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The problem of optimal control of the orientation of an orbit of a spacecraft as a deformable figure

✍ Scribed by Yu. V. Afanas’eva; Yu. N. Chelnokov


Book ID
111453748
Publisher
SP MAIK Nauka/Interperiodica
Year
2008
Tongue
English
Weight
342 KB
Volume
47
Category
Article
ISSN
1064-2307

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The problem of the time-optimal control
✍ M.V. Levskii 📂 Article 📅 2009 🏛 Elsevier Science 🌐 English ⚖ 341 KB

The use of Pontryagin's maximum principle to solve spacecraft motion control problems is demonstrated. The problem of the optimal control of the spatial reorientation of a spacecraft (as a rigid body) from an arbitrary initial angular position to an assigned final angular position in the minimum rot