部队, 辽宁 大连 116023
收稿:2024-08-28,
网络出版:2025-05-07,
纸质出版:2025-05-31
移动端阅览
张旭. 基于声学测量的水下高动态航行参数估计[J]. 兵工学报, 2025,46(5):240741.
Xu ZHANG. Motion Parameter Estimation of High Dynamic Underwater Vehicle Based on Acoustic Measurement[J]. Acta Armamentarii, 2025, 46(5): 240741.
张旭. 基于声学测量的水下高动态航行参数估计[J]. 兵工学报, 2025,46(5):240741. DOI: 10.12382/bgxb.2024.0741.
Xu ZHANG. Motion Parameter Estimation of High Dynamic Underwater Vehicle Based on Acoustic Measurement[J]. Acta Armamentarii, 2025, 46(5): 240741. DOI: 10.12382/bgxb.2024.0741.
针对水下高动态航行体运动特征难以识别的问题
提出一种基于水声测量的运动参数序列估计方法。该方法通过逐点解算得到位置、速度序列
再进行函数化重构和参数辨识
消除随机误差引起的数据抖动
实现平稳、连续的序贯参数获取。在仿真分析中
模拟了边长为数百米的海底四元阵对数十米深度垂向航行过程的测量
参数估计结果的垂向精度相对于逐点解算结果明显提升
位置和速度均方根误差(Root Mean Square Error
RMSE)分别减小27.8%和47.2%。经大样本计算
参数序列估计值趋近于真值
垂向位置和速度偏差分别为0.042m和0.056m/s。水池试验结果表明
物理模型的高动态航行参数估计结果与惯性传感器数据相吻合
垂向位置和速度RMSE分别为0.024m和0.141m/s。新方法可为水下高动态航行体运动性能检验提供准确、平滑、连续的参数估计结果
在海上测试中有一定工程应用前景。
A motion parameter estimation method based on acoustic measurement is proposed for identifying the kinetic characteristics of high dynamic underwater vehicle. In the proposed method
the position and velocity data series are obtained by point-by-point solution
and then the data jitters caused by random errors are removed by functional reconstruction and coefficient identification
so a smooth and continuous parameter sequence is obtained. In simulation
the high dynamic underwater vehicle moves from the depth of several tens of meters to surface
and the motion parameter is measured by the seabed four-receiver array. The simulated results show that the estimated parameter sequence has higher accuracy in vertical direction than the point-by-point solved one
and the root mean square errors (RMSE) of position and velocity are reduced by 27.8% and 47.2%
respectively. Calculations based on large samples indicate that the estimated parameter sequence approaches the true value
and the deviations of position and velocity are 0.042m and 0.056m/s
respectively. The water-tank test results show that the estimated parameter sequence generated by the high dynamic physical model is well consistent with the inertial sensor data
and the RMSEs of position and velocity in vertical direction are 0.024m and 0.141m/s
respectively. The proposed method can provide an accurate
smooth and continuous parameter sequence for the high dynamic underwater vehicle in performance testing and has certain engineering application value in sea trials.
LU J X , WANG C , SONG W C , et al. Experimental investigation on interference characteristics of projectiles launched successively underwater [J ] . Ocean Engineering , 2022 , 250 : 110824 .
施瑶 , 任锦毅 , 高山 , 等 . 航行体水下连续发射尾涡遭遇与运动干扰特性 [J ] . 兵工学报 , 2023 , 44 ( 10 ): 3195 - 3203 . DOI: 10.12382/bgxb.2022.0616 http://doi.org/10.12382/bgxb.2022.0616 为研究不同发射时间间隔下航行体水下连续发射尾涡干扰与弹道特性,基于Realizable k-ε湍流模型和能量方程、流体体积方法和重叠网格技术,开展数值方法和网格无关性验证,数值模拟结果与实验测试结果吻合度较好。建立航行体水下连续发射数值模拟方法,研究航行体尾流区涡结构的演变机理、次发航行体表面压力分布、弹道以及俯仰姿态演变规律。研究结果表明:航行体水下连续发射过程中在其尾流中发现了发卡涡形态的流动结构,该涡结构由涡头与两条涡腿组成,通常以多个共同组合的形式存在于航行体尾部的流场区域中;沿涡腿内侧发生喷射事件,沿涡腿外侧发生扫掠事件,同时在涡结构内部形成一定流向尺度的低速条带区域;在横流效应下,当次发航行体表面穿过尾流中涡结构中的低速条带区时,迎背流面压力分布特性得到较大的改善,增加了弹道姿态稳定性。
SHI Y , REN J Y , GAO S , et al. A study on the wake vortex encounter and movement interference characteristics of projectiles successively launched underwater [J ] . Acta Armamentarii , 2023 , 44 ( 10 ): 3195 - 3203 . (in Chinese) DOI: 10.12382/bgxb.2022.0616 http://doi.org/10.12382/bgxb.2022.0616 In order to study the wake vortex interference and trajectory characteristics of projectiles launc hed successively underwater at different launching time intervals, based on the Realizable k-ε turbulence model and energy equation, volume of fluid (VOF) and overlapping grid technology were adopted. Firstly, verification of numerical method and validation of grid independence were presented. The numerical simulation results were in good agreement with the experimental results. Then the numerical simulation method of projectiles launched successively underwater was established. Based on these, the pressure distribution on the side facing the inflow as well as on the backside, trajectory and pitch attitude, particularly the evolution mechanism of vortex in wake flow were studied. The results showed that hairpin vortex-like flow structure was found, multiple hairpin vortex-like flow structures usually exist in a combined form in the flow field region at the tail of the vehicle. The jet event occurred along the inner side of the vortex leg, and the sweep event occurred outside the vortex leg. Meantime, along the inside of the vortex, a low-speed band with a certain streamwise scale was formed. Under the transverse-flow effect, when the surface of the secondary projectile passed through the low-speed strip region of the vortex in the wake, the pressure distribution characteristics of the flow facing side and its opposite side were greatly improved, the stability of trajectory and pitch attitude was increased.
刘方 , 肖金石 , 韦建明 , 等 . 水下连续发射弹体干扰特性及发射时序优化 [J ] . 兵工学报 , 2024 , 45 ( 1 ): 197 - 205 . DOI: 10.12382/bgxb.2022.0576 http://doi.org/10.12382/bgxb.2022.0576 随着对饱和攻击需求的提高,潜艇连续发射过程的发射时序协调控制研究变得迫切而紧要。考虑到弹体间的流体动力干扰是影响安全发射的主要因素,基于重叠网格多自由度仿真技术,针对连续发射的水下弹体开展姿态弹道干扰特性研究。通过分析流场结构发现,以一定攻角发射的弹体形成的发卡形尾涡是造成后续弹体姿态弹道差异的主要原因。根据不同艇速、时间间隔和空间间隔下弹体间的干扰特性建立干扰评价模型。在保证干扰不影响后续弹体的前提下,以最短发射时长为目标,以综合评价函数为约束,基于改进的贪心算法对大筒多弹式布局的水下弹体开展发射时序优化研究,并采用均匀抽样方法验证优化结果准确性。研究结果表明:相对于均匀抽样方法,改进的贪心算法具有相当的计算准确度和更高的计算效率。
LIU F , XIAO J S , WEI J M , et al. Interference characteristics and launch sequence optimization of projectiles launched successively underwater [J ] . Acta Armamentarii , 2024 , 45 ( 1 ): 197 - 205 . (in Chinese) DOI: 10.12382/bgxb.2022.0576 http://doi.org/10.12382/bgxb.2022.0576 With the increasing demand for saturation attacks, the research on the optimization of launch sequence of projectiles launched successively underwater has become important and urgent. Considering that the hydrodynamic interferences between two underwater projectiles are the main factor affecting launch safety, this paper studies the interference characteristics of projectiles launched successively underwater based on the overlapping mesh methods. By analyzing the flow field, it is found that the hairpin vortices formed by the projectile with an angle of attack are the main reason leading to the attitude difference between two projectiles. An interference evaluation model is established according to the interference between the projectiles under the conditions of different transport speeds, time intervals and space intervals. To ensure that the former projectile interferes little with subsequent projectiles, the launch sequence of projectiles fixed at a launch tube is optimized based on the improved greedy algorithm, in which the shortest launch duration is taken as the goal and the comprehensive evaluation function as the constraint. The uniform sampling method is used to verify the accuracy of the optimized results. The results show that the improved greedy algorithm has comparable accuracy and higher efficiency compared with the uniform sampling method.
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YANG X G , DANG J J , WANG P , et al. The influence of waves on the impact load during high-speed water-entry of a vehicle [J ] . Acta Armamentarii , 2022 , 43 ( 2 ): 355 - 362 . (in Chinese) DOI: 10.3969/j.issn.1000-1093.2022.02.013 http://doi.org/10.3969/j.issn.1000-1093.2022.02.013 The load characteristics of a vehicle entering into water at high-speed under wave conditions are key factors influencing the overall plan and structural design of vehicle. VOF multiphase flow model and dynamic grid technology are used to establish a numerical simulation method of high-speed water-entry, and the accuracy and applicability of the simulation method are verified by experiments. The influences of water entry angle and wave parameters on the axial impact load during high-speed water-entry events are numerically studied. The results show that the peak axial impact force coefficient increases with an increase in the water-entry angle, and has a linear relationship with the tangent function of water-entry angle. The different wave phases change the actual angle between the vehicle and the water surface at the water-entry moment. When entering into the water at 90° or 270° wave phase angle, there is little difference between the axial impact load and that in static water environment; when entering into the water at 0° wave phase angle, the peak value of axial impact load is the largest, and it is basically the same as the axial impact load at the corresponding water-entry angle on static water surface; when entering into the water at 180°wave phase angle, the axial impact load is the smallest, but it is prone to ‘jump’ and cause failure in the water-entry. The actual water-entry angle should be the coupling value of the wave inclination and the vehicle attitude at the entry point under wave conditions, the peak axial impact force coefficient can be obtained by interpolating the peak coefficient curve of impact load in static water environment.
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JIA T Y , GAO J J , SHEN X H , et al. Moving underwater vehicle localization with uncertain sound speed [J ] . Systems Engineering and Electronics , 2022 , 44 ( 9 ): 2699 - 2706 . (in Chinese) DOI: 10.12305/j.issn.1001-506X.2022.09.01 http://doi.org/10.12305/j.issn.1001-506X.2022.09.01 The traditional localization of vehicle using an underwater acoustic positioning system has two problems. One is the motion of the vehicle during observation period is ignored, and the other is that the uncertainty of underwater sound speed is not taken into account. A time measurement model for localization is constructed for the vehicle in motion, and the uncertainty of sound velocity is modeled to solve the above problems. A localization method for the moving vehicle is derived based on weighted least squares estimator, and a sound speed update method based on maximum likelihood estimator is proposed as well. Apart from estimating the vehicle position, the proposed model and the time mesurement are able to update the sound speed. The simulation results verify that the proposed methods outperform the existing methods for various parameter settings and achieve Cramer-Rao lower bound (CRLB) when the time measurement noise is not large. Moreover, the performance of the sound speed update is significantly improved when the time error is not large.
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张瑜 , 吴凯 , 郭杰 , 等 . 基于数据质量评估的自适应序贯航迹关联算法 [J ] . 系统工程与电子技术 , 2022 , 44 ( 11 ): 3477 - 3485 . DOI: 10.12305/j.issn.1001-506X.2022.11.23 http://doi.org/10.12305/j.issn.1001-506X.2022.11.23 针对传感器精度下降时的航迹关联问题, 提出了一种基于数据质量评估的自适应序贯航迹关联算法。将实时数据质量评估结果引入关联门限的调整, 结合熵值法和效用函数法对传感器性能和局部滤波质量两项指标分别进行评估, 构建了两项指标与算法显著性水平之间的模糊关系, 实现关联门限的自适应调整。仿真表明, 在局部传感器精度下降的场景下, 改进算法的关联性能优于对比算法, 且良好的关联效果有益于融合精度的提升, 在目标机动的情况下也具有良好的适应性。
ZHANG Y , WU K , GUO J , et al. Adaptive sequential track-association algorithm based on data quality assessment [J ] . Systems Engineering and Electronics , 2022 , 44 ( 11 ): 3477 - 3485 . (in Chinese) DOI: 10.12305/j.issn.1001-506X.2022.11.23 http://doi.org/10.12305/j.issn.1001-506X.2022.11.23 In order to solve the track-association problem when sensor suffers declined accuracy, an adaptive sequential track-association algorithm based on data quality assessment is proposed. Real-time data quality evaluation results are introduced into the adjustment of correlation threshold. The entropy method and the utility function method are combined to evaluate the performance of sensor and the quality of filtering, and the fuzzy control relationship between two indexes and the significance level is constructed, so as to realize the adaptive adjustment of correlation threshold. The simulation results show that the performance of the improved algorithm is better than that of compared algorithm in the situation of declined sensor accuracy, and the good correlation effect is beneficial to the improvement of fusion accuracy.It also has good adaptability in the case of maneuver target tracking.
CUI Y Q , LIU Y , TANG T T , et al. A new adaptive track correlation method for multiple scenarios [J ] . IET Radar, Sonar & Navigation , 2021 , 15 ( 9 ): 1112 - 1124 .
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