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
β¦ LIBER β¦
Nonlinear attitude control of flexible spacecraft under disturbance torque
β Scribed by Sahjendra N. Singh
- Publisher
- Elsevier Science
- Year
- 1986
- Tongue
- English
- Weight
- 553 KB
- Volume
- 13
- Category
- Article
- ISSN
- 0094-5765
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