1) missile pitch channel
导弹俯仰通道
2) pitch plane
俯仰通道
1.
Integrated guidance and control for the pitch plane of BTT missile;
导弹俯仰通道制导与控制一体化设计
3) control theory of pitch channel
俯仰通道控制原理
4) missile channel
导弹通道
1.
In order to evaluate the effect of air-defense missile system credibility on fire efficiency,regarding typical air-defense missile system as three-echelon series-parallel connection configuration,the evaluation models of missile channels credibility indexes including fire and combat preparative extent index were deduced.
为评估防空导弹系统可靠性对射击效率的影响,将典型防空导弹系统处理成三级串并联系统,推证了导弹通道可靠性指标——发射准备程度和战斗准备程度等评估模型,提出了导弹通道故障时射击决策的优化方法,根据系统及导弹通道可靠性特点,建立了基于可靠性的射击效率评估模型。
6) damping-in-pitch derivative
俯仰阻尼导数
1.
Through the numerical simulation of forced oscillation of liftbody by solving the (N-S) equations, the equilibrium gas effect on damping-in-pitch derivatives is investigated.
通过数值求解N-S方程,模拟升力体外形的强迫振动过程,研究了平衡气体效应对带翼飞行器俯仰阻尼导数的影响。
2.
In this paper, the supersonic damping-in-pitch derivativesof blunt body were calculated with two methods: (1) harmonic perturbationmethod by solving Euler equations; (2) simulant viscous flow field by solving unsteady N-S equations.
分别采用：（1）Euler方程的谐振摄动法；（2）薄层近似的非定常N－S方程模拟有粘扰动流场两种方法计算了钝体外形的高超声速俯仰阻尼导数。
补充资料：俯仰
〈书〉①低头和抬头：～之间。②指一举一动：～由人。
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