STEERING THE SPACECRAFT CONTROL MOMENT GYROSCOPE CLUSTERS

机译：转向航天器控制力矩陀螺仪集群

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Contemporary tendencies on methods for control of the Gyro Moment Clusters (GMCs) based on the single gimbal control moment gyroscopes (gyrodines) are considered. The GMCs are principle executive devices of the spacecraft (SC) attitude control systems. Different schemes for 4 or 6 gyrodines' arrangement on the SC body, the GMCs tuning laws and the gyrodine control algorithms are analyzed. New methods for forming the GMCs control laws and steering are suggested. These methods are based on the explicit analytical relations and allow efficiently predicting realizability of the SC planned angular motion directly onboard. Problems of the MGC dynamics at the SC attitude control, and also ways for supporting their fault tolerance and reliability, are considered.

机译：考虑了基于单云台控制力矩陀螺仪（陀螺仪）的陀螺力矩簇（GMC）控制方法的当代趋势。 GMC是航天器（SC）姿态控制系统的主要执行设备。分析了SC车体上4或6个gyrodine的不同布置方案，GMC调谐规律和gyrodine控制算法。提出了形成GMC控制律和操纵的新方法。这些方法基于显式分析关系，可直接在船上有效预测SC计划角运动的可实现性。考虑了SC姿态控制中MGC动力学的问题，以及支持其容错性和可靠性的方法。

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来源
《Saint Petersburg International Conference on Integrated Navigation Systems; 20030526-28; St.Petersburg(RU)》|2003年|P.403-419|共17页
会议地点 St.Petersburg(RU)
作者
Ye.I. Somov; S.A. Butyrin; A.V. Sorokin; V.N. Platonov;
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作者单位

State Research Institute of Mechanical Systems Reliability 244 Molodogvargeyeskaya Str. Samara 443100 Russia;

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会议组织
原文格式 PDF
正文语种 eng
中图分类导航设备;
关键词
spacecraft; control moment gyros;

机译：航天器;控制力矩陀螺仪;

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专利

1. Potential approach for constrained autonomous manoeuvres of a spacecraft equipped with a cluster of control moment gyroscopes [J] . G Avanzini, G Radice, I Ali Proceedings of the Institution of Mechanical Engineers . 2009,第g3期

机译：配备控制力矩陀螺仪群的航天器的受限自主操纵的潜在方法
2. Potential approach for constrained autonomous manoeuvres of a spacecraft equipped with a cluster of control moment gyroscopes [J] . G Avanzini, G Radice, I Ali Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering . 2009,第3期

机译：配备控制力矩陀螺仪群的航天器的受限自主操纵的潜在方法
3. A new steering law for redundant control moment gyroscope clusters [J] . Ozan Tekinalp, Emre Yavuzoglu Aerospace science and technology . 2005,第7期

机译：冗余控制力矩陀螺仪群的新转向定律
4. STEERING THE CONTROL MOMENT GYROSCOPE CLUSTERS ONBOARD HIGH-AGILE SPACECRAFT [C] . Ye.I. Somov, V.N. Platonov, A.V. Sorokin IFAC Symposium on Automatic Control in Aerospace . 2005

机译：转向控制力矩陀螺仪在船上高敏捷的航天器
5. A novel integrated spacecraft attitude control system using variable speed control moment gyroscopes: A Lyapunov-based approach [D] . Kim, Dohee. 2011

机译：使用变速控制力矩陀螺仪的新型集成航天器姿态控制系统：基于李雅普诺夫的方法
6. Design and Simulation of a MEMS Control Moment Gyroscope for the Sub-Kilogram Spacecraft [O] . Honglong Chang, Wenlong Jiao, Qianyan Fu, 2010

机译：亚公斤级航天器的MEMS控制力矩陀螺仪的设计与仿真
7. Controllability of spacecraft attitude using Control Moment Gyroscopes [O] . BHAT SP, TIWARI PK 2009

机译：使用控制力矩陀螺仪控制航天器姿态
8. Approach to CMG (Control Moment Gyroscopes) Steering Using Feedback Linearization. [R] . dzielski, j. bergmann, e. 1988

机译：用反馈线性化方法研究CmG（控制力矩陀螺仪）转向。

STEERING THE SPACECRAFT CONTROL MOMENT GYROSCOPE CLUSTERS

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