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A frequency domain solution for the linear attitude-control problem of spacecraft with flexible appendages

机译：具有柔性附件的航天器线性姿态控制问题的频域解

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摘要

Linear interaction problem between spacecraft attitude control and flexible appendages solved in frequency domain using Fourier transform

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作者
Trubert, M. R.;
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年度 1970
页码 1-40
总页数 40
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
ATTITUDE CONTROL; FLEXIBLE BODIES; FOURIER TRANSFORMATION; SPACECRAFT STRUCTURES; EQUATIONS OF MOTION; SOLAR CELLS; SPACECRAFT ANTENNAS; STRUCTURAL VIBRATION;

机译：态度控制;灵活的身体;傅里叶变换;航天器结构;运动方程;太阳能电池;航天器天线;结构振动;

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专利

1. Design of Adaptive Feedback Linearization Control for Spacecraft with Flexible Appendages using Model Estimator [J] . Jinli Chen, Donghai Li, Wenxiao Shan, Neural, Parallel & Scientific Computations . 2007,第3期

机译：基于模型估计器的柔性附件航天器自适应反馈线性化控制设计
2. Nonlinear vibration phenomenon of maneuvering spacecraft with flexible jointed appendages [J] . Wei Jin, Cao Dengqing, Huang Hua Nonlinear dynamics . 2018,第4期

机译：具有柔性连接阑尾的非线性振动现象
3. Nonlinear Dynamic Modeling for a Flexible Laminated Composite Appendage Attached to a Spacecraft Body Undergoing Deployment and Locking Motions [J] . You Bin Di, Wen Jian Min, Zhang Guang Yu, Journal of aerospace engineering . 2016,第5期

机译：进行展开和锁定运动的附着在航天器主体上的柔性叠层复合附件的非线性动力学建模
4. Dynamic feedback linearization control of spacecraft with flexible appendages based on extended state observer [C] . CHEN Jinli, LI Donghai, SUN Xianfang International Symposium on Instrumentation and Control Technology; 20061013-15; Beijing(CN) . 2006

机译：基于扩展状态观测器的带有柔性附件的航天器动态反馈线性化控制
5. Applications of global seismic tomography and analysis of variational methods for the solution of the linearly attenuating frequency-domain wave equation. [D] . Johnson, Stuart George. 1997

机译：整体地震层析成像技术的应用和变分方法分析，用于线性衰减频域波动方程的求解。
6. Methods of EEG Signal Features Extraction Using Linear Analysis in Frequency and Time-Frequency Domains [O] . Amjed S. Al-Fahoum, Ausilah A. Al-Fraihat 2014

机译：频域和时域线性分析的脑电信号特征提取方法
7. Time- and frequency-domain subspace identification of a nonlinear spacecraft [O] . Noël, Jean-Philippe, Marchesiello, Stefano, Kerschen, Gaëtan 2012

机译：非线性航天器的时域和频域子空间识别
8. A Frequency Domain Solution for the Linear Attitude-Control Problem of Spacecraft with Flexible Appendages [R] . Trubert, M. R. 1970

机译：具有柔性附件的航天器线性姿态控制问题的频域解

A frequency domain solution for the linear attitude-control problem of spacecraft with flexible appendages

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