In this paper an analytic solution of freeflighttrajectory of ballistic vehicle is presented.
本文提出了弹道式飞行器自由飞行轨道的解析解法。
2
By using the line of sight (LOS) measurements from space based infrared sensors, freeflight phase trajectory estimation problem of ballistic missile is studied.
主要研究空间预警系统利用星载红外传感器的视线测量估计弹道导弹自由飞行段弹道的问题。
3
The trajectory model consists of the uncontrolled freeflight segment, the inertial guided glided segment and the final guidance segment, which accords with the proportional guided law.