On the solar pressure damping and attitude control
β Scribed by V.J. Modi; W.H.H.J. Lunscher
- Publisher
- Elsevier Science
- Year
- 1983
- Tongue
- English
- Weight
- 825 KB
- Volume
- 10
- Category
- Article
- ISSN
- 0094-5765
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Techniques for synthesizing systems using motor-driven inertia wheels for threedimensional spacecraft attitude control are presented which approximately minimize a quadratic index of performance and compensate for non-linear inter-axis coupling due to the inertia-wheels. Summary--Two techniques are
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