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阐述用姿态陀螺仪判定末制导炮弹制导平面的原理，结合末制导炮弹的运动，建立了陀螺仪判定制导平面的理论公式，并进行了误差分析。确定弹丸在飞行弹道上陀螺启动的理想位置。
The principle of using the attitude gyro to determine the guidance plane of the terminal guidance projectile is described. Combined with the movement of the terminal guidance projectile, a theoretical formula for determining the guidance plane of the gyro is established, and the error analysis is carried out. Determine the projectile in the flight trajectory gyroscope ideal position.