We construct explicit time-varying feedbacks that locally asymptotically stabilize the attitude of a rigid spacecraft with two controls.
The explicit synthesis of stabilizing (time optimal) feedback controls for the attitude control of a rotating satelite
β Scribed by Henry Hermes; David Hogenson
- Publisher
- Elsevier Science
- Year
- 1985
- Tongue
- English
- Weight
- 429 KB
- Volume
- 16
- Category
- Article
- ISSN
- 0096-3003
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