In this paper the problem of attitude tracking control for a rigid spacecraft is addressed. It is assumed that only attitude measurements are available, and thus spacecraft's angular velocity has to be properly estimated. Two alternative schemes are proposed in which the unit quaternion is adopted t
β¦ LIBER β¦
On a stabilizing feedback attitude control
β Scribed by H. Hermes
- Publisher
- Springer
- Year
- 1980
- Tongue
- English
- Weight
- 463 KB
- Volume
- 31
- Category
- Article
- ISSN
- 0022-3239
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