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Near-minimum-time control of asymmetric rigid spacecraft using two controls

โœ Scribed by Kim, Donghoon; Turner, James D.


Book ID
124153395
Publisher
Elsevier Science
Year
2014
Tongue
English
Weight
564 KB
Volume
50
Category
Article
ISSN
0005-1098

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๐Ÿ“œ SIMILAR VOLUMES


Attitude stabilization of a rigid spacec
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