reentry vehicle
美 
英
- un.重返大气层飞行器
- 网络再入飞行器；再入目标；和子弹头
英汉解释
例句
Variable bend tail concept may be one of the possible approaches for satisfying the maneuvering requirement of hypersonic reentry vehicle.
可变弯尾飞行器的气动方案是高超声速机动的潜在可行方案。
Finally, the tracking of the guided angle command for a nominal trajectory of a reentry vehicle is simulated as an example.
本文最后以一再入飞行器为例，对标称轨道制导指令角的跟踪进行了仿真。
The shape of ballistic reentry vehicle generally is axial symmetry, but its mass center may be departure from the axis of its symmetry.
弹道式再入飞行器一般为轴对称旋成体，但其质心可以偏离对称轴。
A novel guidance law is devised for developing the guidance technology of optimal glide of a hypersonic reentry vehicle.
针对高超声速再入飞行器最远距离滑翔制导关键技术，设计了一种新型制导律。
A novel three-dimensional(3D) guidance law is proposed for a reentry vehicle with impact angle constraints.
针对再入飞行器带碰撞角约束的末端导引问题，设计了一种新型三维制导律。
The simulation results have demonstrated that the 3CCGL assures the reentry vehicle to impact the target from a specified direction.
数学仿真结果表明：此制导律能导引再入飞行器沿末端约束方向精确命中目标；
Learning Classifier System and Its Application to the Aerodynamic Shape Optimization of Reentry Vehicle
自适应分类器系统及其在再入飞行器气动布局优化中的应用
Numerical simulation of hypersonic flow field around the reentry vehicle
再入三维高超声速粘性流场的数值模拟
aerodynamic prediction and analysis for a reentry vehicle with slice - ailerons
配平翼飞行器的气动计算及分析
Aerodynamics prediction and configuration optimization for reentry vehicle with double-ellipse cross-section
双椭圆截面再入飞行器的气动计算及布局优化设计
Initial Guidance Law of Closed-form Neural Network for Maneuverable Reentry Vehicle
机动再入飞行器神经网络闭路初制导研究
Numerical studies of non-equilibrium flow-fields over a capsule-type hypersonic reentry vehicle
带座舱飞船高超声速再入非平衡流场的数值研究
Response Analysis and Experimental Verification for Reentry Vehicle Shell Subjected to Aerodynamic Noise
再入飞行器壳体气动噪声响应分析和试验验证
Response Analysis and Experimental Verification for Reentry Vehicle Subjected to Aerodynamic Noise
再入飞行器的气动噪声响应分析和试验验证
Improving Design of Reentry Vehicle Trajectory Optimization Using Direct Collocation Method
基于直接配点法的再入轨迹优化设计
Guidance Law of Reentry Vehicle with Terminal Angular Constraint
再入飞行器的终端角度约束制导律设计
Optimum Design and Simulation on Multiple Independently Targeted Reentry Vehicle's Ballistic Program
多弹头导弹分导程序优化设计与仿真
Attitude Control System Design of the Maneuverable Reentry Vehicle for Variable Target
可变落点的再入机动飞行器姿控系统设计
Application of fuzzy multiple-attribute decision for evaluating the reentry vehicle's system design
再入飞行器总体方案评估中模糊多属性决策的应用
Numerical Simulation of Unsteady Transonic Flow around a Free Oscillating Reentry Vehicle
返回舱自由振动跨声速非定常流场数值模拟
De-Orbit Operations Study of Lifting Reentry Vehicle
升力式再入飞行器离轨制动研究
A Prediction Guidance Algorithm for the Maneuvering Reentry Vehicle
机动再入飞行器的一种预测制导方法
Study on Random Vibration Response Analysis of Reentry Vehicle Complex Structure
再入飞行器复杂结构随机振动响应分析研究
Research of the Optimal Deceleration Speed of the Reentry Vehicle
再入飞行器最优减速研究
Software System Design of Reentry Vehicle Six- DOF Semi Physical Simulation
再入体六自由度半实物仿真软件系统设计
The Sub-optimal Prediction Guidance Algorithm for the Reentry Vehicle Based on the Gauss Equation
基于高斯问题的近最优再入预测制导方法研究
An Optimal High-altitude Guidance Law for Reentry Vehicle
再入飞行器高空最优制导律
A Method for Mass Distribution of Reentry Vehicle
一种再入飞行器质量指标分配的方法
