详细研究了不同机动方式对机载武器捷联惯导系统传递对准性能的影响，并对计算机仿真结果进行了深入的分析。
Detailed investigation of different maneuver manners effect on the performance of SINS transfer alignment and in-depth analysis of the simulation outcomes were carried out.
为了实现弹载计算机和惯导的高速数据通信，对数据通信的工程化电路进行了设计。
In order to realize high speed data communication between missile-borne computer and inertial navigation system, the engineering circuitry of data communication is designed.
计算机在捷联式惯导中起着重要的作用。
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