The problem of the time-optimal control
โ
M.V. Levskii
๐
Article
๐
2009
๐
Elsevier Science
๐
English
โ 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