Adaptive set stabilization of the attitude of a rigid spacecraft without angular velocity measurements
โ Scribed by Shihong Ding; Shihua Li; Qi Li
- Book ID
- 107347298
- Publisher
- Academy of Mathematics and Systems Science, Chinese Academy of Sciences
- Year
- 2011
- Tongue
- English
- Weight
- 628 KB
- Volume
- 24
- Category
- Article
- ISSN
- 1009-6124
No coin nor oath required. For personal study only.
๐ SIMILAR VOLUMES
The problem of robust control for the angular velocity of a rigid body subject to external disturbances is addressed. It is shown that if the disturbances are matched there exists a control law attenuating the e ect of the disturbances, whereas in the case of non-matched disturbances no such a feedb
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