大家都搜:
初始校准
1、alignment definition───路线定义
2、wheel alignment───n.前轮定位;前轮校正;n.前轮定位,前轮校正
3、alignment test───精度检查
4、text alignment───n.文字对齐;文本对齐
5、alignment───n.队列,成直线;校准;结盟
6、alignment mark───定位记号;对准记号;调节标记;调整标记,定位记号,对准标记
7、jaw alignment───钳口对齐
8、Initial Rings───初始环
9、initial───n.词首大写字母;原始细胞;adj.最初的;字首的;vt.用姓名的首字母签名
1、Simulation result showed that this algorithm is effective in the study on SINS' initial alignment problem.───FangZhen结果证实了该算法在捷联惯导XiTong初始对准问题研究中的有效性。
2、Bi-GPS receivers are applied to measure the azimuth angle in terms of initial alignment of the integrated system.───并利用双GPS接收机测量方位角解决了组合XiTong的初始方位对准问题。
3、The observability and degree of observability of initial alignment of SIS on moving base are all-around analyzed and studied.───对捷联惯性XiTong动基座初始对准的可观测性和可观测度进行了全面的分析和研究。
4、So the combination of genetic algorithm and simulated annealing could be sufficient to initial alignment for speed and precision.───因此,将遗传算法和模拟退火算法结合起来,能很好地解决初始对准的速度和精度的问题。
5、This technology may help INS to realize fast initial alignment.───该项技术可辅助惯导XiTong实现快速初始对准。
6、Thus, it has practical significance to research on characteristics of errors and integrated initial alignment based on SINS.───因此,研究捷联惯导XiTong的误差特性和基于此的组合对准方法具有重要的现实意义。
7、Linear and nonlinear error models for Inertial Navigation System (INS) initial alignment are established.───建立了惯导XiTong(INS)初始对准的线性和非线性误差模型。
8、The initial alignment and calibration of strap down inertial system on a rocking base are investigated.───研究摇摆基座上捷联惯性导航XiTong的初始对准技术。
9、Initial alignment is a key technique of INS, which plays an important role in the performance of navigation system.───初始对准是惯性导航XiTong的关键技术之一,它直接影响惯导XiTong的导航性能。
1、Because of the poor observability of INS on stationary base, the estimation of the azimuth error will converge very slowly in initial alignment by means of Kalman filter.
2、The time of initial alignment is reduced greatly and the accuracy of azimuth alignment is improved.
3、After the initial alignment, the software of inertial navigation system is completed and the error of inertial navigation system is studied.
4、A fast estimation method of the azimuth error angle is proposed for the initial alignment of INS, and the result illustrates the efficiency of the method.
5、Furthermore, several main error factors on initial alignment precision are analyzed, and the corresponding solutions are provided. The simulation results show that the method is feasible.
6、The simulation results show that this method can effectively carry out initial alignment on an oscillatory base when disturbing frequency characteristics is known.
7、The kernel problem of antenna stabilization and tracking technology is the initial alignment and automatic tracking technology of antenna toward satellite.
8、Linear and nonlinear error models for Inertial Navigation System( INS ) initial alignment are established.