Attitude stabilization of a rigid spacec
✍
Hariharan Krishnan; Mahmut Reyhanoglu; Harris McClamroch
📂
Article
📅
1994
🏛
Elsevier Science
🌐
English
⚖ 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