文章详细信息 关键词： 挠性卫星;;姿态控制;;智能控制;;神经网络 [gap=837]Keywords: flexible satellites;attitude control;intelligent control;neural networks
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flexible satellite platform 柔性卫星平台
flexible satellite attitude control 柔性卫星姿态控制
flexible satellite experimental instrument 挠性卫星实验装置
flexible multi-body satellite 挠性多体卫星的
The attitude control for large angle maneuver of flexible satellite requires the satellite can follow the given angle quickly. Meanwhile,vibration of solar panel caused by maneuver of the satellite is expected to be low.
挠性卫星大角度机动姿态控制要求卫星能够较快地机动到给定位置,同时要求由卫星机动引起的帆板振动强度尽可能地小。
参考来源 - 多目标进化算法在卫星姿态控制中的应用·2,447,543篇论文数据，部分数据来源于NoteExpress
Models of the three-axis stabilized Attitude Control Systems of a rigid satellite and a flexible satellite with a pair of solar arrays are set up.
本论文分别以三轴稳定刚性卫星姿态控制和带太阳帆板的三轴稳定卫星姿态控制为研究对象，建立了控制系统数学模型。
To solve the attitude maneuver of a flexible satellite, this article presents a variable structure tracking control algorithm based on output feedback.
为解决柔性航天器姿态机动的控制问题，给出了基于输出反馈的变结构跟踪控制算法。
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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