reentry vehicle

reentry vehicle

美 　英

• un.重返大氣層飛行器
• 網絡再入飛行器；再入目標；和子彈頭

英漢解釋

un.	1. 重返大氣層飛行器

例句

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；

Learning Classifier System and Its Application to the Aerodynamic Shape Optimization of Reentry Vehicle

自適應分類器系統及其在再入飛行器氣動布局優化中的應用

Numerical simulation of hypersonic flow field around the reentry vehicle

再入三維高超聲速粘性流場的數值模擬

aerodynamic prediction and analysis for a reentry vehicle with slice - ailerons

配平翼飛行器的氣動計算及分析

Aerodynamics prediction and configuration optimization for reentry vehicle with double-ellipse cross-section

雙橢圓截面再入飛行器的氣動計算及布局優化設計

Initial Guidance Law of Closed-form Neural Network for Maneuverable Reentry Vehicle

機動再入飛行器神經網絡閉路初制導研究

Numerical studies of non-equilibrium flow-fields over a capsule-type hypersonic reentry vehicle

帶座艙飛船高超聲速再入非平衡流場的數值研究

Response Analysis and Experimental Verification for Reentry Vehicle Shell Subjected to Aerodynamic Noise

再入飛行器殼體氣動噪聲響應分析和試驗驗證

Response Analysis and Experimental Verification for Reentry Vehicle Subjected to Aerodynamic Noise

再入飛行器的氣動噪聲響應分析和試驗驗證

Improving Design of Reentry Vehicle Trajectory Optimization Using Direct Collocation Method

基于直接配點法的再入軌跡優化設計

Guidance Law of Reentry Vehicle with Terminal Angular Constraint

再入飛行器的終端角度約束制導律設計

Optimum Design and Simulation on Multiple Independently Targeted Reentry Vehicle's Ballistic Program

多彈頭導彈分導程序優化設計與仿真

Attitude Control System Design of the Maneuverable Reentry Vehicle for Variable Target

可變落點的再入機動飛行器姿控系統設計

Application of fuzzy multiple-attribute decision for evaluating the reentry vehicle's system design

再入飛行器總體方案評估中模糊多屬性決策的應用

Numerical Simulation of Unsteady Transonic Flow around a Free Oscillating Reentry Vehicle

返回艙自由振動跨聲速非定常流場數值模擬

De-Orbit Operations Study of Lifting Reentry Vehicle

升力式再入飛行器離軌制動研究

A Prediction Guidance Algorithm for the Maneuvering Reentry Vehicle

機動再入飛行器的一種預測制導方法

Study on Random Vibration Response Analysis of Reentry Vehicle Complex Structure

再入飛行器復雜結構隨機振動響應分析研究

Research of the Optimal Deceleration Speed of the Reentry Vehicle

再入飛行器最優減速研究

Software System Design of Reentry Vehicle Six- DOF Semi Physical Simulation

再入體六自由度半實物仿真軟件系統設計

The Sub-optimal Prediction Guidance Algorithm for the Reentry Vehicle Based on the Gauss Equation

基于高斯問題的近最優再入預測制導方法研究

An Optimal High-altitude Guidance Law for Reentry Vehicle

再入飛行器高空最優制導律

A Method for Mass Distribution of Reentry Vehicle

一種再入飛行器質量指標分配的方法