NONLINEAR DYNAMICS OF GYROMOMENT ATTITUDE CONTROL AND PRECISE ANTENNA POINTING BY THE SESAT SPACECRAFT

机译：芝麻姿态控制的非线性动力学和塞萨斯航天器指向的精确天线

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New research and developments on attitude determination, nonlinear dynamics of precise gyromoment control and antenna pointing by the GEO communication spacecraft Sesat developed by Russian State Space Research & Production Association Applied Mechanics (NPO PM) in cooperation with Alcatel Space Industries (ASI, France) on the order of Eutelsat, are presented.

机译：俄罗斯国立空间研究与生产协会应用力学（NPO PM）与阿尔卡特航天工业（ASI，法国）合作，对俄罗斯国家空间研究与生产协会应用机械（NPO PM）开发的精确旋转控制和天线的非线性动力学的新研究与开发研究提出了Eutelsat的顺序。

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《IFAC Symposium on Automatic Control in Aerospace》|2001年||共6页
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G.P. Titov; Ye.I. Somov; V.A. Rayevsky; A.V. Ovtchinnikov; A. Baiget; R.C. Rogers; International Federation of Automatic Control; null;
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中图分类 V1-53;
关键词
attitude determination; gyromoment control; dynamics; fault tolerance;

机译：姿态确定;旋转控制;动态;容错;

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1. Fault Tolerant Gyromoment Control of Information Spacecraft with Fine Pointing of Large-scale Antennas ? [J] . Ye. Somov, V. Rayevsky, G. Titov, IFAC PapersOnLine . 2015,第9期

机译：具有大型天线精确指向的信息航天器的容错陀螺控制？ < / ce：交叉引用>
2. Spacecraft Nonlinear Attitude Dynamics Control with Adaptive Neuro-Fuzzy Inference System [J] . Tamer Mekky Ahmed Habib International review of automatic control . 2019,第5期

机译：与自适应神经模糊推理系统的航天器非线性姿态动力学控制
3. Spacecraft Attitude Stabilization Using Nonlinear Delayed Multiactuator Control and Inverse Dynamics [J] . Morad Nazari, Eric A. Butcher, Hanspeter Schaub Journal of guidance, control, and dynamics . 2013,第5期

机译：非线性延迟多执行器控制和逆动力学的航天器姿态稳定
4. NONLINEAR DYNAMICS OF GYROMOMENT ATTITUDE CONTROL AND PRECISE ANTENNA POINTING BY THE SESAT SPACECRAFT [C] . G.P. Titov, Ye.I. Somov, V.A. Rayevsky, 15th IFAC Symposium on Automatic Control in Aerospace 2001, Sep 2-7, 2001, Bologna/Forli, Italy . 2001

机译：SESAT航天器对陀螺姿态姿态控制和精确天线指向的非线性动力学
5. Nonlinear observer/controller designs for spacecraft attitude control systems with uncalibrated gyros. [D] . Thienel, Julie K. 2004

机译：具有未校准陀螺仪的航天器姿态控制系统的非线性观察器/控制器设计。
6. Finite-Time Attitude Stabilization Adaptive Control for Spacecraft with Actuator Dynamics [O] . Chunbao Wang, Dong Ye, Zhongcheng Mu, 2019

机译：具有执行器动力学的航天器航天器的有限时间态度稳定控制
7. Agile and Precise Attitude Switching Maneuver of Flexible Spacecraft based on Nonstationary Frequency-Shaped Robust Control [O] . Ryota IKEDA, Masaki TAKAHASHI 2011

机译：基于非间断频率形状鲁棒控制的柔性航天器敏捷和精确姿态切换机动

NONLINEAR DYNAMICS OF GYROMOMENT ATTITUDE CONTROL AND PRECISE ANTENNA POINTING BY THE SESAT SPACECRAFT

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