挠性卫星动力学模型分析及其控制方案研究。
Analysis of flexure dynamics and study of its control method.
将基于滑模控制的自学习模糊控制应用于挠性卫星的姿态稳定控制中。
The self-learning fuzzy control based on sliding mode control is applied to the attitude stabilization of flexible satellites.
从工程角度出发，以具有挠性太阳翼的卫星为背景，着重研究了挠性卫星的智能控制方案。
Intelligent control scheme in view of engineering for flexible space structure was studied such as satellites with solar arrays.
并应用该方法研究了自旋卫星(包括陀螺体卫星)，挠性卫星以及空腔充液卫星的姿态稳定性问题。
Moreover, this method is used for the research on the problems of attitude stability of dual-spinning satellite, the large flexible spacecraft and the satellite with cavity containing fluid.
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。
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.
随着挠性附件的数目的不同，卫星系统的拓扑构型也将有所不同。
Such a system will have different topological configurations if the quantity of flexible appendages is different.
研究了最近提出的非线性自抗扰控制器(adrc)在大挠性多体卫星姿态控制中的应用问题。
The recently developed nonlinear active disturbance rejection controller (ADRC) is applied to attitude control of large flexible multi-body satellite with reaction wheels.
本文研究带四根挠性杆的自旋卫星姿态稳定性问题。
The attitude stability of a spin satellite with four flexible booms is studied in this paper.
研究了最近提出的非线性自抗扰控制器在大挠性多体卫星姿态控制中的应用问题。
The recently developed nonlinear Active Disturbance Rejection Controller (ADRC) was applied to the attitude control of large flexible multi-body satellite with reaction wheels.
文中还讨论了卫星的质量几何和自旋速度，以及挠性杆的几何和弹性性质对姿态稳定性的影响。
The influence of the mass geometry and the spin rate of the satellite, as well as the geometry and the stiffness of the booms on the attitudes…
本文建立了挠性双自旋卫星的姿态稳定性判据。
The attitude stability criteria for dual spinning flexible satellites is presented in this paper.
排在前几位的最终优胜者是：土星的卫星—土卫六，得分为0.64，其次是火星(0.59)以及木星的卫星—木卫二(0.47)，它这被认为拥有一片由潮汐可挠性加热的地下海洋。
The top finisher here was Saturn's moon Titan, which scored 0.64, followed by Mars (0.59) and Jupiter's moon Europa (0.47), which is thought to host a subsurface water ocean heated by tidal flexing.
卫星轨道控制期间，轨道控制推力会激振挠性太阳帆板，从而也影响卫星的姿态。
When the satellite takes orbital maneuver, the control force may stimulate the vibration of the flexible appendages and, therefore, affects the attitude of the satellite.
文中还讨论了卫星的质量几何和自旋速度，以及挠性杆的几何和弹性性质对姿态稳定性的影响。
The influence of the mass geometry and the spin rate of the satellite, as well as the geometry and the stiffness of the booms on the atti…
文中还讨论了卫星的质量几何和自旋速度，以及挠性杆的几何和弹性性质对姿态稳定性的影响。
The influence of the mass geometry and the spin rate of the satellite, as well as the geometry and the stiffness of the booms on the atti…
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