Computing Algorithm for Impulse Program of Managing Angular Turn of Spacecraft
Annotation
The study considers the problem of formulating the impulse program for managing angular turn of spacecraft using kinematic equations expressed via the Rodrigues-Hamilton parameters. The suggested computational algorithm is based on using the method of approximate adjustment operator. Such a technique enables one to use simplified algorithms for approximate computing of management within the scheme of numerical solution of complete problem. Computation results are presented to illustrate convergence and high computer resource saving features of the technique.
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