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本文对弹道式导弹捷联制导系统的动态误差作了理论分析,进行了实例计算,并与阿波罗登月舱应急系统的相应数据进行了比较,结果相当接近。
In this paper, the dynamic error of the ballistic missile strapdown guidance system is analyzed theoretically, and the example calculation is made. The result is quite close to the corresponding data of Apollo lunar module emergency system.