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Attitude control of a rigid spacecraft with one variable-speed control moment gyro

✍ Scribed by Gui, Hai-Chao; Jin, Lei; Xu, Shi-Jie

Book ID
125354459
Publisher
The Chinese Society of Theoretical and Applied Mechanics; Institute of Mechanics, Chinese Academy of Sciences
Year
2013
Tongue
English
Weight
446 KB
Volume
29
Category
Article
ISSN
0567-7718

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Attitude stabilization of a rigid spacec
Attitude stabilization of a rigid spacecraft using two control torques: A nonlinear control approach based on the spacecraft attitude dynamics
✍ Hariharan Krishnan; Mahmut Reyhanoglu; Harris McClamroch πŸ“‚ Article πŸ“… 1994 πŸ› Elsevier Science 🌐 English βš– 501 KB

The attitude stabilization problem of a rigid spacecraft using control torques supplied by gas jet actuators about only two of its principal axes is considered. If the uncontrolled principal axis of the spacecraft is not an axis of symmetry, then the complete spacecraft dynamics are small time local