1、

The experiment results show that the ACLD control strategy and the robust controller can suppress the vibration of the solar array effectively.

实验结果表明所建理论模型是正确的,采用主动约束阻尼控制技术和鲁棒反馈控制器对抑制电池翼的振动是有效的。

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2、

The complication about dynamic analysis connected with the structural characteristics of the solar array was pointed out.

针对该种太阳电池阵的结构特点,指出了动力学分析的复杂性。

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3、

Study on the Block Phenomenon in Solar Array Driving System

太阳帆板驱动中堵转现象的分析

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4、

Thermal Analysis of the Solar Array in the Lunar Orbit

太阳电池阵极月轨道在轨热分析

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5、

The only advice we can offer with respect to suspension is that it should be soft enough to protect the car and solar array from unnecessary jolts and firm enough to provide a stable ride.

唯一的建议,我们可以提供关于暂停是,它应该是软足以保护汽车和太阳能电池阵列不必要的震动和坚定的,足以提供一个稳定的车程。

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6、

Aiming at the characteristics of distributed system and solar array , a photovoltaic generation simulator was designed.

本文针对分布式发电系统的特点和太阳能电池阵列的输出特性, 建立了光伏发电模拟系统.

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7、

The results reveal that solar radiation, control style and solar array obviously affect the floating performance of the airship.

结果表明:太阳辐射、飞艇的控制模式和太阳能电池阵列对其定点性能有较大影响。

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8、

Analysis of Air Flow and Added Mass Induced by Vibration of Solar Array

太阳帆板振动诱导空气流场分析及其附加质量计算

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9、

the kinematics characteristic parameters of the solar array in extending will determine its success extending, also it will affect the satellite's gesture control.

太阳电池阵展开时的运动特性参数,不仅会影响展开的成败,而且也会影响到卫星的姿态控制,为此在地面测试中测量太阳电池阵展开运动特性参数是非常重要的。

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10、

Artist's rendition of solar array.

艺术家演奏的太阳能电池板.

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11、

Taking the rigid solar array as the research object, the controller method is shown to be feasible and effective through the numerical simulation. ( 5) Validating vibration control experiment of the imitational foldaway solar array with ACLD treatments is done.

以太阳能电池翼为研究对象,通过数值仿真验证了控制器设计方法的可行性和有效性。(5)开展了基于主动约束阻尼技术的太阳能电池翼振动控制的验证性实验研究。

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12、

Parameter Sensitivity Analysis for the Solar Array of the Satellite Thermal Design

卫星太阳能电池板热设计参数的灵敏度分析

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13、

With the increasing requirements for high power and high voltage of the spacecraft, the power system of spacecraft has experienced great development in recent years, and the solar array-battery power supply system has been widely used by far.

随着航天器高功率高电压的发展要求,航天器电源系统在近几年中经历了巨大的发展,其中太阳能电池阵&蓄电池电源系统是目前最常用的供电系统。

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14、

The bending of solar array composed of three orthotropic rectangular plate under the lateral forces

三块各向正交异性矩形板构成的卫星帆板在各种载荷下的横向弯曲

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15、

Active vibration control of Large Flexible Solar Array ( LFSA) is a challenging subject in the domain of spacecraft dynamics and control.

大型挠性太阳能电池翼的振动控制是航天器动力学与控制领域的挑战性课题。

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16、

The integrated demonstration system model of large solar array has been produced already. On the base of the sampler, the tests of deployment, main deployment mechanism mode, semi rigidity solar cell panel vibration and two dimension drive mechanism are carried out.

生产出了全尺寸的集成演示样机,进行了展开试验、主展开机构的模态试验,以及半刚性太阳电池板和二自由度驱动机构的振动试验。

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17、

The three-axis attitude stabilization system of the flexible satellite has been studied, in which three basic vibration modes of the solar array have been considered.

在挠性卫星动力学模型的基础上,建立了只考虑太阳帆板三阶振动模态的挠性卫星三轴姿态控制模型。

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18、

Loss model of solar array power caused by rocket motor plume flow contamination

在轨发动机羽流污染导致太阳帆板电功率损失计算模型

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19、

Manned spacecraft launching window and solar array optimum sunshine

载人航天器的发射窗口及太阳能帆板的最佳受晒

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20、

An intelligence control method for realizing PEAK-POWER-TRACKING of a solar array

一种实现太阳阵峰值功率跟踪的智能控制方法

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