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为减小舰船匀转向情况下电罗经的航向误差,提高电罗经指向精度,在分析某型罗经实测数据基础上,利用最小二乘法建立其误差模型,并对模型参数进行了估计。实践表明,该方法用于电罗经航向误差补偿效果较好。 相似文献
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介绍了一种在动态环境下对特定目标进行跟踪来反推舰船航向真值的测量方法-目标真值测量法。该方法采用了动态条件下高精度连续测量技术、数据融合处理技术和动态测量精度分配技术,实现了动态条件下舰船航向真值的高精度连续测量。 相似文献
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《舰船科学技术》2020,(4)
在错综复杂的水路巷道中,舰船需要通过航向通道系统的计算,来完成对舰船航向路径的规划选定。其中,海量数据在综合计算过程中会出现信号间的相互抑制,抑制信号会转化为判定误差,造成舰船航向通道控制出现偏差。为解决上述问题,提出基于嵌入式技术的舰船航向通道自动控制系统。通过嵌入式技术,组建前端数据独立计算平台,通过数据处理硬件对多项数据进行分离计算。通过设计融合策略对独立计算后的数据进行融合分析计算,最后,通过非线性控制算法对通道数据进行自动分析判定,实现自适应的自动控制效果。通过设计仿真场景对设计系统进行数据模拟测试,并对测试数据进行对比分析得出可行性结论。 相似文献
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《舰船科学技术》2015,(12):117-122
载波相位GPS测姿实施中,其姿态解算是核心技术之一,目前有多种姿态解算算法,其中对于单基线姿态测量,直接算法因具有原理简单、计算速度快、实时性好等特点被广泛应用。但在舰船测姿实施中,对姿态角的测量会产生一定的误差。采用直接算法在解算中没有对粗大误差和GPS信号缺失进行处理,使得解算结果误差较大。因此提出一种改进的舰船姿态解算算法即基于自适应卡尔曼滤波的姿态解算算法。建立航向角和纵摇角的解算模型,从理论上推导了基线越长,航向角测量精度越高;航向角的解算精度比纵摇角的解算精度高;基于自适应卡尔曼滤波的姿态解算算法的解算精度比直接法的解算精度高。通过仿真实验,对上述推理进行验证,航向角的解算精度比纵摇角的结算精度高出一个数量级;改进算法的解算精度比直接算法的解算精度高出一个数量级。 相似文献
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该文从几何精度系数出发给出了导航定位误差的一般分析方法,从而得出导航定位误差的简单估计和分析所造物标的最佳配置。 相似文献
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统计能量分析方法能够有效预示舰船和车辆等结构的高频振动及噪声。本文通过建立两子结构耦合模型,利用差分法研究了瞬态统计能量分析中参数误差对子结构响应能量的影响,同时给出了参数误差与所导致能量误差的关系函数。结果表明:对于外载荷直接激励的子结构,内损耗因子和耦合损耗因子的误差都会导致被预示总能量的减小。对于外载荷间接激励的子结构,内损耗因子的误差会导致峰值能量的减小,而耦合损耗因子的误差会导致峰值能量的增加。本文内容对改进动力学系统数值模型以及提高结构振动和噪声预示精度有一定的帮助。 相似文献
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舰用高精度激光陀螺惯导内杆臂误差分析及补偿方法研究 总被引:1,自引:0,他引:1
对于高精度激光陀螺旋转惯导系统,大部分惯性器件误差都能够通过惯性测量单元( IMU)旋转而调制掉,内杆臂误差不仅不能够被调制掉,反而因为 IMU旋转将误差引入到系统对准和导航过程中。基于此,本文对内杆臂误差进行分析与建模,推导内杆臂误差与导航速度误差之间的数学表达式,通过分析确定内杆臂长度和振动频率是影响内杆臂误差的2个因素,并提出基于内杆臂长度的误差补偿方法。最后,通过试验对内杆臂误差模型和补偿方法进行了验证。 相似文献
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通过分析和推导船用天文测姿系统的各项误差源,建立各项误差与测量误差之间的数学模型,为航姿测量误差的定量计算提供理论基础,并对系统测量误差进行计算,绘制相应的影响曲线. 相似文献
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This article presents a study on the accuracy of the numerical determination of the friction and pressure resistance coefficients
of ship hulls. The investigation was carried out for the KVLCC2 tanker at model- and full-scale Reynolds numbers. Gravity
waves were neglected, i.e., we adopted the so-called double-model flow. Single-block grids with H–O topology were adopted
for all the calculations. Three eddy viscosity models were employed: the one-equation eddy viscosity and the two-equation
models proposed by Menter and the TNT version of the two-equation k-ω model. Verification exercises were performed in sets of nearly geometrically similar grids with different densities in the
streamwise, normal, and girthwise directions. The friction and pressure resistance coefficients were calculated for different
levels of the iterative error and for computational domains of different size. The results show that on the level of grid
refinement used, it is possible to calculate the viscous resistance coefficients in H–O grids that do not match the ship contour
with a numerical uncertainty of less than 1%. The differences between the predictions of different turbulence models were
larger than the numerical uncertainty; however, these differences tended to decrease with increases in the Reynolds number.
The pressure resistance was remarkably sensitive to domain size and far-field boundary conditions. Either a large domain or
the application of a viscous–inviscid interaction procedure is needed for reliable results.
This work was presented in part at the International Conference on Computational Methods in Marine Engineering—MARINE 2007,
Barcelona, June 3–4, 2007. 相似文献
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系统观测目标误差渗透着系统误差和随机误差,系统误差和随机误差的分离与溯源理论和应用一直是误差分析的难点和热点。文中基于系统误差和随机误差的互相关系与传递特征,提出了以传递函数为基础的误差传递模型,并基于该模型,将复杂系统划分为若干个子系统,分析了各子系统在观测目标误差中的主次作用( primary and secondary position a-nalysis,PSPA)。算例表明,该理论能够分析得出引起观测误差灵敏度较高的子系统,这对于误差溯源、分析和控制误差,提高观测目标的精度具有一定的指导意义。 相似文献
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This paper presents a study on the numerical calculation of the friction resistance coefficient of an infinitely thin plate
as a function of the Reynolds number. Seven eddy-viscosity models have been selected: the one-equation turbulence models of
Menter and Spalart–Allmaras; the k-ω two-equation model proposed by Wilcox and its TNT, BSL and SST variants and the two-equation model. The flow has been computed at 14 Reynolds numbers in sets of seven geometrically similar Cartesian grids
to allow a reliable estimation of the numerical uncertainty. The effect of the computational domain size has been reduced
to negligible levels (below the numerical uncertainty). And the same holds for the iterative and round-off errors. In the
finest grids of each set, the numerical uncertainty of the friction resistance coefficient is always below 1%. Special attention
has further been given to the solution behaviour in the laminar-to-turbulent transition region. Curve fits have been applied
to the data obtained at the 14 Reynolds numbers and the numerical friction lines are compared with four proposals from the
open literature: the 1957 ITTC line, the Schoenherr line and the lines suggested by Grigson and Katsui et al. The differences
between the numerical friction lines obtained with the seven turbulence models are smaller than the differences between the
four lines proposed in the open literature. 相似文献
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