Author:
Chelnokov Yuriy Nikolaevich,Pankratov Ilya Alekseevich,Sapunkov Yakov Grigorievich
Abstract
Abstract
The problem of optimal reorientation of the spacecraft orbit is considered. For solving the problem we used quaternion equations of motion written in rotating coordinate system. The use of quaternion variables makes this consideration more efficient. The problem of optimal control is solved on the basis of the maximum principle. An example of numerical solution of the problem is given.
Subject
Control and Optimization,Modeling and Simulation,Control and Systems Engineering
Cited by
3 articles.
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