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Nonlinear attitude control for a rigid spacecraft by feedback linearization

✍ Scribed by Bang, Hyochoong ;Lee, Jung-Shin ;Eun, Youn-Ju


Publisher
Springer-Verlag
Year
2004
Tongue
Korean
Weight
670 KB
Volume
18
Category
Article
ISSN
1226-4865

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Attitude stabilization of a rigid spacec
✍ 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