The structures,mechanical properties and electronic structures of M metals(M=Ti,V,Cr,Mn and Fe)dopedβ-Si_(3)N_(4) were investigated by First-principles calculations within CASTEP.The calculated lattice parameters of...The structures,mechanical properties and electronic structures of M metals(M=Ti,V,Cr,Mn and Fe)dopedβ-Si_(3)N_(4) were investigated by First-principles calculations within CASTEP.The calculated lattice parameters ofβ-Si_(3)N_(4) were consistent with previous date.The cohesive energy and formation enthalpy show that initialβ-Si_(3)N_(4) has the highest structural stability.The calculated elastic constant and the Voigt-Reuss-Hill approximation indicate that elastic moduli ofβ-Si_(3)N_(4) are slightly reduced by M doping.Based on Poisson’s and Pugh’s ratio,β-Si_(3)N_(4) is a ductile material and the toughness ofβ-Si_(3)N_(4) increases with M doping,and Fe doping exhibited the best toughness.The results of density of states,charge distributions and overlapping populations indicate thatβ-Si_(3)N_(4) has the strong covalent and ionic bond strength between N and Si.展开更多
针对重力扰动引起惯性水平基准姿态测量误差进而导致天文/惯性组合导航系统定位精度下降的问题,提出天文/惯性组合系统中的重力扰动补偿方法。首先,基于导航误差模型分析了影响天文/惯性组合导航系统定位精度的主要因素。其次,推导了重...针对重力扰动引起惯性水平基准姿态测量误差进而导致天文/惯性组合导航系统定位精度下降的问题,提出天文/惯性组合系统中的重力扰动补偿方法。首先,基于导航误差模型分析了影响天文/惯性组合导航系统定位精度的主要因素。其次,推导了重力扰动、惯性水平基准姿态测量误差与天文导航定位误差之间的传播机理。然后,研究了重力扰动建模与修正方法,并将重力扰动补偿方法应用于惯性水平基准的导航解算回路中,实现重力扰动的有效补偿。跑车试验结果表明,所提重力扰动补偿方法可以将天文/惯性组合导航系统中定位误差的振荡幅值由1.6 n mile降低至0.5 n mile。展开更多
文摘The structures,mechanical properties and electronic structures of M metals(M=Ti,V,Cr,Mn and Fe)dopedβ-Si_(3)N_(4) were investigated by First-principles calculations within CASTEP.The calculated lattice parameters ofβ-Si_(3)N_(4) were consistent with previous date.The cohesive energy and formation enthalpy show that initialβ-Si_(3)N_(4) has the highest structural stability.The calculated elastic constant and the Voigt-Reuss-Hill approximation indicate that elastic moduli ofβ-Si_(3)N_(4) are slightly reduced by M doping.Based on Poisson’s and Pugh’s ratio,β-Si_(3)N_(4) is a ductile material and the toughness ofβ-Si_(3)N_(4) increases with M doping,and Fe doping exhibited the best toughness.The results of density of states,charge distributions and overlapping populations indicate thatβ-Si_(3)N_(4) has the strong covalent and ionic bond strength between N and Si.
文摘针对重力扰动引起惯性水平基准姿态测量误差进而导致天文/惯性组合导航系统定位精度下降的问题,提出天文/惯性组合系统中的重力扰动补偿方法。首先,基于导航误差模型分析了影响天文/惯性组合导航系统定位精度的主要因素。其次,推导了重力扰动、惯性水平基准姿态测量误差与天文导航定位误差之间的传播机理。然后,研究了重力扰动建模与修正方法,并将重力扰动补偿方法应用于惯性水平基准的导航解算回路中,实现重力扰动的有效补偿。跑车试验结果表明,所提重力扰动补偿方法可以将天文/惯性组合导航系统中定位误差的振荡幅值由1.6 n mile降低至0.5 n mile。