DYNAMICS OF PRECISE GYROMOMENT CONTROL SYSTEMS BY THE LAND-SURVEY SPACECRAFT

机译：土地勘测航天器的精密陀螺仪控制系统动力学

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Gyromoment precise motion control systems of spacecraft (SC) for remote sensing the Earth surface are considered. Elaborated methods for dynamic research of the SC programmed angular motion at principle modes under external, structural and parametric disturbances, partial discrete measurement of the state and digital control of the gyro moment cluster (GMC) by the minimum-excessive gyrodine scheme, are presented.

机译：考虑了用于遥感地球表面的航天器（SC）的陀螺仪精密运动控制系统。提出了在外部，结构和参数扰动下的原理模式下的SC编程角运动的动态研究，通过最小过量的陀螺仪方案对状态进行部分离散测量以及对陀螺力矩簇（GMC）进行数字控制的动态研究方法。

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来源
《Saint Petersburg International Conference on Integrated Navigation Systems; 20040524-26; Saint Petersburg(RU)》|2004年|P.289-290|共2页
会议地点 Saint Petersburg(RU)
作者
G.P. Anshakov; Ye.I. Somov; S.A. Butyrin;
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作者单位

State Research Production Rocket-Space Center 'TsSKB-PROGRESS', Federal Space Agency 18 Pskovskaya Str. Samara 443009 Russia;

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会议组织
原文格式 PDF
正文语种 eng
中图分类无线电导航;
关键词
spacecraft; gyromoment control; dynamics;

机译：航天器;转角控制;动力学;

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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. Impulsive controllability of linear dynamical systems with applications to maneuvers of spacecraft [J] . XinzhiLiu, Allan R.Willms Mathematical Problems in Engineering: Theory, Methods and Applications . 1996,第4期

机译：线性动力系统的脉冲可控性及其在航天器操纵中的应用
3. Investigation of the dynamics of angular motion and construction of algorithms for controlling the angular momentum of spacecraft using a magnetic attitude control system [J] . Egorov Yu. G., Kulkov V. M., Terentyev V. V., Doklady. Physics . 2016,第11期

机译：角运动动力学的研究和使用磁姿态控制系统控制航天器角动量的算法的构建
4. Precision gyromoment attitude control systems of rapid manoeuvring spacecrafts for remote sensing and land-survey [C] . Anshakov, G.P., Antonov, . 1994

机译：快速机动航天器的精密陀螺姿态控制系统，用于遥感和土地测量
5. Investigation of the crossed flexure pivot and the dynamics of the momentum management system spacecraft control component and the dynamically tuned gyroscope. [D] . Cain, Jeffrey Stuart. 1999

机译：研究交叉弯曲枢轴，动量管理系统，航天器控制组件和动态调谐陀螺仪的动力学。
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. Impulsive controllability of linear dynamical systems with applications to maneuvers of spacecraft [O] . Xinzhi Liu, Allan R. Willms 1996

机译：线性动力系统的脉冲可控性及其在航天器机动中的应用

DYNAMICS OF PRECISE GYROMOMENT CONTROL SYSTEMS BY THE LAND-SURVEY SPACECRAFT

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