Mobile
Log In Sign Up
Home > chinese-english > "yawing motion" in English

English translation for "yawing motion"

偏航运动

Related Translations:
yaw:  n.【海、空】偏航(角);侧滑(角)。vi.【海、空】偏航,左右摇转;摇摇晃晃地前进;盘旋。vt.使偏航;使左右摇转;使摇摇晃晃地前进。n.-er 【航空】偏航控制器;方向舵。
yaws:  n.pl. 【医学】雅司病〔一种热带慢性痘疹状皮肤传染病〕。
yaw accuracy:  偏航精度
yawed tube:  带侧滑角的管
yaw law:  侧滑关系曲线
yawing force:  侧向力偏航力
yawing rotation:  偏航旋转偏航运动绕垂直轴的转动
yaw vibration:  横摆振动(汽车绕过重心垂直轴的角振动)
bush yaws:  鼻咽粘膜利什曼病
yaws arthritis:  雅司病性关节炎
Example Sentences:
1.Identical autopilots are used to control the pitch and yaw motions if the missile has two planes of symmetry .
如果导弹有两个对称面,则使用相同的自动驾驶仪控制俯仰和偏航运动。
2.In this paper , wheel - rail rolling contact creepages and creeps of independently rotating wheel are analyzed , the effects of lateral and yaw motions of independently rotating wheel , and the curve radius to creepages of wheel - rail rolling contact are emphasisatically researched . 4
论文对独立旋转车轮的轮轨滚动接触蠕滑率/力进行了分析,研究了轮对横移和摇头运动以及曲线半径对独立旋转车轮轮轨蠕滑率的影响情况。
3.This paper studies optimal helicopter flight operations in the event one - engine failure . a three - dimensional point mass with a yawing motion of uh - 60a has been used to study rto and cto from an elevated heliport or from a heliport , a first order dynamic of the oei contingency power is considered . flight after engine failure are formulated as nonlinear optimal control problems
双发及多发直升机单发失效后,直升机飞行所需要的功率由剩余发动机提供,而在某些需要大功率的飞行状态时,如起飞状态、着陆状态等,剩余发动机提供的功率可能满足不了,这就需要对剩余发动机的可用功率进行合理利用。
4.The problem is then fed to a nonlinear programming routine to solve for all parameters . the flight dynamics model with yawing motion of uh - 60a is given , scale factors of state variables and control variables are applied based on the consideration of algorithm convergence . then , the optimization of trajectories is expressed as optimal control problem with a performance index constrained by helicopter performance limits , faa regulation and so on
首先,建立带偏航运动的直升机点质量模型,然后对状态变量和控制变量进行无量纲处理,因为状态变量和控制变量量值相差较大,这使得优化算法收敛效果变差,所以需要选择适当的缩放因子,最后把直升机单台发动机停车后的飞行轨迹表示成一个最优控制问题,即在考虑直升机性能限制和far规范后,指定一个优化性能指标,选择合适的路径约束,然后再解最优控制问题。
Similar Words:
"yawing moment due to rolling velocity" English translation, "yawing moment due to rudder" English translation, "yawing moment due to yawing velocity" English translation, "yawing moment-due-to roll" English translation, "yawing moment-due-to sideslip" English translation, "yawing oscillation" English translation, "yawing oscillations" English translation, "yawing rate" English translation, "yawing rotation" English translation, "yawing stability" English translation