Spacecraft attitude control using magnetic actuators
β Scribed by M. Lovera; A. Astolfi
- Publisher
- Elsevier Science
- Year
- 2004
- Tongue
- English
- Weight
- 646 KB
- Volume
- 40
- Category
- Article
- ISSN
- 0005-1098
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π SIMILAR VOLUMES
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
## Abstract A new attitude control strategy for rotational manoeuvre of an elastic spacecraft is presented. Adaptive sliding mode control with hybrid sliding surface (HSS) is used to minimize the effects of uncertainties, disturbances and the difficulties arising from measurement of flexible dynami