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《舰船科学技术》2013,(12):114-120
本文研究旋转惯导系统设计中的一些重要问题,包括误差调制机理、误差传播特性和旋转方案设计。考虑惯性器件的一些典型误差,分析旋转式惯导系统的误差传播特性,并验证旋转调制下误差的影响效果。通过分析,提出双轴旋转方案合理设计的条件,设计出一种基于64次序的双轴旋转方案以实现平均掉惯性器件所有常值误差的目标。基于该旋转方案,仿真出惯性测量单元主要误差项的调制形式,通过一个旋转周期的积分,得到这些误差引起的累积速度或角度误差的调制形式,进一步验证了旋转调制对误差的调制效果。最后,通过对旋转调制下惯导系统长时间导航误差的仿真,验证了所设计旋转方案的有效性和旋转调制的优越性。 相似文献
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提高惯导系统对于惯性器件误差负面影响的抑制能力,对于改善系统的导航精度具有重要意义.本文对惯导系统误差方程进行分析,重点讨论对称位置上惯性器件误差的积累效果,系统地研究了单轴旋转调制对捷联惯性导航系统惯性器件误差的自动补偿机理,详细分析了单轴旋转对惯性器件常值误差、标度因数误差的抑制情况.对单轴旋转调制方案进行仿真,验证了理论分析的正确性. 相似文献
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旋转调制式捷联惯导系统初始对准方案研究 总被引:1,自引:0,他引:1
初始对准技术是惯性导航的关键技术之一,其精度将直接影响导航精度。旋转调制式捷联惯导系统在一定的旋转方案下虽然可以将惯性组件的误差调制掉从而提高系统导航精度,但其初始对准的误差则不受调制,所以有必要对旋转调制式惯导系统的初始对准进行深入研究,确定适合旋转式捷联系统使用的对准技术和方案以进一步提高系统精度。文章对可应用于旋转调制式捷联惯导系统的三种对准方案做了研究分析并进行了仿真。结果显示,二位置对准方案可显著提高系统变量的可观测度,连续旋转方案对准精度最高,收敛速度最快,效果最好。 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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舰船武器系统海上航行精度测试[1]需要真航向进行系统误差分析,而舰船在没有装备真航向测量系统情况下,如何提供真航向测量数据一直是需要解决的难题。论文采用舰船高精度光电跟踪仪、有源岸标和差分GPS定位设备,对舰船瞬时真航向测量方法及其可行性进行了深入细致的分析与研究,最终确定出系统瞬时航向测量精度是否满足使用要求。 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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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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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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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