CHEN Hai-ming, XIONG Zhi, QIAO Li, et al. Application of CNS-INS integrated navigation technology in high-altitude aircraft[J]. 2008, (9): 4-6+10. DOI: 10.13873/j.1000-97872008.09.005.
天文—惯性组合导航技术在高空飞行器中的应用
摘要
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。概括了CNS/INS导航的特有优点
提出了发展CNS-INS组合导航的必要性
讨论了今后机载CNS-INS组合导航技术的研究发展方向。
Abstract
The application and development of CNS-INS integrated navigation system in high-altitude aircrafrt are overviewed.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 the aviation aircraft of implementation of the long voyage and high-flying
it can meet the needs of aviation aircraft to high-precision navigation system.The unique advantages of CNS/INS integrated navigation system is summarized.The necessity of development of CNS-INS integrated navigation system is proposed
and the future research development direction for CNS-INS navigation technology on aircraft is discussed.