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研究与计算结果表明:地地战术导弹,射程在300公里以内时,全程惯性制导与半程惯性制导相比,陀螺工具误差引起的落点偏差有明显的减少。并从物理概念上对此作了解释。
The result of research and calculation shows that compared with half-way inertial guidance, the ground-based tactical missile has a significant reduction of landing deviation caused by the error of the gyro tool when the range is within 300 km. And from the physical concept of this explanation.