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Stabilization and utilization of nonlinear phenomena based on bifurcation control for slow dynamics

✍ Scribed by Hiroshi Yabuno

Publisher
Elsevier Science
Year
2008
Tongue
English
Weight
558 KB
Volume
315
Category
Article
ISSN
0022-460X

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πŸ“œ SIMILAR VOLUMES

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