reentry vehicle的例句大全

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。

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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。

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de-orbit operations study of lifting reentry vehicle

升力式再入飞行器离轨制动研究

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The estimation state for high velocity reentry vehicle is an important subject in the modern defence.

高速再入飞行器的状态估计是现代国防研究中的重要课题.

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MIRV ( multiple independently targeted reentry vehicle )

多弹头分导再入飞行器 ( 多弹头导弹 )

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The guidance method satisfies terminal angular constraint as reentry vehicle hitting target, but also ensures minimum loss of maneuvering velocity for reentry vehicle.

该方法利用最优控制理论的思想方法，不仅使飞行器命中目标时满足了终端角度约束的条件，而且保证了再入飞行器机动速度损失最小。

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Research on the dynamic stability of an orbital reentry vehicle in pitching

飞船返回舱俯仰振荡的动态稳定性研究

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According to the strength characteristic on the multiple independently targeted reentry vehicle ( MITRV) during different stage, establish RV stage and warhead's unpowered ballistic model under launch coordinate on basis of control coefficient, then calculate it in the way of VC++ 6.0 program.

根据分导式多弹头导弹母舱在分导段和被动段的飞行受力特点，建立了母舱、子弹头在发射坐标系下基于开关系数的弹道模型，利用VC对所建模型进行了仿真计算。

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The Design of Flight Control Semi-physical Simulation System for Maneuver Reentry Vehicle

机动再入体飞行控制半实物仿真系统设计

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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

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Study on Thermal Peak, Maximum Overload and Dynamic Pressure Peak during Reentry Flight of Common Aero Vehicle

通用航空飞行器再入大气的热流峰值、最大过载和动压峰值研究

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The objective of this paper is to design the reentry flight control laws for the Suborbital Reusable Launch Vehicle ( SRLV) based on nonlinear dynamic-inversion.

基于非线性动态逆理论，设计了亚轨道可重复使用运载器（SRLV）的再入控制律。

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The aerodynamic performance of a tandem two-stage-to-orbit ( TSTO) reusable launch vehicle ( RLV) and its reentry orbiter are studied through employing computational fluid dynamic ( CFD) method.

应用CFD方法研究了两级重复使用运载器上升段和轨道器再入段的气动性能。

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Research on Modeling and Dynamic Simulation of Unmanned Aerospace Vehicle Reentry Trajectory Optimization for Manned Deep Space Exploration

空天无人飞行器的建模及其动态仿真研究载人航天器深空飞行返回再入轨迹优化

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