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
On the dynamics and control of the relative motion between two spacecraft
โ Scribed by Shaohua Yu
- Publisher
- Elsevier Science
- Year
- 1995
- Tongue
- English
- Weight
- 520 KB
- Volume
- 35
- Category
- Article
- ISSN
- 0094-5765
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