๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

Nonlinear Attitude Tracking Control of a Spacecraft with Thrusters Based on Error Quaternions

โœ Scribed by Wu-xing JING; Shi-jie XU


Book ID
114335301
Publisher
Elsevier Science
Year
2002
Tongue
English
Weight
302 KB
Volume
15
Category
Article
ISSN
1000-9361

No coin nor oath required. For personal study only.


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