这个实验将以十一月的模拟着陆作为结束。
The experiment is due to finish with a mock landing in November.
受过良好训练的战士在模拟装置上进行跳伞练习，完全模仿跳伞过程(尤其是脱离飞机并着陆的过程)。
While the better trained soldiers practise a parachute jump in a simulator which perfectly imitates the jump (especially the moment of leaving the aircraft and landing).
在对着陆缓冲装置进行分类的基础上，给出了在地球表面模拟微重力的几种常用方法。
On the basis of classifying the buffering devices of the space lander, a few of common ways to simulate micro gravity on the Earth surface are presented.
而计算多体系统动力学和虚拟样机技术的出现，使得对于飞机着陆过程起落架和机身动态响应的模拟更逼近于现实。
Computational multibody dynamics and virtual prototyping technology are brand new modeling and analysis methods for simulating the landing process of an aircraft.
在实验室模拟条件下，研究着陆冲击力与着陆冲击时间的关系。
Under simulated condition in laboratory the relationship between landing impact force and landing impact time was studied.
机舱容积只有五百五十立方米，要有医疗，睡眠，着陆，储藏，和表面模块等模拟功能和设备。
The capsule included medical, sleeping, landing, storage and surface modules with a total interior space of only 550 cubic meters.
在正弦风切变假定下，利用计算机计算和飞行模拟器模拟研究了长周期振动频率上下的正弦波风切变对飞机着陆航迹的影响。
On the assumption that the wind shear is sinusoidal, the effects of long periodic oscillation on the landing path of an aircraft were studied by computer calculation and with flight simulator.
使用上述模型，分别进行了主起落架落震仿真试验和全机着陆仿真试验，用以模拟真实的起落架落震和全机着陆情况，并将二者得到的主起落架仿真结果进行了对比。
The above models are used to simulate the dropping test of the main landing gear and landing test of the aircraft. The two results have a good correspondence.
介绍自行研制的用于模拟航天器着陆的撞击试验装置和测试系统。
The paper introduces a kind of simulation test equipment of the mash screen.
针对电传控制增稳飞机进行了进场着陆的飞行品质地面模拟试验研究。
The studies of flying qualities during approach to landing for the fly—by—wire aircraft with control and augmented system were conducted on a fixed—base flying quality simulator in this paper.
本文针对某型着陆装备着陆要求和指标，以双气室缓冲气囊为对象，开展了着陆缓冲气囊缓冲过程数值模拟分析与优化设计研究。
Numerical simulation and optimal design of the process of double-chamber airbag landing are studied aimed at landing requirement of the landing equipment.
本文针对某型着陆装备着陆要求和指标，以双气室缓冲气囊为对象，开展了着陆缓冲气囊缓冲过程数值模拟分析与优化设计研究。
Numerical simulation and optimal design of the process of double-chamber airbag landing are studied aimed at landing requirement of the landing equipment.
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