The Launch and Test Range System includes ground-based surveillance, navigation, flight operations and analysis, command and control, communications and weather assets for space missions.

发射和测试系统包括空间飞行的地面系统任务的监视，导航，飞行操作和分析，指挥和控制，通信和气象资产。

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These tasks range from design of the mechanics, sensor system, energy system, computer architecture of the robot, control and navigation algorithms to an adequate operating system and user interface.

这些业务范围从设计的力学、传感器系统、能源系统、计算机体系结构的机器人、控制和导航算法到适当的操作系统和用户界面。

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This dissertation works on the pre-theoretical research and technical exploration with SINS /GPS embedded integrated navigation system, which based on the pseudo-range and pseudo-range rate.

本文针对基于伪距、伪距率的SINS/GPS嵌入式组合导航系统，开展了前期理论研究和技术探索。

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