1) laser strapdown inertial measurement unit(LSIMU)
激光捷联惯组
2) laser SINS
激光捷联惯导
1.
Influence of turntable angular position reference errors on laser SINS calibration
转台角位置基准误差对激光捷联惯导标定的影响分析
3) SIMU
捷联惯组
1.
The Method Study of Increase the Stabilization Period of SIMU;
延长捷联惯组稳定期的方法研究
2.
Prior distribution of SIMU successive test data based on random weighting;
基于随机加权的捷联惯组历次测试数据验前分布研究(英文)
3.
The Population Parameter Prior Distribution Study of Successive Test Data of SIMU Based on Random Weighting Method;
基于随机加权法的捷联惯组历次测试数据总体参数验前分布研究
4) strapdown inertial measurement unit
捷联惯组
1.
Engineering calibration technology of strapdown inertial measurement unit before launch
捷联惯组射前工程化标定技术
2.
Aiming at the small sample of strapdown inertial measurement unit(SIMU) successive test data,a Bayesian method was used to study its statistical characteristics.
针对捷联惯性测量组合(捷联惯组)历次测试数据小样本的问题,提出了通过Bayes方法研究捷联惯组历次测试数据的统计特性。
3.
This paper mainly discusses the error model of strapdown inertial measurement unit,presents an error separating and data processing scheme under dynamic condition based on rocket sled test,and analyses the data processing method in rocket sled test.
捷联惯组火箭橇试验是验证捷联惯组在复合环境下的误差模型、评定制导系统误差模型精度以及分离大过载条件下捷联惯组误差系数的有效手段。
5) laser strapdown inertial navigation system
激光捷联惯性导航系统
1.
The principle of noncommutativity errors is presented, which exists in the attitude and velocity updating algorithms of laser strapdown inertial navigation system.
针对激光捷联惯性导航系统姿态和速度算法中所引入的不可交换性误差进行了原理上的分析 ,重点分析了速度计算过程中不可交换性误差产生的原因 。
6) LSINS
激光捷联惯导系统
1.
Kalman/particle filter’s design and simulation in LSINS/TAN;
激光捷联惯导系统/地形辅助导航系统中卡尔曼/粒子组合滤波算法设计及仿真
补充资料：惯捷
1.熟练敏捷。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条