Inclusion of a Redundant Controlling Gyro Cluster Into the Spacecraft Attitude Control System

机译：将冗余控制陀螺仪群集包含到航天器姿态控制系统中

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The method for a rotors spin up and the bringing of redundant controlling gyro cluster to its park state without creation of disturbing torques is suggested and studied. We present the research results on the gyro moment cluster switching on into the attitude control system for a space robot and a land-surveying satellite in sun-synchronous orbit.

机译：提出并研究了一种使转子旋转的方法，并在不产生干扰转矩的情况下将多余的控制陀螺仪簇带到其停车状态。本文介绍了在太阳同步轨道上将陀螺矩簇切换到空间机器人和陆地测量卫星的姿态控制系统中的研究成果。

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《International Conference on Recent Advances in Space Technologies》|2019年|901-906|共6页
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Yevgeny Somov; Sergey Butyrin; Sergey Somov; Tatyana Somova;
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Rotors; Space vehicles; Attitude control; Switches; Quaternions; Satellites; Tuning;

机译：转子;航天器;姿态控制;开关;四元数;卫星;调谐;

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专利

1. Small-time local controllability of spacecraft attitude using control moment gyros [J] . Gui Haichao, Jin Lei, Xu Shijie Automatica . 2015,第Null期

机译：控制力矩陀螺仪对航天器姿态的局部局部可控性
2. Local controllability and stabilization of spacecraft attitude by two single-gimbal control moment gyros [J] . Gui Haichao, Jin Lei, Xu Shijie 中国航空学报（英文版） . 2013,第005期

机译：两个单臂控制力矩陀螺仪对航天器姿态的局部可控性和稳定性
3. A coupled nonlinear spacecraft attitude controller and observer with an unknown constant gyro bias and gyro noise [J] . Thienel J., Sanner R.M. IEEE Transactions on Automatic Control . 2003,第11期

机译：具有未知常数陀螺偏置和陀螺噪声的耦合非线性航天器姿态控制器和观测器
4. Inclusion of a Redundant Controlling Gyro Cluster Into the Spacecraft Attitude Control System [C] . Yevgeny Somov, Sergey Butyrin, Sergey Somov, International Conference on Recent Advances in Space Technologies . 2019

机译：将冗余控制陀螺仪纳入航天器姿态控制系统
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. Fault-Tolerant Attitude Control System for a Spacecraft with Control Moment Gyros Using Multi- Objective Optimization [O] . Ai Noumi, Takuya Kanzawa, Misuzu Haruki, 2015

机译：基于多目标优化的控制力矩陀螺航天器容错姿态控制系统

Inclusion of a Redundant Controlling Gyro Cluster Into the Spacecraft Attitude Control System

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