青年中文reentry vehicle的意思
reentry vehicle中文翻譯：
[航]再入飛行器
vehicle───n.車輛；工具；交通工具；運載工具；傳播媒介；媒介物
reentry shock───再入激波
vehicle simulator───車輛模擬器
vehicle type───車型；車輛類型
airless vehicle───無空氣車輛
aerial vehicle───[航]飛行器
vehicle control───[醫]車輛控制
vehicle exhaust───[醫]車輛排氣；汽車廢氣
motor vehicle───汽車；機動車輛；n.機動車輛，摩托車輛; 汽車
optimal guidance law for reentry vehicle with high altitude maneuvering on downward phase is studied.───研究了在降弧段進行高空機動的再入飛行器最優制導律。
Programming maneuvering flight guidance scheme about reentry vehicle is presented in this paper.───種關于再入飛行器程序機動飛行的制導方案。
High temperature chemical non equilibrium phenomena have a great effect on the flow field around a reentry vehicle.───高溫非平衡化學反應對高超聲速再入飛行器繞流流場的氣動熱特性有較大影響。
Variable bend tail concept may be one of the possible approaches for satisfying the maneuvering requirement of hypersonic reentry vehicle.───可變彎尾飛行器的氣動方案是高超聲速機動的潛在可行方案。
Finally, the tracking of the guided angle command for a nominal trajectory of a reentry vehicle is simulated as an example.───本文最后以一再入飛行器為例，對標稱軌道制導指令角的跟蹤進行了仿真。
The shape of ballistic reentry vehicle generally is axial symmetry, but its mass center may be departure from the axis of its symmetry.───彈道式再入飛行器一般為軸對稱旋成體，但其質心可以偏離對稱軸。
A novel guidance law is devised for developing the guidance technology of optimal glide of a hypersonic reentry vehicle.───針對高超聲速再入飛行器最遠距離滑翔制導關鍵技術，設計了一種新型制導律。
A novel three-dimensional(3D) guidance law is proposed for a reentry vehicle with impact angle constraints.───針對再入飛行器帶碰撞角約束的末端導引問題，設計了一種新型三維制導律。
The simulation results have demonstrated that the 3CCGL assures the reentry vehicle to impact the target from a specified direction.───數學仿真結果表明：此制導律能導引再入飛行器沿末端約束方向精確命中目標；
In this paper aerodynamic characteristics of maneuvering reentry vehicle of cruciform configuration and bifurcate configuration are compared by means of the wind tunnel test results.
The estimation state for high velocity reentry vehicle is an important subject in the modern defence.
Finally, some considerations to identify the time - variant parameters for reentry vehicle are also presented.
An optimal guidance law for reentry vehicle with high altitude maneuvering on downward phase is studied.
This paper mainly studies the optimal transition trajectory of a reentry vehicle.
The paper widens the application of local method which used to be utilized in rarefied flow to the quick prediction of aerodynamic characteristics of missile-like reentry vehicle in hypersonic flow.