1.
Based on the inertial guidance instrument error model, the model of reentry point's parameters is established in this paper.
基于惯性制导工具误差模型,推导出存在工具误差时的再入点运动参数模型。
2.
Instrument Error Calculation and Compensation of Rate Strapdown Inertial Navigation System
速率捷联惯导系统工具误差计算与补偿研究
3.
THE CORRECTION FOR THE BASIC AXIS ERROR OF THE INERTIAL TERMINAL GUIDANCE ON THE ANTIRADAR MISSILE
反雷达导弹惯性末制导基准轴误差的修正
4.
Improved FOG Strapdown Inertial Navigation System and Error Analysis
旋转光纤捷联惯性导航系统的误差调制分析
5.
Rsearch on SINS Error Transfer Model of Ballistic Missile
弹道导弹捷联惯性导航系统误差传播模型
6.
This paper proposes a nonlinear model for guidance instrument systematic error separation based on tracking trajectory data.
给出了在弹道参数上直接解算的制导工具系统误差分离非线性模型。
7.
Research on Error Excitatedation in Flexible SINS Caused by Airborne Installation Way;
挠性捷联惯导系统机载安装方式误差激励研究
8.
Error Compensation Methods for Inertial Navigation System in Deep Sea
深海环境惯性导航系统误差补偿方法的研究
9.
The Equipollence Validation of Two Inertial Error Models in SINS/GPS Integrated Navigation
SINS/GPS组合导航中两种惯导误差模型的等价性验证
10.
inertial navigation and guidance
惯导与制导惯性导航与制导
11.
Tilt Angle Error Model of Inertial Navigation System
惯性导航系统水平角误差计算机辅助分析与建模
12.
Analysis for Gravity Anomaly’s Influence on Platform INS Error
重力异常对平台式惯性导航系统误差的影响分析
13.
Methods of error compensation for azimuth holding system in an INS (inertial navigation system) are presented.
给出了陆用惯性导航系统方位保持仪的误差补偿方法.
14.
Errors-in-Variables Model based Error Separation of Inertial Navigation Platform
基于EV模型的惯导平台误差分离方法
15.
Error Analysis for Measurement of Missile's Movement Inertia with Torsion Pendulum
扭摆法测量导弹转动惯量的误差分析
16.
A Practical Algorithm for Speed Error Compensation of SINS
捷联惯导系统速度误差补偿实用算法
17.
IMU Error Coefficient Compensation in Free-field Segment of Ballistic Missile
弹道导弹惯导系统误差系数自由段补偿
18.
Measurement Error Model of IMU in Strapdown Inertial Guidance System of Manpads Missile
单兵导弹捷联惯导系统IMU测量误差模型