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针对进一步提高新一代运载火箭入轨精度的问题,本文在分析运载火箭制导系统基本结构的基础上,对采用我国北斗系统与捷联惯性导航系统双源信号深组合导航方式在新一代运载火箭制导系统中的应用进行了初步的探索。结合新一代运载火箭的新特点,从北斗系统与捷联惯性导航系统双源信号深组合导航方式的结构和适用条件两个方面进行了简要的分析。其研究成果可为我国新型运载火箭制导系统的研制提供一定的理论依据和技术支持。
In order to further improve the accuracy of a new generation of launch vehicle orbit, based on the analysis of the basic structure of the launch vehicle guidance system, this paper adopts the dual-source deep combination navigation system of BeiDou system and SINS in a new generation of launch vehicle guidance The application of the system has been initially explored. Combined with the new characteristics of the new generation of launch vehicles, this paper briefly analyzes the structure and applicable conditions of the deep navigation system with dual sources of Beidou system and SINS. The research results can provide some theoretical basis and technical support for the development of China’s new launch vehicle guidance system.