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本文从二自由度进动陀螺仪在鱼雷武器中使用的具体条件出发,提出了影响陀螺仪支架误差的主要因素。并采用了坐标转换矩障的方法推导出在各种使用条件下和不同安装方式的支架误差计算公式。可供分析计算支架误差用。 本文着重指出发射条件对陀螺仪支架误差的影响,而这一点对在运动着的基座上启动的陀螺仪十分重要,这一因素在提供支架误差的一般资料中往往被忽略。因此本文所提供的陀螺支架误差计算公式,不仅适用于鱼雷武器,而且也适用于具有相同条件的其它自航体用同类陀螺仪支架误差的计算。
In this paper, starting from two degrees of freedom precession gyroscope torpedo weapons used in the specific conditions, the main factors that affect the gyroscope support error. The method of coordinate transformation moment is used to derive the calculation formula of the bracket error under different conditions of use and different installation methods. Available for analysis and calculation of bracket error. This article highlights the effects of launch conditions on the gyroscope mount error, which is important for gyroscopes that are actuated on a moving base, a factor that is often overlooked in providing general information on bracket errors. Therefore, the gyroscope error calculation formula provided in this paper not only applies to torpedo weapons, but also to the calculation of the gyroscope bracket error of other gyroscopes with the same conditions.