Lunar lander的例句大全

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

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

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

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。

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

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

A Novel Lunar Lander with Magnetic Damping of Eddy Current

新型涡流磁阻尼月球着陆器

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

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

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。

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。

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

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。

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

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。

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。

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

Considering that it is very difficult to finish low gravity in simulating landing experiments of lunar lander, the existed low gravitation experiment methods used abroad were studied and compared.

针对月球着陆器模拟着陆试验中低重力实现困难的问题，对国外已有低重力着陆试验方法进行了分析比较。

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。

The size and structure of the Mars probe will be similar to Chang'e-3, China's first lunar lander that was launched in 2013, though there are many differences, he said.

叶培建还透露，尽管有许多不同之处，但是我国火星探测器的大小和结构，与我国于2013年发射的第一个月球着陆器嫦娥三号相似。