So it is necessary to calculate gravity anomaly real - time on the missile.
主动段扰动引力是引起弹道导弹制导方法误差的主要因素.
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Formulas of inversion and cosine transform spectrum of gravity anomaly cylinderfinite stretched staircase were deduced.
提出利用余弦变换,研究规则体重力异常谱特征及反演方法.
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