lunar lander

Experimental researches on buffer characteristics of lunar lander with three legs

三支撑月球着陆器缓冲性能试验研究

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State-jump Semi-active Control of Lunar Lander Soft Landing

月球着陆器软着陆状态跳跃半主动控制

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The results show that the buffer effectiveness is very good for the novel lunar lander with magnetic damping of eddy current.

结果表明，新型涡流磁阻尼月球着陆器具有较好的缓冲效果。

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Metal rubber was used in a principle model machine of Lunar Lander at first as a damping element with elastic behavior.

金属橡胶作为一种有弹性的阻尼元件首次用在月球着陆器原理样机中。

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Compared with a certain type of passive lunar lander, the semiactive control is analyzed.

通过与某型被动控制的着陆器进行对比分析，研究了半主动控制。

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Research of the Buffering Capability for the Aluminum Honeycomb Component on the Lunar Lander

月球着陆器铝蜂窝元件缓冲性能实验装置研究

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A Novel Lunar Lander with Magnetic Damping of Eddy Current

新型涡流磁阻尼月球着陆器

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Design of impact isolating landing legs for microminiature lunar lander

微小型月球着陆器冲击隔离着陆腿研究

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The larger of the two will loft the lunar lander and other equipment into Earth orbit.

两者中较大的一个将发射月球着陆器和其它的设备进入地球轨道。

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By the modal analysis of lunar lander based on MSC.

以某型号着陆器软着陆机构为研究对象，采用MSC。

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Based on ADAMS mechanical simulation software, a microgravity environment was established by computer and some simulation study had been carried out about the lunar lander.

在机械仿真软件ADAMS基础上，用计算机建立了月球微重力环境并进行了数字仿真。

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Development of Soft Landing for Lunar Lander

月球软着陆系统关键技术研究与发展综述

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Experimental Researches on Impact Characteristics of Damping Materials used in Lunar Lander

月球着陆器用阻尼材料冲击性能试验

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This paper mainly introduces the new crew exploration vehicle, the lunar lander and the shuttle-derived launch vehicles for returning to the moon.

介绍执行美国重返月球计划的新型载人探测飞行器、月球登陆器以及航天飞机衍生型运载火箭；

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Touchdown Stability Simulation of Landing Gear System for Lunar Lander

月球着陆器软着陆机构着陆稳定性仿真分析

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The most impressive spaceship ever, I believe, was a Grumman Lunar Lander.

史上最震撼人心的宇宙飞船，我相信，是格鲁曼公司（Grumman）所做的登月艇。

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The Design of Lunar Lander Attitude Control System based on Variable Structure Control with Sliding Mode

滑模变结构控制的月球着陆舱姿态控制系统设计

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A formula concerning the upper limit amplitude of the lunar lander is obtained from theoretical analysis.

基于能量原理和振动理论，通过理论推导得出了月球着陆器上限振幅值计算公式。

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To improve the analysis accuracy of soft landing impact response for lunar lander, a method based on nonlinear transient dynamic analysis was presented.

为提高分析月球着陆器软着陆有效载荷着陆冲击响应的准确性，提出一种基于瞬态动力学的着陆器有效载荷软着陆冲击响应分析方法。

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The sample application simulates the control technology for an unmanned Lunar Lander module.

示例应用程序模拟了无人值守的Lunar Lander登月舱的控制技术。

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Upper limit amplitude of lunar lander based on ADAMS software

基于ADAMS平台的月球着陆器上限振幅研究

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Executives say they will buy existing rockets and capsules for the launches, developing new spacesuits and a lunar lander.

高官们说他们将购买现存火箭和太空舱用以发射，并开发新式航天服和登月飞行器。

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The new lunar lander will be similarly improved, with updated electronics and materials.

新的月球着陆器将被同样地加以改进，使用最新的电子仪器设备和原料。

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The dynamic response of a lunar lander to the impact of the surface of the Moon with damp is analyzed using the energy principle and vibration theory.

对月球着陆器撞击月面时产生的冲击振动等动力学响应进行了仿真研究。

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Experimental investigation are carried out for Buffer characteristics of homemade principle models of the lunar lander with magnetic damping of eddy current.

自制了涡流磁阻尼月球着陆器原理模型，对其缓冲性能进行了试验研究。

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As the study of outer space exploration develops, a lunar lander with high safety and multifunction is necessary.

随着人类对地球以外空间探测技术研究的逐步深入，对着陆器的设计要求越来越高，一台具有高安全性、多功能的着陆器是必不可少的。

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Experimental investigation on mechanical property of metal rubber used in Lunar Lander in high or low temperature

月球着陆器用金属橡胶高低温力学性能试验研究

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An Experimental Method for Simulating Lunar Lander Low Gravitation Landing

一种模拟月球着陆器低重力着陆试验方法

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Honeycomb as a new type of a material have an extensive practice in soft landing of lunar Lander.

铝蜂窝缓冲器是月球探测器软着陆机构常用缓冲装置。

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All the researchs indicate that it is feasible to apply the honeycomb buffer and the MR buffer on the lunar lander.

上述研究表明：蜂窝材料缓冲器和磁流变缓冲器在登陆器上的应用是可行的。

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