1) reentry warhead
再入弹头
1.
The stochastic mathematical model about maneuverable reentry warhead attacking ground target was established.
建立了机动再入弹头攻击地面目标的随机数学模型,根据再入机动弹头攻击目标的要求,选择合理的代价函数和控制量的约束方程,利用随机最优控制理论,结合再入弹头的运动学与动力学方程,获得再入弹头的最优制导律。
2.
In order to hit the target accurately,with minimum velocity losses as its objective,an optimal guidance law in the plane for reentry warhead on angular velocity was deduced according to the theory of sub-parallel approach and optimal theory.
为了使再入弹头的速度损失最小,并能准确击中目标。
3.
The Stochastic mathematic model of maneuvering reentry warhead was proposed, and the rational slide switch surface was chosen based on the desire of attacking ground target.
建立了机动再入弹头随机数学模型,根据攻击目标的要求选择合理的滑模变结构开关面。
2) 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。
3) non-spinning reentry warhead
非自旋再入弹头
4) reentry-warhead
再人弹头
5) 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。
6) 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。
补充资料：弹头烧蚀(见弹头防热)
弹头烧蚀(见弹头防热)
warhead ablation
dantou shaoshi弹头烧蚀(warhead的lation)见弹头防热。
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