小高炮高角及飞行时间误差的计算与近似
LCULATION AND APPROXIMATION OF SUPERELEVATION ERROR AND FLIGHT-TIME ERROR FOR SMALL-CALIBER ANTI-AIRCRAFT GUN
高角及飞行时间误差计算高炮毁歼概率的基础数据。根据空气弹道弹丸质心方程组，给出了解弹道方程组与高阶插值结合计算非标准条件下高角及飞行时间误差的方法，计算出某型高炮三种偏差条件下的误差数据，并对一种现有的误差近似计算公式进行了验证，给出了近似系数。
he superelevation errors and flight-time errors are the basic data for calculating kill capability of anti-airceaft guns. A method for obtaining those errors under abnormal conditions is present by solving the set of ballistic equations and interpolating in hihg-order associatively, and the error data of a certain gun are calculated under three deviated conditions. An existed set of approximated formulas is proved and corresponding coefficients are presented.
廖洲宝、刘钊
火炮
弹道方程组 弹道条件偏差 高角误差 飞行时间误差
set of ballistic equations deviation of fire conditions superelevation error flight-time error
廖洲宝,刘钊.小高炮高角及飞行时间误差的计算与近似[EB/OL].(2006-11-06)[2025-08-06].http://www.paper.edu.cn/releasepaper/content/200611-87.点此复制
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