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Synthesis of decoupling laws for attitude stabilization of a spacecraft

โœ Scribed by N. E. Zubov; E. A. Mikrin; M. Sh. Misrikhanov; V. N. Ryabchenko

Book ID
114993133
Publisher
SP MAIK Nauka/Interperiodica
Year
2012
Tongue
English
Weight
298 KB
Volume
51
Category
Article
ISSN
1064-2307

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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
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