Invariant Stabilization Algorithms in a Control System with Rotating Operating Device
Journal Title: American journal of Engineering Research - Year 2017, Vol 6, Issue 10
Abstract
The publication suggests how to significantly improve the spacecraft center of mass movement stabilization accuracy in the active phases of trajectory correction during interplanetary and transfer flights, which in some cases provides for high navigation accuracy, when rigid trajectory control method is used. The required stability conditions obtained are consistent with the known criteria in the invariant theory.
Authors and Affiliations
Nickolay Zosimovych
Keywords
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