1) Loran inertial navigation system
劳兰惯性导航系统
2) Loran-inertial integrated navigation
劳兰-惯性组合导航系统
4) Loran C-inertial integrated navigation
罗兰C-惯性导航系统
5) inertial navigation system
惯导系统;惯性导航系统
6) 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。
补充资料:罗兰—C导航系统(见飞机双曲线导航系统)
罗兰—C导航系统(见飞机双曲线导航系统)
Loran-C navigation system
七以U工un一七Qaonang xitong罗兰一C导航系统(Loran一c nav堪at、onsystem)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