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1)  fighter plane attack envelope
飞机攻击区
1.
This paper introduces the method of short distance navigation, path characteristics and parameters of fighter plane, presents calculation methods of fighter plane attack envelope and missile launch envelope based on short distance navigation effciency.
介绍了载机近距引导的方法、轨迹 (路径 )特征及参数变化情况 ,给出了基于近距引导效能的飞机攻击区、导弹发射区的计算方法 ,并对一定条件下的近距引导效能进行了分析计算。
2)  attacking aircraft
攻击型飞机
1.
The great changes have taken place in the operational environments of modem wars due to the development of military techniques and the performance improvements of weaponry equipment provide attacking aircraft many opportunities to show its predominance.
攻击型飞机是现代战争的主力,也是世界各国空中力量的发展重点。
3)  Attack area
攻击区
1.
The corresponding simplified autopilot,the influencing factors and the searching algorithm of attack area are also analyzed.
采用程序转弯和空间比例导引复合制导以实现导弹越肩发射,并设计了相应的简单自动驾驶仪,分析了攻击区影响因素以及攻击区搜索算法,最后计算出了空空导弹的全向攻击区,验证了制导方法的正确性。
2.
Base on the models builds up model of attack area of general air to air missile ,and calculates the general attack air to iar missile ,and calculates the general attack area.
推导了空空导弹攻击空中目标的三维空间控制系统数学模型 ,该模型由目标运动方程组 ,导弹运动方程组 ,导弹与目标间的相对运动方程组 ,导弹控制与制导模型以及导弹状态模型等组成 ,在此基础上建立了通用空空导弹攻击区计算模型 ,并进行了仿真计算。
3.
By calculating and simulating,the three dimensional attack area of the bomb has been got,and the three dimensional animation technology is applied to the software development of the real time simulation system.
通过仿真计算,得到了该弹的三维攻击区,并将三维动画技术应用于实时仿真系统的软件开发
4)  launch area
攻击区
1.
Through the model,we can form the launch area of all kinds of attack conditions.
建立了空空导弹攻击区快速模拟法解算的模型,该模型可快速生成各种攻击条件下的导弹攻击区,且具有一定通用性,适合全向攻击。
5)  Attacking area
攻击区
1.
It is put forward that the optimal launch point should be selected in the common segment of attacking path and attacking area according to the rule of maximizing the overall kill probability.
提出在攻击航线与攻击区的相交段上 ,以综合杀伤概率最大化原则来选择多目标攻击的最佳发射点。
6)  Distinguishing attack
区分攻击
1.
Improved distinguishing attack on Py;
对Py的一种改进的区分攻击
2.
In this paper,the authors improve the lower bound of the linear complexity of the balanced shrinking sequences,and analyze the security of the generator with correlation attack and distinguishing attack.
改进了平衡收缩序列线性复杂度的下界,并从相关攻击和区分攻击的角度对平衡收缩生成器的安全性进行了分析,认为平衡收缩序列依然不能抵抗相关攻击和区分攻击。
3.
A distinguishing attack on this structure is presented.
对新提议的一种基于线性反馈移位寄存器、非线性反馈移位寄存器和过滤布尔函数的序列密码结构的安全性进行了研究,对这种结构给出了一种区分攻击。
补充资料:变后掠翼飞机(见后掠翼飞机)


变后掠翼飞机(见后掠翼飞机)
swing-wing aircraft

bianhoul位eyi feiii变后掠翼飞机(swing一wing aircran)见后掠翼飞机。
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