Experimental evidence is presented showing obvious azimuthal dependence of single event upsets(SEU) and multiple-bit upset(MBU) patterns in radiation hardened by design(RHBD) and MBU-sensitive static random access mem...Experimental evidence is presented showing obvious azimuthal dependence of single event upsets(SEU) and multiple-bit upset(MBU) patterns in radiation hardened by design(RHBD) and MBU-sensitive static random access memories(SRAMs), due to the anisotropic device layouts. Depending on the test devices, a discrepancy from 24.5% to 50% in the SEU cross sections of dual interlock cell(DICE) SRAMs is shown between two perpendicular ion azimuths under the same tilt angle. Significant angular dependence of the SEU data in this kind of design is also observed, which does not fit the inverse-cosine law in the effective LET method. Ion trajectory-oriented MBU patterns are identified, which is also affected by the topological distribution of sensitive volumes. Due to that the sensitive volumes are periodically isolated by the BL/BLB contacts along the Y-axis direction, double-bit upsets along the X-axis become the predominant configuration under normal incidence.Predominant triple-bit upset and quadruple-bit upset patterns are the same under different ion azimuths(Lshaped and square-shaped configurations, respectively). Those results suggest that traditional RPP/IRPP model should be promoted to consider the azimuthal and angular dependence of single event effects in certain designs.During earth-based evaluation of SEE sensitivity, worst case beam direction, i.e., the worst case response, should be revealed to avoid underestimation of the on-orbit error rate.展开更多
一些舰艇装备两套或多套惯性导航系统。为提高这些舰艇导航信息输出的精度和稳定性,提出一种双惯导组合导航方法。从惯性导航系统的误差特性出发,分析了固定指北惯性导航系统和台体方位旋转惯导系统的误差特性,并根据两种惯导系统的不...一些舰艇装备两套或多套惯性导航系统。为提高这些舰艇导航信息输出的精度和稳定性,提出一种双惯导组合导航方法。从惯性导航系统的误差特性出发,分析了固定指北惯性导航系统和台体方位旋转惯导系统的误差特性,并根据两种惯导系统的不同误差特性,设计了Kalman滤波组合导航控制方案,通过仿真验证了组合导航控制方案的效果。仿真结果表明,采用该方法后,在不增加任何硬件成本的基础上,能够提高导航信息输出精度和稳定性。例如,当陀螺漂移为0.002(°)/h,加速度计零偏5×10-5 g时,固定指北惯导24 h定位误差约为2.8 n mile,速度误差波动约0.2 kn,台体方位旋转惯导系统24 h定位精度约为1.7 n mile,速度误差波动约0.5 kn;当采用组合导航控制时,组合输出24 h定位精度约1.5 n mile,速度误差波动约0.15 kn。展开更多
基金Supported by National Natural Science Foundation of China(Nos.11179003,10975164,61204112 and 61204116)China Postdoctoral Science Foundation(No.2014M552170)
文摘Experimental evidence is presented showing obvious azimuthal dependence of single event upsets(SEU) and multiple-bit upset(MBU) patterns in radiation hardened by design(RHBD) and MBU-sensitive static random access memories(SRAMs), due to the anisotropic device layouts. Depending on the test devices, a discrepancy from 24.5% to 50% in the SEU cross sections of dual interlock cell(DICE) SRAMs is shown between two perpendicular ion azimuths under the same tilt angle. Significant angular dependence of the SEU data in this kind of design is also observed, which does not fit the inverse-cosine law in the effective LET method. Ion trajectory-oriented MBU patterns are identified, which is also affected by the topological distribution of sensitive volumes. Due to that the sensitive volumes are periodically isolated by the BL/BLB contacts along the Y-axis direction, double-bit upsets along the X-axis become the predominant configuration under normal incidence.Predominant triple-bit upset and quadruple-bit upset patterns are the same under different ion azimuths(Lshaped and square-shaped configurations, respectively). Those results suggest that traditional RPP/IRPP model should be promoted to consider the azimuthal and angular dependence of single event effects in certain designs.During earth-based evaluation of SEE sensitivity, worst case beam direction, i.e., the worst case response, should be revealed to avoid underestimation of the on-orbit error rate.
文摘一些舰艇装备两套或多套惯性导航系统。为提高这些舰艇导航信息输出的精度和稳定性,提出一种双惯导组合导航方法。从惯性导航系统的误差特性出发,分析了固定指北惯性导航系统和台体方位旋转惯导系统的误差特性,并根据两种惯导系统的不同误差特性,设计了Kalman滤波组合导航控制方案,通过仿真验证了组合导航控制方案的效果。仿真结果表明,采用该方法后,在不增加任何硬件成本的基础上,能够提高导航信息输出精度和稳定性。例如,当陀螺漂移为0.002(°)/h,加速度计零偏5×10-5 g时,固定指北惯导24 h定位误差约为2.8 n mile,速度误差波动约0.2 kn,台体方位旋转惯导系统24 h定位精度约为1.7 n mile,速度误差波动约0.5 kn;当采用组合导航控制时,组合输出24 h定位精度约1.5 n mile,速度误差波动约0.15 kn。
