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Spin-axis stabilization of symmetric spacecraft with two control torques

✍ Scribed by Panagiotis Tsiotras; James M. Longuski


Publisher
Elsevier Science
Year
1994
Tongue
English
Weight
620 KB
Volume
23
Category
Article
ISSN
0167-6911

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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