Nonlinear predictive control of the small lunar explorer three-axes attitude control using reaction wheels

1、

Collectivity Scheme Design for Modern Small Lunar Explorer

现代小型月球探测器总体方案设计

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2、

China has the scientific research on samples collected by its Chang'e-5 lunar probe.

中国启动嫦娥五号月球探测器所收集样本的科学研究工作。

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3、

Lunar Probe Path Planning Using Case-Based Learning Algorithm

月球探测器路径规划的基于案例的学习算法研究

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4、

Kinematic Analysis of Soft-landing Mechanism for a Lunar Probe in the Deployment Process

月球探测器软着陆机构展开过程的运动学分析

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5、

Study on the Hover Control of the Lunar Probe

月球探测器悬停控制技术的研究

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6、

Soft Landing Optimal Terminal Guidance Strategy of Lunar Probe

月球探测器软着陆最优末制导策略

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7、

China has announced multiple scientific findings from the Chang'e-4 lunar probe.

中国公布了嫦娥四号月球探测器的多项科学发现。

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8、

Algorithms Research on Autonomous Navigation and Control of Lunar Explorer

月球探测器自主导航与控制方法研究

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9、

Navigation for the Lunar Probe Based on Ground Tracking Sites

地面站对月球探测器的导航

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10、

Review of the Development of Soft-landing Mechanisms for Lunar Explorations

月球探测器软着陆机构发展综述

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11、

China has successfully launched its Chang'e 3 lunar probe into orbit.

中国的嫦娥三号月球探测器已经成功进入轨道。

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12、

Reaction Wheels Control for Lunar Probe Attitude Large Angle Slew

月球探测器姿态大角度机动的反作用轮控制

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13、

Autonomous celestial navigation for lunar explorer based on genetic algorithm particle filter

月球探测器天文导航的遗传粒子滤波方法

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14、

Passive Image-based Safe Landing Site Searching and Slope Estimation in Probe Landing

月球探测器着陆中基于被动图像的着陆场搜索及斜坡估计

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15、

It is China's second lunar probe-the first was launched in2007.

本次是中国的第二个月球探测器&第一个于2007年发射。

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16、

A Study of the Guidance and Control Strategy in Lunar Soft-landing

月球探测器软着陆制导控制方法研究

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17、

Optimal Design of Direct Soft-Landing Trajectory of Lunar Prospector

月球探测器直接软着陆最优轨道设计

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18、

Due to a reorganization last year, Brin and co-founder Larry Page now run Alphabet, a holding company that includes the company's "moonshot activities," while Pichai runs Google.

经过去年的重组之后，目前布林和共同创始人拉里·佩奇正在掌控研制“月球探测器”的母公司Alphabet，而皮查伊则负责谷歌业务。

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19、

The lunar trajectories are designed and computed by using the method of genetic algorithms and B plane parameters in this paper. The result shows that the iterations of transfer trajectories are wholly and quickly achieved by combining genetic algorithms with B plane parameters.

通过遗传算法和B平面参数对月球探测器地月转移轨道进行了设计和计算，计算结果表明，结合遗传算法和B平面参数可以很好地解决探月轨道搜索的全局性和快速收敛性问题。

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20、

For the impulse thrusters, the PID control is used to control the height, and then the maintenance of the hover state is realized.

对于脉冲式发动机采用PID控制，实现月球探测器悬停状态的保持。

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