Design and analysis of a moment control unit for agile satellite with high attitude stability requirement-Reference-Cited by-同舟云学术

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Design and analysis of a moment control unit for agile satellite with high attitude stability requirement

Published:2016-05 Issue: Volume:122 Page:90-105
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Zhang Yao,Li Mou,Song Zhuoyue,Shan Jinjun,Guan Xin,Tang Liang

Funder

National Natural Science Foundation of China, China

Excellent Young Scholars Research Fund of the Beijing Institute of Technology

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference29 articles.

1. Controllability of spacecraft attitude using control moment gyroscopes;Bhat;IEEE Trans. Autom. Control,2009

2. Precision spacecraft pointing using single gimbal control moment gyroscopes with disturbance;Heiberg;J. Guid. Control Dyn.,2000

3. Calculation and fitting of boundaries between elliptic and hyperbolic singularities of pyramid-type control moment gyros;Kojima;Acta Astronaut.,2014

4. Singuarity analysis and steering control laws for adaptive-skew pyramid-type control moment gyros;Kojima;Acta Astronaut.,2013

5. Directional passability and quadratic steering logic for pyramid-typr single gimbal control moment gyros;Yamada;Acta Astronaut.,2014

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