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
โฆ LIBER โฆ
Dynamic stability of a flexible spacecraft in the presence of nonlinear resonances
โ Scribed by I. N. Zharikov; V. S. Khoroshilov
- Publisher
- Springer US
- Year
- 1992
- Tongue
- English
- Weight
- 409 KB
- Volume
- 28
- Category
- Article
- ISSN
- 1573-8582
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