The optimal glidetrajectory and control system of combined guidance munition were studied.
研究了制导炮弹最优滑翔弹道与控制问题。
2
The longitudinal glidetrajectory design for general air-to-ship missile is studied. Using spline function as glide standard trajectory of missile is presented.
对一般空舰导弹的纵向下滑弹道进行了设计研究,提出用样条函数作为导弹的纵向下滑基准弹道。
3
By the study of extended range guided munitions (ERGM) trajectory characteristics, ERGM free-flight and glidetrajectory characteristics are revealed and illustrated.