Optimal control of reorientation of a spacecraft using free trajectory method
โ Scribed by M. V. Levskii
- Book ID
- 110157862
- Publisher
- Springer
- Year
- 2011
- Tongue
- English
- Weight
- 894 KB
- Volume
- 49
- Category
- Article
- ISSN
- 0010-9525
No coin nor oath required. For personal study only.
๐ SIMILAR VOLUMES
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
In this paper, we consider the planar motion of a free-#ying robot equipped with the jet thrust mechanism. Based on the non-linear equations of motion of the free-#ying robot, we calculate the optimal control such that the fuel consumption is minimized and that the given terminal condition is satis"