3) micro inertial navigation system
微惯性导航系统(MINS)
4) inertial navigation system
惯导系统;惯性导航系统
5) Inertial navigation system(INS)
惯性导航系统
1.
On the basis of the analysis of aviation aircraft load celetid navigation system(CNS)/inertial navigation system(INS)integrated navigation system at home and abroad,the technical performance of CNS/INS integrated navigation system from working environment,integrated patterns and navigation solution is analyzed and it is pointed out that CNS-INS integrated navigation system is more applicable to .
综述了天文—惯性组合导航在高空飞行器中的应用和发展概况,在分析了国内外装载天文导航系统(CNS)/惯性导航系统(INS)的航空飞行器基础上,从工作环境、组合模式、导航解算等方面分析了CNS/INS的技术性能,指出CNSI-NS组合导航更适用于执行长航时、高空飞行的航空飞机,能够满足航空飞行器对高精度导航系统的需要。
2.
A new fusion algorithm of the measurements from global positioning system(GPS) and inertial navigation system(INS)is presented to compensate the weaknesses of current integrated navigation system.
为了弥补现有组合导航算法的不足,提出了一种新的GPS量测数据和惯性导航系统(INS)数据的融合算法。
6) inertial navigation system
惯性导航系统
1.
Simulation and optimization of heat-transfer route of isolator in a certain type of Inertial navigation system;
某型号惯性导航系统内减振器导热路径优化仿真(英文)
2.
Study on algorithm of compensating the gyro drift for Inertial Navigation System;
惯性导航系统陀螺漂移补偿算法研究
3.
Research of unscented Kalman filter in initial alignment of inertial navigation systems;
UKF方法在惯性导航系统初始对准中的应用研究
补充资料：奥米加导航系统(见飞机双曲线导航系统)
奥米加导航系统(见飞机双曲线导航系统)
Omega navigation system
Aomiiia daohang Xitong奥米加导航系统(omeg。。avigationsystem)见飞机双曲线导航系统。
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