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Informational approaches to angular motion control of spacecraft

โœ Scribed by B.N. Petrov; A.B. Krymov; E.I. Mitroshin

Publisher
Elsevier Science
Year
1978
Tongue
English
Weight
270 KB
Volume
5
Category
Article
ISSN
0094-5765

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๐Ÿ“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
โœ Hariharan Krishnan; Mahmut Reyhanoglu; Harris McClamroch ๐Ÿ“‚ Article ๐Ÿ“… 1994 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 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