摘要
该文运用机构学的数学工具——刚体旋转矩阵,推导并建立了根据火炮(含火箭炮)姿态计算装定诸元的解析公式。在此基础上,进行了验证性计算。
In this paper, a mathematical means of mechanics--rigidbody rotation matrix is applied to derive a set of analytic formulas forgun (including rocket) setting data calculation, when the state of gunis known. On the basis of this, testing and verifying computations havebeen processed.
