1) Maneuverable Reentry Trajectory
再入机动弹道
3) Reentry trajectory
再入弹道
1.
in this paper, an adaptive estimator of reentry trajectory parameters is proposed.
本文研究再入弹道参数的自适应估计。
4) reentry maneuvering warhead
再入机动弹头
1.
Variable structure guidance law of reentry maneuvering warhead with terminal angular constraint
带落角约束的再入机动弹头的变结构导引律
2.
Because perpendicular impact on the target was required for reentry maneuvering warhead,the integrated guidance law with terminal angular constraint,which comprised diving-plane guidance equation and turning-plane guidance equation,was derived.
针对再入机动弹头垂直打击目标的要求,研究了具有末端落角约束的复合导引律。
5) Ballistic Reentry
弹道式再入
1.
Neural network is used in the ballistic reentry guidance of orbit weapon to get flight-path angle in real time.
将神经网络应用于轨道武器的弹道式再入制导中,实时得到所需航迹角,以此形成制导信号。
6) re-entry vehicle
再入弹道段
补充资料：弹道(见弹道学)
弹道(见弹道学)
trajectory
dQfldQO弹道(t rajectory)见弹道学。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条