shaowen Hao, Jian Gao, Jiarun Wang, Le Li

“…This paper presents a fault-tolerant model predictive control approach for cross-rudder autonomous underwater vehicles to achieve heading control, considering rudder stuck faults and unknown disturbances. …”
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Chattering-Free Sliding-Mode Control for Electromechanical Actuator with Backlash Nonlinearity by Dongqi Ma, Hui Lin, Bingqiang Li

“…Considering the backlash nonlinearity and parameter time-varying characteristics in electromechanical actuators, a chattering-free sliding-mode control strategy is proposed in this paper to regulate the rudder angle and suppress unknown external disturbances. …”
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Experimental Study on the Nonlinear Behavior of a Sailing Container Ship under Landslide-Induced Surges by Pei-yin Yuan, Ping-yi Wang, Yu Zhao, Mei-li Wang

“…In this study, twenty groups of orthogonal experiments of landslide-induced impulse wave were conducted, the details of the self-propulsion of ships were designed, the values of the propeller, rudder, and shafting were calculated, and the model of the propeller and rudder was processed. …”
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UNFOLDING PERFORMANCE OF FOLDING WING FOR ACTUATOR AND EXPERIMENT by LIU DuanChen, HAN XueFeng, ZHANG Yue, ZHANG MingYue, LIU XiaoDong

“…Then,related dates such as deployable time,impact and stress of the rudder slice were obtained by rigid-flexible coupling dynamics imitating analysis of the spreading process through MSC. …”
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AIRCRAFT SPOILER SUSPENSION STIFFNESS TEST AND ANALYSIS (MT) by GAO Jie, LI Chao

“…During the stiffness characteristic test, it was found that the monitoring data of the spoiler structure showed a jumping trend which was not consistent with the conventional rudder surface test and the theoretical expectation. …”
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Novel Model for Manoeuvrability of Ships Advancing in Landslide-Generated Tsunamis by Peiyin Yuan, Pingyi Wang, Yu Zhao

“…The correlations between the maximum roll angle and the navigation position, sailing speed, and rudder angle were investigated in detail. A safety risk response theory of navigation in the area of landslide-generated tsunamis was proposed, and a scientific basis was provided for the safe navigation of ships in the Three Gorges Reservoir area.…”
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Command Filter AILC for Finite Time Accurate Tracking of Aircraft Track Angle System Based on Fuzzy Logic by Chunli Zhang, Xu Tian, Yangjie Gao, Fucai Qian

“…In this paper, the longitudinal model of an uncertain aircraft is taken as the research object, and the aircraft path inclination is controlled by controlling the input rudder deflection angle. An adaptive iterative learning control (AILC) scheme is proposed to solve the accurate tracking control problem of the flight path inclination on a finite time interval. …”
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Ground Motion Modeling and Adaptive Joint Control for Large-Scale UAVs by Bo Wang, Wensheng Wang, Xiaodan Cui, Xiaoxiong Liu

“…Aiming at the problem of lateral deviation of large-scale long-endurance solar-powered UAVs relative to the runway during takeoff or landing, a UAV ground motion control structure based on the combination of engine differential and rudder was proposed. According to the structural characteristics of large-scale long-endurance solar-powered UAVs, a ground motion model of a three-point layout UAV including landing gear was established, and the ground rolling dynamics and modal characteristics were analyzed. …”
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Parameter Identification of an Unmanned Surface Vessel Nomoto Model Based on an Improved Extended Kalman Filter by Sihang Lu, Baolin Wang, Zaopeng Dong, Zhihao Hu, Yilun Ding, Wangsheng Liu

“…These parameters are incorporated into the Nomoto model, and simulations are conducted by inputting the same rudder inputs as in the experimental data. The predicted heading angle and yaw rate are compared with experimental results, showing that the mean absolute error (MAE) for the heading angle is within 10° and the MAE for the yaw rate is within 1.5°/s. …”
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Construction and application of a physically-based constitutive model for superplastic deformation of near-α TNW700 titanium alloy by Lixia Ma, Dingyong He, Bangjian Yang, Xiuquan Han, Jichun Zhang, Weidong Li

“…The TNW700 alloy is designed for short-term service up to 700 °C to meet the high-temperature titanium alloy requirements for complex thin-walled cabin and rudder/wing components in high Mach aircraft. This study aims to develop a high-precision, physically-based unified viscoplastic constitutive model to predict superplastic deformation and microstructure evolution of TNW700 alloy conical components under complex loading. …”
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Experimental Study of H-Shaped Honeycombed Stub Columns with Rectangular Concrete-Filled Steel Tube Flanges Subjected to Axial Load by Jing Ji, Maomao Yang, Zhichao Xu, Liangqin Jiang, Huayu Song

“…The results showed that rudder slip diagonal lines occur on the steel tube outer surface and the concrete-filled steel tube flanges of all specimens exhibit shear failure. …”
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Integrated Guidance and Control of Interceptor Missile Based on Asymmetric Barrier Lyapunov Function by Xiang Liu, Xiaogeng Liang

“…Finally, in light of redundancy in such actuators as aerodynamic rudders and jet devices, a dynamic control allocation algorithm is designed to assign the desired control moments to the actuators. …”
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