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Modelling the Attitude Noise of the Gaia Spacecraft. A

✍ Scribed by Ralf Keil; Stephan Theil

Publisher
Springer Netherlands
Year
2010
Tongue
English
Weight
572 KB
Volume
151
Category
Article
ISSN
0038-6308

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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